US2336711A - Flight control coordinator - Google Patents

Flight control coordinator Download PDF

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US2336711A
US2336711A US418579A US41857941A US2336711A US 2336711 A US2336711 A US 2336711A US 418579 A US418579 A US 418579A US 41857941 A US41857941 A US 41857941A US 2336711 A US2336711 A US 2336711A
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indicator
flight
stick
hand
foot
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US418579A
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Theodore C Barber
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    • GPHYSICS
    • G09EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09BEDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00Simulators for teaching or training purposes
    • G09B9/02Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/08Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
    • G09B9/28Simulation of stick forces or the like

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  • This invention relates to means designed to be used as an aid in the training of airplane pilots, and it has reference more particularly to the provision of means whereby student pilots may be taught, while onthe ground, the proper coordination of the usual hand and foot controls, which, in the actual flight of an airplane, are operated conjointly to maintain the airplane in stable flight.
  • the present invention resides in the provision of a training device for the purpose above stated, which for convenience will be referred to as a training cab; this cab being designed to rest upon the ground, or upon any suitable floor, and which is preferably similar in form and appearance to the pilots cockpit or compartment in the typical training plane, and is equipped with an instrument panel on which a bank indicator is mounted, and an artificial means not under control of the student in training, is provided for causing movements of the bank indicator to take place, to simulate those of the bank indicator of a plane in flight.
  • the pivoted stick has cable connections with the planes elevators whereby direct forward and direct rearward cscillating movements of the stick will cause actuation of the elevators for directing the plane downwardly and upwardly.
  • the stick also has cable connections with the ailerons of right and left wings whereby hinging actuation of the ailerons for banking toward one side or the other, according to the direction and extent of movement of the stick, may be effected.
  • the two foot pedals have cable connections with the rudder, and these connections provide that the pedals may be used selectively to eflect actuation of the rudder for right or left turning.
  • the pedals may be used selectively to eflect actuation of the rudder for right or left turning.
  • the stick be actuated at the same time to move the ailerons to accomplish the proper banking of the plane to maintain it stable during the turning operations.
  • airplanes are normally equipped on the instrument panel at a location conveniently visible to the pilot, with a gravity actuated bank indicator which visibly indicates whether or not the plane is in stable flight.
  • the invention also has for its object to provide improvements upon the device of my copending application, filed on February 11, 1941, under Serial No. 378,407, particularly in the simplification of means for causing the various movements of the bank indicator which are to simulate those indicating conditions of unstable flight, and also in the means and devices operable under control of the hand and foot actuated members, for causing the application of compensating influences, or counteracting forces on the bank indicator whereby to cause it to return to its neutral position or to a position indicating the desired stability of flight.
  • Still another object of the invention is to simplify the structure of the device which is the subject of the above mentioned application, particularly by the elimination of the more or less complicated arangement of cable connections between the hand and foot controls and the bank indicator, and to employ in their stead simple and practical electrical equipment and controls accomplishing the same results.
  • Fig. l is a perspective view of the present training cab.
  • Fig. 2 is an enlarged sectional view of the same, in the longitudinal vertical plane.
  • Fig. 3 is a horizontal section on line 5-3 in Fig. 2.
  • Fig. l is an underside View of the cab floor, showing the relationship of parts mounted thereby.
  • Fig. 5 is a detail of the motor driven means for efiecting the artificial actuation of the bank indicator.
  • Fig. 6 is a cross section on line 6 showing the joy stick mounting.
  • Fig. 7 is a cross section on the line ii in Fig. 3 showing the foot pedal mountin
  • Fig. 8 is a view showing the manner of mounting the stick and wheel which may be used as an alternative in lieu of the stick as shown in 3 in Fig.3
  • Fig, 9 is a side View of the parts as seen in Fig. 8.
  • Fig. 10 is a horizontal section on line ii -i9 in Fig. 8.
  • Fig. 11 is a wiring diagram and diagrammatic illustration of the electrical controls.
  • Fig. 12 is a detail of the mounting of one or" the rheostats used.
  • Fig. 13 is a plan of the same.
  • the present invention comprises a training cab, resembling the cockpit section of an airplane, and equipped with a bank indicator and means whereby the bank indicator may be caused to move from side to side with rather irregular and varying movements.
  • means is operable under control or" hand and foot controls, like those of the typical airplane, whereby to counteract the moving influences artificially produced on the bani: indicator and which cause its irregular movement, so that the indicator may be maintained at a neutral position. It is the intent that the coordinated movements of hand and foot controls must be substantially the same in this training cab, to maintain a stable indication of the bank indicator, as would be required in an actual flight under like action or indications of the bank indicator.
  • the training cab embodied by this invention preferably is in accordance with the showing of Fig. l, and for most satisfactory results is made to resemble the cockpit portion of a typical air plane.
  • Such cabs may be constructed in various dimensions and of difierent materials suitable for its intended purpose.
  • the cab has a horizontal floor i, right and left side walls 2 2', front and rear end walls 3 and 3, and a cowl
  • the construction of the cab resembles that found in an open cockpit airplane and there is a chair, or seat 5 for occuancy by a person in training, and forwardly of the chair, and directly below the cowl, is an instrument panel 6.
  • the side wall 3 thereof is equipped with a hinged door "i giving easy access to the cockpit. It is also to be observed that the horizontal floor E is supported somewhat above the level of the foundation on which the cab rests in order to give the necessary clearance for parts supported below the door, as will presently be explained.
  • a horizontal tube or shaft Disposed transversely of the cockpit, in its forward portion and closely adjacent the floor, is a horizontal tube or shaft it, rigidly supported by brackets ii that are welded thereto near its ends and which are bolted or otherwise secured to the floor l.
  • brackets ii that are welded thereto near its ends and which are bolted or otherwise secured to the floor l.
  • Revolubly supported by the tube, or shaft 58 at its opposite ends and adapted for independent oscillation, are upwardly directed, right and left foot pedals l2 and I'd, each of which has a lever arm projecting doumwardly therefrom, extending somewhat below the floor through openings therein.
  • the openings in this showing are designated by reference numerals i5, and the downwardly extendins levers, for foot pedals i2 and i3, are designated respectively by numerals i211 and i360.
  • a coiled spring it is associated with each of the levers i205 and idea, and are attached unde' tension to the lower ends of these levers.
  • the springs have connection with posts 5? fixed in and extended downwardly from the floor.
  • the pull of the two springs E6 on the levers causes the cable it to be drawn taut and provides further that forward pressure on either one of the pedals will effect a corresponding rearward movement of the other pedal; this being a condition like that in training airplanes.
  • bearings 22 and 23 are fixed in spaced relationship on floor I in the central, longitudinal line of the cockpit, rearwardly of the cross rod l5 and forwardly of the seat 5, each hearing member having an attaching cracket 2d.
  • Rotatably supported by the hearings and 23 are the forward and rearward ends of a horizontal shaft comprising a tubular outer portion 26 and a round rod 2'5 that has a part thereof telescopically and rigidly contained in the tube.
  • Th forward end portion of the tube 26 is revolubly threaded into the forward bearing while the rearward end of the rod 2?, which extends somewhat beyond the rear end of the tube, is revolubly threaded into the bearing 21.
  • a lateral ear 23 is fixed on the rear end of tube 26, and coinciding with this and fixed on the rod 2'! is a lateral ear 29, a bolt 5% is threaded through the ears 23 and 28 to the tube and rod against relative rotation.
  • a lever arm 32 is fixed rigidly to and extends directly downward from the forward end portion of the tube 25, passing through an opening 33 in the floor.
  • coiled springs S t-J4 which have inner ends fixed to the lower end portion of the lever arm 32 and their outer ends fixed to posts or studs 35 in the floor. These springs extend laterally in opposite directions from the lever arm and are fixed under balanced tension whereby the lever arm is normally yieldingly held in vertical position.
  • a tubular cross rod 80 Fixed to the rearward end portion of the rod 27 and extending equally to opposite sides thereof is a tubular cross rod 80, and pivotally mounted by the cross rod is the mounting means for the joystick.
  • This as best shown in Fig. 6, comprises a yoke having opposite side straps ll and H, spaced at the medial portions, then directed toward each other and joined together along their lower end portions, and with their upper end portions directed toward each other and fixed to the opposite sides of a socket member 44 in which the lower end of a lever, or stick i is fitted.
  • the two side straps 4i and 4 i of the yoke pass across the opposite ends of the tubular cross member 4!], and a pivot bolt 46 is extended therethrough and through the tube to thereby pivotally mount the yoke for forward and rearward oscillation of the stick, and it will be understood also that the stick may be oscillated laterally in opposite directions by reason of the rotatable mounting of the longitudinal support in the bearings 22 and 23.
  • the lower end portion of the yoke that is formed by the uniting of the lower end portions of the straps-4I ii', extends down through an openiw 38 in the floor 1.
  • coiled springs E9 and '50 extend forwardly and rearwardly from the opening 48. These springs have adjacent ends fixed to the lower end portion of the yoke, and have their other ends fixed, respectively to posts 5! and 52 that are fixed in the floor. These two springs are under balanced tension and normally act to retain the stick in an upright, neutral position.
  • One of the features of this invention resides in the provision for an interchangeable use of two diiferent types of hand controls; one being the usual joy stick already described, which may be oscillated from a neutral upright position, laterally from side to side, and also from front to rear,
  • FIG. 8 The alternative device has been illustrated in Figs. 8 to where the joy stick 45, as previously used, has been replaced by a stick 53 which likewise is removably applied to the socket 64L
  • This stick is provided with laterally extending and downwardly inclined brace rods 55 and 55' which, at their lower ends, have pivoted connection with brackets 56 and 56' that are fixed to the floor at opposite sides of the floor opening 48.
  • the pivotal connections are affixed by means of bolts 51 which extend through the lower ends of the brace rods and the corresponding brackets, and it is to be observed that the bolts 57 are alined coaxially with the horizontal pivot bolt 46.
  • a hand wheel 6! Fixed on the shaft is a pulley 63 about which a cable 64 is wound and secured, with the opposite end portions of the cable extended downwardly and laterally and attached, respectively, to the ends of laterally and rearwardly extended lever arms 65 and 65' fixed to the tubular member 26. These arms also extend to the axial line of the bolt 46 where the cable connections are made therewith.
  • the tubular member 26 may be rotated by the turning of the hand wheel through the mediacy of the cable connections.
  • the stick 53 still has a forward and rearward movement like that of the joy stick 45 previously described.
  • a bank indicator 70 For the purpose of training the student pilot in control coordination, there is provided centrally, or at other location conveniently visible upon the instrument panel 6, a bank indicator 70.
  • This indicator in this instance, is an electrical instrument and is mechanically controlled to artificially produce certain movements of its indicator element which are intended to simulate those of a bank indicator in an airplane when fiying in an unstable manner.
  • the bank indicator 70 in this instance is an instrument like an ordinary milliammeter operating as a galvanometer.
  • This indicator comprises a housing 14 that is fixed to the panel 6.
  • the usual resistance coil not shown, with terminal connections 76 and H.
  • the bank indicator needle normally vertically disposed at its zero or neutral position, and movable in opposite directions therefrom.
  • the positive and negative poles l6 and Ti of the indicator are electrically connected, respectively, by circuit wire 82 and 83 as illustrated in Fig. 11, with the movable resistance varying elements of rheostats 8i! and 8!, as seen in Fig. 11.
  • a source of electrical current here provided by use of a storage battery indicated at 84, has circuit wires 85 and 86 leading from its positive and negative terminals to poles 81 and 88 of the rheostat Bi, and as noted in Fig. 11, the rheostat 89 has its poles 89-90 electrically joined by wires 9! and 92 with the wires 85 and 36.
  • the two rheostats, 8B and 85 are associated with the mechanical equipment in the manner best illustrated in Fig. 4, wherein it is shown that the rheostat 8! is mounted on the under side of the floor I near the transverse run of cable l8.
  • Each rheostat comprises a housing in which there is a resistance coil and a contact movable therealo-ng by the movement of a lever arm extended from the housing.
  • the resistance element of the rheostat BI is designated diagrammatically in Fig. 11 by numeral Ma and a movable resistance varying contact is designated at B5 and is fixed on a pivot shaft 95 which has an actuating lever arm El.
  • This arm Ell has a cable connection 98 with the cable it, and a coiled spring 93 is attached under tension to the lever to keep the cable 9 3 taut.
  • the lever 97 will be caused to move accordingly by reason of its connection with cable l8. This will actuate the contact member 5 5 along the resistance coil 8 i a.
  • the rheostat 8d likewise, has a housing Silas, a resistance element 55a, and a resistance varying contact member lei on a pivot shaft N32 to which an actuating lever arm H313 is fixed.
  • the arm I83 has a cable connection iil i with the lower end of the joy stick yoke and a coiled spring 665 is attached under tension to arm iilt to keep the cable taut.
  • the rheostat 83 its housing Eda: is rotatably mounted by a pivot tube Hi8 carried by a bracket Hi3 fixed to the under side of floor I.
  • a lever arm 1 l2 Fastened to the housing 8dr is a lever arm 1 l2, and the outer end or" this arm has a link 5 i3 pivotally connecting it with one arm, M ld of a bell crank lever lid, operable as presently described, to rotatably move the housing, thus to cause relative movements of the resistance element 86a and contact member lei.
  • the electric motor M22 is energized and set in operation so that through the action of cam E23 and bell crank mechanism disclosed, the housing 85$ of the rheostat 88 will be given rotative movements of various amounts in opposite directions.
  • These rotative movements of housing 8% cause a relative adjustment of the contact element along the resistance coil of the rheostat, and in accordance with the Well known principles, thus cause the needle of the bank indicator to move from neutral indication toward one side or the other to varying extent in accordance with the action of the housing under influence of the cam lZii.
  • the bank indicator can be brought back to show a neutral indication, it will be understood therefore that should the bank indicator needle swing to the left, indicating a high right wing, the proper correcting action of the joy stick is to press it to the right.
  • This causes a compensating movement of the rheostat lever arm IE3, tending thereby to counteract the movement of the resistance element which has been caused by the bell crank linkage.
  • the student depresses the corresponding foot pedal, thereby moving the cable l8 so that through the lever 9?
  • the contact element of the rheostat ti is moved accordingly; it being understood that is the contact element of the rheostat 55 is caused to move one direction, the contact element of the other rheostat should be moved correspondingly the opposite direction, thus to effect a balance of resistances which will stabilize the needle of the indicator 18.
  • the student pilot may be taught the proper coordinated movements of the hand and foot controls and how to effect the bringing of the needle back to a neutral indication, and since these coordinated movements are the same in this training device as are required in the actual flying plane, the training period for this particular type of instruction can be materially shortened and all danger removed.
  • I provide a variable resistance as at I25 interposed in the wire 85. This may be controlled by a button as at I25 located on the instrument panel. Also, there maybe a suitable switch as at lei? for opening or closing the circuit.
  • the subject matter contained in this case covers a stationary or ground trainer for teaching coordination of hand and foot controls as used in an airplane in flight for maintaining stability in flight, and the invention features the use of a ball bank simulator element and an artificial means for causing typical flight movements thereof, in combination with means operable under control of the hand and foot controls, Whereby the moving influence of the artificial means may be nullified, thus to cause the ball bank simulator element to assume a position that would indicate stable flight.
  • typical flight movements I mean movements from right to left of the bank indicator, such as are produced when an airplane is in unstable flight; it being understood that the ball bank indicator is in neutral position when the plane is stabilized.
  • an electrically energized bank indicator simulator having a movable indicator element, means for causing the application of variable electric iorces to said indicator to effect typical movements of the indicator element of varying degree and direction, movable right and left foot controls adapted to be selectively actuated by the users feet, a hand control adapted to be actuated to right or left by the users hands, and means operable under the conjoint control of the said hand and foot controls for producing counteracting electrical influences in the bank indicator simulator, variable in direction and extent in accordance with the selection or controls and extent of their movement, and whereby the indicator moving forces may be nullified.
  • a coordinator of the character described comprising in combination, an electrically energized bank indicator simulator having an indicator element movable from a neutral indication to right or left according to direction of flow of current and potential on its terminals, selectively operable right and left foot controls, a hand control lever selectively movable from neutral position to right and left sides, an electrical resistance element associated with the hand control, a source of electrical energy with connections from its positive and negative poles to the opposite ends of each of the resistance elements, a contactor for each resistance element, means electrically connecting the contactors respectively with the terminals of the bank indicator, means for causing relative movement of one of the contactors along its resistance, and means operable by movements of said hand and foot controls to right or left to adjust the contactors along the resistance elements corresponding thereto accordingly to eiTect the neutralization of forces in the indicator.
  • a coordinator of the character described comprising, in combination, right and left foot pedals operable selectively by the users feet, a hand control member operable selectively to right or left by the users hands, an electrical resist ance element associated with the foot control pedals having a contactor movable therealong, a resistance element associated with the hand con trol, and a contactor movable therealong, a bank indicator simulator comprising a galvanometer having its opposite poles electrically connected respectively to the contactors of said resistance elements, a source of electrical energy having electrical connections from its positive and negative poles, respectively, to the opposite ends of the said resistance elements, mechanically driven means for causing movement of one of the contactor elements in different direction and extent along its resistance coil to change potential on the galvanometer terminals and effect typical movements of the galvanometer needle, and means movable with the foot pedals and other means movable by the hand control to cause a readjustment of the contact elements along their corresponding resistances to efiect the neutralization of the needle moving influence in the gal
  • a set of foot pedals adapted to be depressed respectively by the users right and left feet, a joy stick operable to right and left from neutral by the users hands, springs acting on the pedals and on the stick to yieldingly retain them at their neutral positions, a cable connection between the pedals and movable in opposite directions according to the depression of one or the other of the foot pedals, an electrical resistance coil associated with the pedals, a contactor for the coil, and means connecting the contactor and cable whereby the contactor will be moved in opposite directions along the resistance according to the pedal depressed, a resistance coil associated with the joy stick, a contactor for the coil, and means connecting the contactor and joy stick for moving the contactor along the coil in opposite directions and extent as determined by the direction and extent of movement of the stick, a source of electrical energy having positive and negative poles electrically joined with the opposite ends of said resistance coils, and a bank indicator simulator comprising a galvanometer having its opposite poles electrically connected with the said contactors, and
  • a stationary coordinator trainer for airplane fiight training comprising a cockpit frame, hand and foot control devices, and a turn and bank indicator element simulating parts of an airplane; an auxiliary means operable to cause typical flight movements of the turn and bank indicator element, and means associated with the said auxiliary means and operable by the hand and foot control devices to counteract the movement producing action on the indicator element of the said auxiliary means.

Description

Dec. 14, 1943.- T. BARBER FLIGHT CONTROL COORDENATOR 4 Sheets-Sheet 1 Filed Nov. 10, 1941 Dec. 14, 1943. 1". c. BARBER 2,336,711-
FLIGHT CONTROL COORDINATOR Filed Nov 10,1941 4 Shets-Sheet 2 INVENTOR 72/500025 C. BHEBEB ATTORNEY- T. C. BARBER FLIGHT CONTROL CQORDINATOR Dec. 14, 1943.
4 Sheets-Sheet 3 Filed Nov. 10, 1941 TOR INVE 72/500025 CI gmasz/e BY Q5 l lllll ll-Illllllllllrl'lllllllll ATTORNEY Dec. 14, 1943. c BARBER 2,336,711
FLIGHT CONTROL COORDINATOR Filed Nov. 10, 1941 4 Sheets-Sheet 4 lNVENTOR 72/[00035 C. 5/4/ 552,
TTORNEY Patented Dec. 14, 1943 ilN'i'ED STAS E ATENT OFFICE FLIGHT CONTROL COORDINATOR Theodore 0. Barber, Seattle, Wash. Application November 10, 1941, Serial No. 418,579
Claims.
This invention relates to means designed to be used as an aid in the training of airplane pilots, and it has reference more particularly to the provision of means whereby student pilots may be taught, while onthe ground, the proper coordination of the usual hand and foot controls, which, in the actual flight of an airplane, are operated conjointly to maintain the airplane in stable flight.
More specifically stated, the present invention resides in the provision of a training device for the purpose above stated, which for convenience will be referred to as a training cab; this cab being designed to rest upon the ground, or upon any suitable floor, and which is preferably similar in form and appearance to the pilots cockpit or compartment in the typical training plane, and is equipped with an instrument panel on which a bank indicator is mounted, and an artificial means not under control of the student in training, is provided for causing movements of the bank indicator to take place, to simulate those of the bank indicator of a plane in flight. Also, there are hand and foot controls, like those in the typical airplane, operable by the student in the same manner and by the same coordination as would be required in actual flight, to counteract the artificially induced movements of the bank indicator and thus cause the return of the bank indicator to a stable or neutral indication.
Explanatory to the invention, it Will here be stated that, generally speaking, the control and stability of an airplane in normal flight is maintained by the proper manipulation of ailerons, rudder and elevators. These controls are placed under control of the pilot through the mediacy of right and left foot controls or pedals, and a hand lever, referred to as the stick which lever is pivoted for forward and rearward, and also lateral oscillations; the direction of flight, or the control of flight being dependent upon the conjoint action of the rudder, elevators, and ailerons, as actuated by the above mentioned controls.
In the usual arrangement and connection of hand and foot controls, the pivoted stick has cable connections with the planes elevators whereby direct forward and direct rearward cscillating movements of the stick will cause actuation of the elevators for directing the plane downwardly and upwardly. The stick also has cable connections with the ailerons of right and left wings whereby hinging actuation of the ailerons for banking toward one side or the other, according to the direction and extent of movement of the stick, may be effected.
The two foot pedals have cable connections with the rudder, and these connections provide that the pedals may be used selectively to eflect actuation of the rudder for right or left turning. To those familiar with this art, it is understood that in making a turn to right, or left, under influence of the rudder movement, it is the accepted practise that the stick be actuated at the same time to move the ailerons to accomplish the proper banking of the plane to maintain it stable during the turning operations.
As an aid to flight control, airplanes are normally equipped on the instrument panel at a location conveniently visible to the pilot, with a gravity actuated bank indicator which visibly indicates whether or not the plane is in stable flight.
It is understood, furthermore, that for the proper or satisfactory control of a plane in flight, there must be proper coordination of the controls, as operated by hand and foot. In actual flight, the pilot endeavors to maintain the bank indicator at a neutral indication, in turning and banking, as well as in straight flight, and this may be accomplished through the proper coordination of the hand and foot controls, the exact manipulations of which might vary under different flying conditions and at different speeds, and while in some unusual situations, stability in flight might be maintained by the manipulation of hand or the foot controlled devices individually, it is the usual practise, and is the accepted procedure, that stability be accomplished through the conjoint and properly coordinated action of foot and hand controls.
In View of the foregoing, it has been the principal object of this invention to provide means for expediting the training of student pilots in the rudiments of handling and controlling an airplane in flight, and more particularly for expediting the teaching of proper coordination of movements of hand and foot controls, to maintain stable flight.
The invention also has for its object to provide improvements upon the device of my copending application, filed on February 11, 1941, under Serial No. 378,407, particularly in the simplification of means for causing the various movements of the bank indicator which are to simulate those indicating conditions of unstable flight, and also in the means and devices operable under control of the hand and foot actuated members, for causing the application of compensating influences, or counteracting forces on the bank indicator whereby to cause it to return to its neutral position or to a position indicating the desired stability of flight.
Still another object of the invention is to simplify the structure of the device which is the subject of the above mentioned application, particularly by the elimination of the more or less complicated arangement of cable connections between the hand and foot controls and the bank indicator, and to employ in their stead simple and practical electrical equipment and controls accomplishing the same results.
Still other objects of the invention reside in the details of construction of parts, in their relationship, and in their mode of operation, as will hereinafter be fully described.
In accomplishing these and other objects of the invention, I have provided the improved details of construction, the preferred forms of which are illustrated in the accompanying drawings, wherein- Fig. l is a perspective view of the present training cab.
Fig. 2 is an enlarged sectional view of the same, in the longitudinal vertical plane.
Fig. 3 is a horizontal section on line 5-3 in Fig. 2.
Fig. l is an underside View of the cab floor, showing the relationship of parts mounted thereby.
Fig. 5 is a detail of the motor driven means for efiecting the artificial actuation of the bank indicator.
Fig. 6 is a cross section on line 6 showing the joy stick mounting.
Fig. 7 is a cross section on the line ii in Fig. 3 showing the foot pedal mountin Fig. 8 is a view showing the manner of mounting the stick and wheel which may be used as an alternative in lieu of the stick as shown in 3 in Fig.3
Fig. 6.
Fig, 9 is a side View of the parts as seen in Fig. 8.
Fig. 10 is a horizontal section on line ii -i9 in Fig. 8.
Fig. 11 is a wiring diagram and diagrammatic illustration of the electrical controls.
Fig. 12 is a detail of the mounting of one or" the rheostats used.
Fig. 13 is a plan of the same.
In brief, the present invention comprises a training cab, resembling the cockpit section of an airplane, and equipped with a bank indicator and means whereby the bank indicator may be caused to move from side to side with rather irregular and varying movements. Also, wherein means is operable under control or" hand and foot controls, like those of the typical airplane, whereby to counteract the moving influences artificially produced on the bani: indicator and which cause its irregular movement, so that the indicator may be maintained at a neutral position. It is the intent that the coordinated movements of hand and foot controls must be substantially the same in this training cab, to maintain a stable indication of the bank indicator, as would be required in an actual flight under like action or indications of the bank indicator.
Referring more in detail to the drawings- The training cab embodied by this invention preferably is in accordance with the showing of Fig. l, and for most satisfactory results is made to resemble the cockpit portion of a typical air plane. Such cabs may be constructed in various dimensions and of difierent materials suitable for its intended purpose. As here shown, the cab has a horizontal floor i, right and left side walls 2 2', front and rear end walls 3 and 3, and a cowl The construction of the cab resembles that found in an open cockpit airplane and there is a chair, or seat 5 for occuancy by a person in training, and forwardly of the chair, and directly below the cowl, is an instrument panel 6.
For convenience in use of the cab, the side wall 3 thereof is equipped with a hinged door "i giving easy access to the cockpit. It is also to be observed that the horizontal floor E is supported somewhat above the level of the foundation on which the cab rests in order to give the necessary clearance for parts supported below the door, as will presently be explained.
Disposed transversely of the cockpit, in its forward portion and closely adjacent the floor, is a horizontal tube or shaft it, rigidly supported by brackets ii that are welded thereto near its ends and which are bolted or otherwise secured to the floor l. Revolubly supported by the tube, or shaft 58, at its opposite ends and adapted for independent oscillation, are upwardly directed, right and left foot pedals l2 and I'd, each of which has a lever arm projecting doumwardly therefrom, extending somewhat below the floor through openings therein. The openings in this showing are designated by reference numerals i5, and the downwardly extendins levers, for foot pedals i2 and i3, are designated respectively by numerals i211 and i360.
By reference to Fig. 8, which shows the parts at the underside of the fiOOl I, it will be observed that a coiled spring it is associated with each of the levers i205 and idea, and are attached unde' tension to the lower ends of these levers. Also, the springs have connection with posts 5? fixed in and extended downwardly from the floor. Also, there is a cable l3 attached at its opposite ends, respectively, to the lower end portions of the lovers 52a and lEa, and extending forvardly therefrom and about laterally spaced guide sheaves id and 26, providing that a part of the cable extend transversely of the floor. The pull of the two springs E6 on the levers causes the cable it to be drawn taut and provides further that forward pressure on either one of the pedals will effect a corresponding rearward movement of the other pedal; this being a condition like that in training airplanes.
Referring now more particularly to Figs. 2 and 3, it is to be observed that bearings 22 and 23 are fixed in spaced relationship on floor I in the central, longitudinal line of the cockpit, rearwardly of the cross rod l5 and forwardly of the seat 5, each hearing member having an attaching cracket 2d.
Rotatably supported by the hearings and 23 are the forward and rearward ends of a horizontal shaft comprising a tubular outer portion 26 and a round rod 2'5 that has a part thereof telescopically and rigidly contained in the tube. Th forward end portion of the tube 26 is revolubly threaded into the forward bearing while the rearward end of the rod 2?, which extends somewhat beyond the rear end of the tube, is revolubly threaded into the bearing 21. A lateral ear 23 is fixed on the rear end of tube 26, and coinciding with this and fixed on the rod 2'! is a lateral ear 29, a bolt 5% is threaded through the ears 23 and 28 to the tube and rod against relative rotation. This particular connection will later b referred to in describing the use of the alternative stick shown in Figs. 6 and 7.
A lever arm 32 is fixed rigidly to and extends directly downward from the forward end portion of the tube 25, passing through an opening 33 in the floor. Located below the floor, at opposite sides of the opening, and transversely directed, are coiled springs S t-J4 which have inner ends fixed to the lower end portion of the lever arm 32 and their outer ends fixed to posts or studs 35 in the floor. These springs extend laterally in opposite directions from the lever arm and are fixed under balanced tension whereby the lever arm is normally yieldingly held in vertical position.
Fixed to the rearward end portion of the rod 27 and extending equally to opposite sides thereof is a tubular cross rod 80, and pivotally mounted by the cross rod is the mounting means for the joystick. This, as best shown in Fig. 6, comprises a yoke having opposite side straps ll and H, spaced at the medial portions, then directed toward each other and joined together along their lower end portions, and with their upper end portions directed toward each other and fixed to the opposite sides of a socket member 44 in which the lower end of a lever, or stick i is fitted. The two side straps 4i and 4 i of the yoke pass across the opposite ends of the tubular cross member 4!], and a pivot bolt 46 is extended therethrough and through the tube to thereby pivotally mount the yoke for forward and rearward oscillation of the stick, and it will be understood also that the stick may be oscillated laterally in opposite directions by reason of the rotatable mounting of the longitudinal support in the bearings 22 and 23.
The lower end portion of the yoke that is formed by the uniting of the lower end portions of the straps-4I ii', extends down through an openiw 38 in the floor 1. At the under side of the fioor, coiled springs E9 and '50 extend forwardly and rearwardly from the opening 48. These springs have adjacent ends fixed to the lower end portion of the yoke, and have their other ends fixed, respectively to posts 5! and 52 that are fixed in the floor. These two springs are under balanced tension and normally act to retain the stick in an upright, neutral position.
One of the features of this invention resides in the provision for an interchangeable use of two diiferent types of hand controls; one being the usual joy stick already described, which may be oscillated from a neutral upright position, laterally from side to side, and also from front to rear,
while the other type of control comprises a lever,
or stick, that may be moved directly forwardly or rearwardly for control of the elevators but in lieu of the lateral movements for control of the ailerons, carries at its upper end a rotatable hand wheel with cable connections for the rotative action of the tube 26.
To use this alternative type of stick, it is required that the bolt 36 which fixed the parts 26 and 21 against relative rotation, be removed, the joy stick 45 withdrawn from its socket, the alternative stick applied to the socket, and parts attached to the floor as will now be described.
The alternative device has been illustrated in Figs. 8 to where the joy stick 45, as previously used, has been replaced by a stick 53 which likewise is removably applied to the socket 64L This stick is provided with laterally extending and downwardly inclined brace rods 55 and 55' which, at their lower ends, have pivoted connection with brackets 56 and 56' that are fixed to the floor at opposite sides of the floor opening 48. The pivotal connections are affixed by means of bolts 51 which extend through the lower ends of the brace rods and the corresponding brackets, and it is to be observed that the bolts 57 are alined coaxially with the horizontal pivot bolt 46.
Rotatably mounted at the upper end of the lever 53, is a hand wheel 6!] fixed on a supporting shaft 6! that revolves in a bearing 62 at the upper end of the stick. Fixed on the shaft is a pulley 63 about which a cable 64 is wound and secured, with the opposite end portions of the cable extended downwardly and laterally and attached, respectively, to the ends of laterally and rearwardly extended lever arms 65 and 65' fixed to the tubular member 26. These arms also extend to the axial line of the bolt 46 where the cable connections are made therewith.
In the use of this alternative control, with the bolt 3!! removed from the ears 28 and 29, the tubular member 26 may be rotated by the turning of the hand wheel through the mediacy of the cable connections. The stick 53, however, still has a forward and rearward movement like that of the joy stick 45 previously described.
For the purpose of training the student pilot in control coordination, there is provided centrally, or at other location conveniently visible upon the instrument panel 6, a bank indicator 70. This indicator, in this instance, is an electrical instrument and is mechanically controlled to artificially produce certain movements of its indicator element which are intended to simulate those of a bank indicator in an airplane when fiying in an unstable manner. Also, there are means controlled by the student pilot for counteracting and compensating for these artificially produced movements of the bank indicator; it being the intent that the pilot in training shall, by those certain coordinated movements of the hand and foot controls, as would be required in actual flight, cause the application of counter-acting forces which will maintain the bank indicator at, or return it to a stable indication.
The bank indicator 70 in this instance, is an instrument like an ordinary milliammeter operating as a galvanometer. This indicator comprises a housing 14 that is fixed to the panel 6. In the housing is the usual resistance coil, not shown, with terminal connections 76 and H. Also, there is the bank indicator needle 18, normally vertically disposed at its zero or neutral position, and movable in opposite directions therefrom. The positive and negative poles l6 and Ti of the indicator are electrically connected, respectively, by circuit wire 82 and 83 as illustrated in Fig. 11, with the movable resistance varying elements of rheostats 8i! and 8!, as seen in Fig. 11.
A source of electrical current here provided by use of a storage battery indicated at 84, has circuit wires 85 and 86 leading from its positive and negative terminals to poles 81 and 88 of the rheostat Bi, and as noted in Fig. 11, the rheostat 89 has its poles 89-90 electrically joined by wires 9! and 92 with the wires 85 and 36.
The two rheostats, 8B and 85, are associated with the mechanical equipment in the manner best illustrated in Fig. 4, wherein it is shown that the rheostat 8! is mounted on the under side of the floor I near the transverse run of cable l8. Each rheostat comprises a housing in which there is a resistance coil and a contact movable therealo-ng by the movement of a lever arm extended from the housing. The resistance element of the rheostat BI is designated diagrammatically in Fig. 11 by numeral Ma and a movable resistance varying contact is designated at B5 and is fixed on a pivot shaft 95 which has an actuating lever arm El. This arm Ell has a cable connection 98 with the cable it, and a coiled spring 93 is attached under tension to the lever to keep the cable 9 3 taut. Thus, since the cable i3 will be moved in opposite directions in accordance with depression of the foot pedals i2 and it, it can be seen that the lever 97 will be caused to move accordingly by reason of its connection with cable l8. This will actuate the contact member 5 5 along the resistance coil 8 i a.
The rheostat 8d, likewise, has a housing Silas, a resistance element 55a, and a resistance varying contact member lei on a pivot shaft N32 to which an actuating lever arm H313 is fixed. The arm I83 has a cable connection iil i with the lower end of the joy stick yoke and a coiled spring 665 is attached under tension to arm iilt to keep the cable taut.
In the use of the rheostat 83, its housing Eda: is rotatably mounted by a pivot tube Hi8 carried by a bracket Hi3 fixed to the under side of floor I. Fastened to the housing 8dr is a lever arm 1 l2, and the outer end or" this arm has a link 5 i3 pivotally connecting it with one arm, M ld of a bell crank lever lid, operable as presently described, to rotatably move the housing, thus to cause relative movements of the resistance element 86a and contact member lei.
It will now be understood, by referring to Fig. 11, that with both rheostats in neutral setting, the indicator needle ii of the bank indicator it will be located at a neutral indication. However,
should the contact element of rheostat 55 be moved toward either side by a relative movement of the resistance and contact element, this will cause movement of the bank indicator to one side or the other and the extent of movement and direction will be in accordance with the extent and direction of rotative movement of the housing. Thus, it is possible by this means to produce movements of the bank indicator to simulate those of the bank indicator of an airplane in unstable flight. These artificially produced movements can be made H1016 or less erratic through actuation of the bell crank lid, and in this instance, I have shown it to be actuated by the rotation of a plural-lobed cam 529 that is fixed on a shaft 52! driven by an electric motor i222 through suitable gear reduction, as at i 53, that may be fixed in any suitable manner to the under side of floor 5 or at any other suitable place.
Assuming the rheostats and bank indicator to be so arranged, and electrically connected, their use for training a student pilot in coordination of controls is as follows:
First, the electric motor M22 is energized and set in operation so that through the action of cam E23 and bell crank mechanism disclosed, the housing 85$ of the rheostat 88 will be given rotative movements of various amounts in opposite directions. These rotative movements of housing 8% cause a relative adjustment of the contact element along the resistance coil of the rheostat, and in accordance with the Well known principles, thus cause the needle of the bank indicator to move from neutral indication toward one side or the other to varying extent in accordance with the action of the housing under influence of the cam lZii.
Since the purpose of the present apparatus is to teach coordination of hand and foot controls, and since the student is taught as a fundamental principle that by proper coordination of their movements, the bank indicator can be brought back to show a neutral indication, it will be understood therefore that should the bank indicator needle swing to the left, indicating a high right wing, the proper correcting action of the joy stick is to press it to the right. This causes a compensating movement of the rheostat lever arm IE3, tending thereby to counteract the movement of the resistance element which has been caused by the bell crank linkage. At the same time, the student depresses the corresponding foot pedal, thereby moving the cable l8 so that through the lever 9? and spring connection, the contact element of the rheostat ti is moved accordingly; it being understood that is the contact element of the rheostat 55 is caused to move one direction, the contact element of the other rheostat should be moved correspondingly the opposite direction, thus to effect a balance of resistances which will stabilize the needle of the indicator 18.
With the bank indicator thus being artificially moved from side to side to varying degrees, the student pilot may be taught the proper coordinated movements of the hand and foot controls and how to effect the bringing of the needle back to a neutral indication, and since these coordinated movements are the same in this training device as are required in the actual flying plane, the training period for this particular type of instruction can be materially shortened and all danger removed.
In order that the intensity of the movement of the needle 78 of the indicator may be somewhat controlled, I provide a variable resistance as at I25 interposed in the wire 85. This may be controlled by a button as at I25 located on the instrument panel. Also, there maybe a suitable switch as at lei? for opening or closing the circuit.
The subject matter contained in this case covers a stationary or ground trainer for teaching coordination of hand and foot controls as used in an airplane in flight for maintaining stability in flight, and the invention features the use of a ball bank simulator element and an artificial means for causing typical flight movements thereof, in combination with means operable under control of the hand and foot controls, Whereby the moving influence of the artificial means may be nullified, thus to cause the ball bank simulator element to assume a position that would indicate stable flight. In use of the term typical flight movements, I mean movements from right to left of the bank indicator, such as are produced when an airplane is in unstable flight; it being understood that the ball bank indicator is in neutral position when the plane is stabilized.
Having thus described my invention, what I claim as new therein and desire to secure by Letters Patent is:
1. In a coordinator of the character described, in combination, an electrically energized bank indicator simulator having a movable indicator element, means for causing the application of variable electric iorces to said indicator to effect typical movements of the indicator element of varying degree and direction, movable right and left foot controls adapted to be selectively actuated by the users feet, a hand control adapted to be actuated to right or left by the users hands, and means operable under the conjoint control of the said hand and foot controls for producing counteracting electrical influences in the bank indicator simulator, variable in direction and extent in accordance with the selection or controls and extent of their movement, and whereby the indicator moving forces may be nullified.
2. A coordinator of the character described comprising in combination, an electrically energized bank indicator simulator having an indicator element movable from a neutral indication to right or left according to direction of flow of current and potential on its terminals, selectively operable right and left foot controls, a hand control lever selectively movable from neutral position to right and left sides, an electrical resistance element associated with the hand control, a source of electrical energy with connections from its positive and negative poles to the opposite ends of each of the resistance elements, a contactor for each resistance element, means electrically connecting the contactors respectively with the terminals of the bank indicator, means for causing relative movement of one of the contactors along its resistance, and means operable by movements of said hand and foot controls to right or left to adjust the contactors along the resistance elements corresponding thereto accordingly to eiTect the neutralization of forces in the indicator.
3. A coordinator of the character described comprising, in combination, right and left foot pedals operable selectively by the users feet, a hand control member operable selectively to right or left by the users hands, an electrical resist ance element associated with the foot control pedals having a contactor movable therealong, a resistance element associated with the hand con trol, and a contactor movable therealong, a bank indicator simulator comprising a galvanometer having its opposite poles electrically connected respectively to the contactors of said resistance elements, a source of electrical energy having electrical connections from its positive and negative poles, respectively, to the opposite ends of the said resistance elements, mechanically driven means for causing movement of one of the contactor elements in different direction and extent along its resistance coil to change potential on the galvanometer terminals and effect typical movements of the galvanometer needle, and means movable with the foot pedals and other means movable by the hand control to cause a readjustment of the contact elements along their corresponding resistances to efiect the neutralization of the needle moving influence in the gal- Vanometer.
4. In a coordinator of the character described, a set of foot pedals adapted to be depressed respectively by the users right and left feet, a joy stick operable to right and left from neutral by the users hands, springs acting on the pedals and on the stick to yieldingly retain them at their neutral positions, a cable connection between the pedals and movable in opposite directions according to the depression of one or the other of the foot pedals, an electrical resistance coil associated with the pedals, a contactor for the coil, and means connecting the contactor and cable whereby the contactor will be moved in opposite directions along the resistance according to the pedal depressed, a resistance coil associated with the joy stick, a contactor for the coil, and means connecting the contactor and joy stick for moving the contactor along the coil in opposite directions and extent as determined by the direction and extent of movement of the stick, a source of electrical energy having positive and negative poles electrically joined with the opposite ends of said resistance coils, and a bank indicator simulator comprising a galvanometer having its opposite poles electrically connected with the said contactors, and mechanically operable means for effecting the movement of one of the resistance coils and its contactors to produce action of the bank indicator needle.
5. A stationary coordinator trainer for airplane fiight training comprising a cockpit frame, hand and foot control devices, and a turn and bank indicator element simulating parts of an airplane; an auxiliary means operable to cause typical flight movements of the turn and bank indicator element, and means associated with the said auxiliary means and operable by the hand and foot control devices to counteract the movement producing action on the indicator element of the said auxiliary means.
THEODORE C. BARBER.
US418579A 1941-11-10 1941-11-10 Flight control coordinator Expired - Lifetime US2336711A (en)

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Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2422552A (en) * 1943-08-16 1947-06-17 California Aero Glider Co Inc Preflight pilot training aircraft apparatus
US2428706A (en) * 1944-07-05 1947-10-07 Fred W Genrich Jr Preflight training plane
US2460743A (en) * 1944-06-30 1949-02-01 Bell Telephone Labor Inc Aircraft personnel trainer
US2463602A (en) * 1946-09-12 1949-03-08 Dehmel Richard Carl Rough air simulating means for grounded aircraft trainers
US2472888A (en) * 1945-02-21 1949-06-14 Ibm Apparatus for training pilots and other aircraft personnel
US2485266A (en) * 1944-07-14 1949-10-18 Link Aviation Inc Training apparatus
US2485286A (en) * 1948-01-02 1949-10-18 Link Aviation Inc Inclinometer and compass indicating means for grounded aviation trainers
US2487758A (en) * 1946-04-25 1949-11-08 Link Aviation Inc Instrument simulating means for grounded aviation trainers
US2514606A (en) * 1945-08-01 1950-07-11 Curtiss Wright Corp Trainer control loading device
US2519233A (en) * 1944-06-30 1950-08-15 Bell Telephone Labor Inc Aircraft trainer
US2526371A (en) * 1947-03-05 1950-10-17 Gordon Laughead Company Airplane flight instruction device
US2554155A (en) * 1946-12-13 1951-05-22 Bell Telephone Labor Inc Ground trainer for training aircraft crews
US2584261A (en) * 1944-06-30 1952-02-05 Bell Telephone Labor Inc Ground trainer for aircraft crew
US2604706A (en) * 1949-12-23 1952-07-29 Walter F Grether Apparatus for testing the coordination of aviators
US3702504A (en) * 1970-06-17 1972-11-14 Cramer Instr Flight School Inc Aircraft instrument operation trainer
US4527980A (en) * 1983-04-07 1985-07-09 Miller Robert W Flight simulating video game

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2422552A (en) * 1943-08-16 1947-06-17 California Aero Glider Co Inc Preflight pilot training aircraft apparatus
US2519233A (en) * 1944-06-30 1950-08-15 Bell Telephone Labor Inc Aircraft trainer
US2460743A (en) * 1944-06-30 1949-02-01 Bell Telephone Labor Inc Aircraft personnel trainer
US2584261A (en) * 1944-06-30 1952-02-05 Bell Telephone Labor Inc Ground trainer for aircraft crew
US2428706A (en) * 1944-07-05 1947-10-07 Fred W Genrich Jr Preflight training plane
US2485266A (en) * 1944-07-14 1949-10-18 Link Aviation Inc Training apparatus
US2472888A (en) * 1945-02-21 1949-06-14 Ibm Apparatus for training pilots and other aircraft personnel
US2514606A (en) * 1945-08-01 1950-07-11 Curtiss Wright Corp Trainer control loading device
US2487758A (en) * 1946-04-25 1949-11-08 Link Aviation Inc Instrument simulating means for grounded aviation trainers
US2463602A (en) * 1946-09-12 1949-03-08 Dehmel Richard Carl Rough air simulating means for grounded aircraft trainers
US2554155A (en) * 1946-12-13 1951-05-22 Bell Telephone Labor Inc Ground trainer for training aircraft crews
US2526371A (en) * 1947-03-05 1950-10-17 Gordon Laughead Company Airplane flight instruction device
US2485286A (en) * 1948-01-02 1949-10-18 Link Aviation Inc Inclinometer and compass indicating means for grounded aviation trainers
US2604706A (en) * 1949-12-23 1952-07-29 Walter F Grether Apparatus for testing the coordination of aviators
US3702504A (en) * 1970-06-17 1972-11-14 Cramer Instr Flight School Inc Aircraft instrument operation trainer
US4527980A (en) * 1983-04-07 1985-07-09 Miller Robert W Flight simulating video game

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