US2207084A - Retractable antenna - Google Patents

Retractable antenna Download PDF

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Publication number
US2207084A
US2207084A US253014A US25301439A US2207084A US 2207084 A US2207084 A US 2207084A US 253014 A US253014 A US 253014A US 25301439 A US25301439 A US 25301439A US 2207084 A US2207084 A US 2207084A
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United States
Prior art keywords
antenna
housing
door
doors
closure member
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Expired - Lifetime
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US253014A
Inventor
Herbert L Bowers
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Bell Aircraft Corp
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Bell Aircraft Corp
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Filing date
Publication date
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Priority to US253014A priority Critical patent/US2207084A/en
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Publication of US2207084A publication Critical patent/US2207084A/en
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Expired - Lifetime legal-status Critical Current

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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/08Means for collapsing antennas or parts thereof
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/12Supports; Mounting means
    • H01Q1/1235Collapsible supports; Means for erecting a rigid antenna

Definitions

  • My invention relates to retractable antennae, and more particularly for retractable, antennae of the loop type, such as may be adapted for use in aircraft.
  • loop antenna is useful in connection with radio, compass and direction finder arrangements.
  • Yet another object of the invention is to pro vide a construction of loop antenna. which permits it to be positively and readily placed in onerative position. and rotated in any desired direction in that position.
  • a still further object of the invention is to provide an antenna which can be quickly brought into either operative or inoperative positions, and when in such positions, the surface of the fuse lage will be closed and flush.
  • Figure l is a view partly in section showing my loop antenna in the out or operative position, one of the doors through which. it has been. swung being shown in the open position and the other door showing its open positions by dotted lines;
  • Fig. 2 is a sectional view showing my loop antenna housed within the fuselage
  • Fig. 3 is a sectional view showing the position of the parts when the main door is closed;
  • FIG. 4 is a sectional view showing the details of construction of the antenna mounting
  • Fig. 5 is a bottom plan view of my construction with the doors closed. 5
  • I have shown an airplane fuselage i having an opening 2 therein.
  • the hinges 5 and 5 have their plates 7 and B riveted to a downwardly projecting bracket 9.
  • the other plates are attached to the doors 3 and l, respectively, as exemplified with respect to door 4, at
  • Door carries, adjacent its periphery, an offset recess !2 formed therein.
  • a resilient cushion i3 is attached to the inner surface of the fuselage adjacent the opening 2. This resilient cushion i3 is adapted to contact against the peripheral recess i2 and cause a tight fit.
  • the outer surfaces of each of the doors 3 and i are adapted to follow the curve of the fuselage, as indicated in Figure 3.
  • Door 3 has a similar oiiset recess l2 which is adapted, in the closed position, to v bear against the cushion It to make a tight fit.
  • Both doors 3 and 4 are provided with downwardly projecting brackets in which are adapted to slide spring pin latches Iii and H, respectively, which latch into apertures formed in a bracket 58, attached on the inside of the fuselage 1 near the edge of the doors opposite the hinges.
  • the swinging loop antenna construction comprises a housing iii having a rotatin head 2i at the bottom for rotating a swinging loop am tenna 22,
  • the swinging loop antenna is held in a mounting 23 which may be integrally formed with a shaft construction, indicated generally by the numeral 24, which is rotatable in the housing 20.
  • the shaft construction 24 is adapted to be rotated by means of the rotating head 2i.
  • the housing 29 is supported by means of a support arm 25, one end of which is pivoted at 23.
  • a gear sector 27 Integrally formed with the support arm 25 is a gear sector 27 which meshes with a worm 28 which is mounted in a bracket 25, attached to the inside of the fuselage i. To rotate the worm 23 I have provided a rotating handle it.
  • (see Figs. 2 and 4). This comprises on three sides an offset recess 32 which is adapted to engage the resilient strip I3 carried on the inside of the fuselage l adjacent the door opening.
  • On the other side the closure 3
  • the loop antenna 22 can be turned by means of the operating end or disk 2
  • the antenna By opening the door 4 and revolving the handle 30 in the proper direction the antenna may be swung downwardly in the position shown in Figure 2, in which case the door 3 is closed and held by means of the spring pin latch l6, and the door 4 is closed after having been opened to admit the antenna, this last door, as previously explained, being held by spring pin latch H.
  • the housing is strong and sturdy.
  • the surface of the fuselage is substantially unbroken (see Figure 2).
  • the drag is minimized by reason of the relatively smooth surface presented by the fuselage adjacent the point of egress of the loop antenna.
  • the loop antenna in the out position of course in itself presents a considerable drag, but after use it may be quickly and easily moved back into inoperative position.
  • a retractable antenna construction a housing, an antenna mounted therein, a base for the antenna, means to move the antenna to a point outside of the housing, said means being situated within the housing, two doors mounted in the housing, one through which the antenna proper is adapted to move and the other through which the base of the antenna is adapted to move, means to hold the first mentioned door closed when the antenna is outside of the housing, said second mentioned door remaining open until the antenna is withdrawn into the housing, resilient means between the doors and the housing to insure a tight fit, and a closure member associated with the antenna which closes the aperture left in the housing when the second mentioned door is open, said closure member being provided with a flanged edge which engages the resilient means, thereby aiding the closure member to tightly close the aperture left by the open door when the antenna is in a position outside the housing.
  • a retractable antenna construction a housing, an antenna mounted therein, a base for the antenna, means to move the antenna to a point outside of the housing, said means being situated within the housing, two doors mounted in the housing, one through which the antenna proper is adapted to move and the other through which the base of the antenna is adapted to move, means to hold the first mentioned door closed when the antenna is outside of the housing, a bracket for said door, said second mentioned door remaining open until the antenna is with drawn into the housing, resilient means between the doors and the housing to insure a tight fit, and a closure member associated with the antenna which closes the aperture left in the housing when the second mentioned door is open, three sides of said closure member being provided with a flanged edge which engages the resilient means, and the fourth side being provided with a resilient member which bears against the said door bracket, thereby aiding the closure member to tightly close the aperture left by the open door when the antenna is in a position outside the door.
  • a housing an antenna provided with a base, a casing in which the antenna is mounted, a support for said casing, a mount within the housing on which the support is pivotally mounted, means to transmit a swinging movement to the said support thereby causing an arcuate movement of the antenna to a point outside of the housing, two doors mounted in the housing, one through which the antenna proper is adapted to move and the other through which the means for supporting the antenna is adapted to move, means to hold the first mentioned door closed when the antenna is outside of the housing, said second mentioned door remaining open until the antenna is withdrawn into the housing, resilient means between the doors and the housing to insure a tight fit, and a closure member mounted on the casing which closes the aperture left in the housing when the second mentioned door is open, said closure member being provided with a flanged edge which engages the resilient means, thereby aiding the closure member to tightly close the aperture left by the open door when the antenna is in a position outside the housing.
  • a housing an antenna provided with a base, a casing in which the antenna is mounted, a support for said casing, a mount within the housing on which the support is pivotally mounted, means to transmit a swinging movement to the said support thereby causing an arcuate movement of the antenna to a point outside of the housing, two doors mounted in the housing, one through which the antenna proper is adapted to move and the other through which the means for supporting the antenna is adapted to move, means to hold the first mentioned door closed when the antenna is outside of the housing, a bracket for said door, said second mentioned door remaining open until the antenna is withdrawn into the housing, resilient means between the doors and the housing to insure a tight fit, and a closure member mounted on the casing which closes the aperture left in the housing when the second mentioned door is open, three sides of said closure member being provided with a flanged edge which engages the resilient means, and the fourth side being provided with a resilient member which bears against the said door bracket, thereby aiding the closure
  • a retractable antenna construction comprising a housing, an antenna provided with a base, a casing in which the base of the antenna is journalled for rotative movement, a support for said casing, a mount within the housing on which the support is pivotally mounted, means associated with said mount to transmit a swinging movement to the said support, thereby causing an arcuate movement of the antenna to a point outside of the housing, two doors mounted in the housing, one through which the antenna proper is adapted to move and the other through Which the means for supporting the antenna is adapted to move, means to hold the first mentioned door closed when the antenna is outside the housing, said second mentioned door remaining open until the antenna is withdrawn into the housing, resilient means between the doors and the housing to insure a tight fit, and a closure member mounted on the casing which closes the aperture left in the housing when the second mentioned door is open, said closure member being provided with a flanged edge which engages the resilient means, thereby aiding the closure member to tightly close the aperture left by the open door when the antenna is in a

Description

July 9, 1940.
H. L. BOWERS 2,207,084
RETRACTABLE ANTENNA .Filed Jan. 26, 1939 2 Sheets- Sheet l 23 Fg.1 l3 2 7 3| '5 I HERBERT L. BOWERS July 9, 1940. H. L. BowERs 2,207,084
RETRACTABLE ANTENNA Filed Jan. 26, 1939 2 Sheets-Sheet 2 HERBERT L. BOWERS Patented July 9, 1940 PATENT ()FFiCE RETRACTABLE ANTENNA Herbert L. Bowers, Kenmore, N. EL, assignor to Bell Aircraft Corporation, Buffalo, N. Y., a corporation of New York Application January 26, 1939, Serial No. 253,014
6 Glaims.
My invention relates to retractable antennae, and more particularly for retractable, antennae of the loop type, such as may be adapted for use in aircraft.
It is often desirable in aircrait to have an an tenna which is readily retractable. Particularly, loop antenna is useful in connection with radio, compass and direction finder arrangements. Here, where the loop antenna is projected beyond the confines of the fuselage of the airplane, it produces considerable drag, it therefore be= comes desirable to retract the loop antenna when it is not actually in use.
It is object of my invention to provide a retractable antenna which, when housed within the body of the fuselage, produces but little drag.
It is a further object of my invention to provide a construction which is strong and sturdy, and easy to repair and replace.
Yet another object of the invention is to pro vide a construction of loop antenna. which permits it to be positively and readily placed in onerative position. and rotated in any desired direction in that position.
A still further object of the invention is to provide an antenna which can be quickly brought into either operative or inoperative positions, and when in such positions, the surface of the fuse lage will be closed and flush.
With these and other objects in View, which may be incident to my improvements. the invention consists in the parts and combinations to be hereinafter set forth and claimed. with the understanding that the several necessary elements comprising my invention may be varied in construction, proportions and arrangements, without departing from the spirit and scope of the appended claims.
In order to make my invention more clearly understood, I have shown in the accompanying drawings means for carrying the same into practical effect without limiting the improvements in their useful applications to the particular constructicns which, for the purpose of explanation, have been made the subject of illustration.
In the drawings:
Figure l is a view partly in section showing my loop antenna in the out or operative position, one of the doors through which. it has been. swung being shown in the open position and the other door showing its open positions by dotted lines;
Fig. 2 is a sectional view showing my loop antenna housed within the fuselage;
Fig. 3 is a sectional view showing the position of the parts when the main door is closed;
'Fig. 4 is a sectional view showing the details of construction of the antenna mounting;
Fig. 5 is a bottom plan view of my construction with the doors closed. 5 Referring to the drawings I have shown an airplane fuselage i having an opening 2 therein. In this opening are hingedly mounted doors 3 and i on hinges 5 and 8, respectively, The hinges 5 and 5 have their plates 7 and B riveted to a downwardly projecting bracket 9. The other plates are attached to the doors 3 and l, respectively, as exemplified with respect to door 4, at
H, in Fig. 3.
Door carries, adjacent its periphery, an offset recess !2 formed therein. A resilient cushion i3 is attached to the inner surface of the fuselage adjacent the opening 2. This resilient cushion i3 is adapted to contact against the peripheral recess i2 and cause a tight fit. The outer surfaces of each of the doors 3 and i are adapted to follow the curve of the fuselage, as indicated in Figure 3. Door 3 has a similar oiiset recess l2 which is adapted, in the closed position, to v bear against the cushion It to make a tight fit. Both doors 3 and 4 are provided with downwardly projecting brackets in which are adapted to slide spring pin latches Iii and H, respectively, which latch into apertures formed in a bracket 58, attached on the inside of the fuselage 1 near the edge of the doors opposite the hinges.
The swinging loop antenna construction comprises a housing iii having a rotatin head 2i at the bottom for rotating a swinging loop am tenna 22, The swinging loop antenna is held in a mounting 23 which may be integrally formed with a shaft construction, indicated generally by the numeral 24, which is rotatable in the housing 20. The shaft construction 24 is adapted to be rotated by means of the rotating head 2i. The housing 29 is supported by means of a support arm 25, one end of which is pivoted at 23.
Integrally formed with the support arm 25 is a gear sector 27 which meshes with a worm 28 which is mounted in a bracket 25, attached to the inside of the fuselage i. To rotate the worm 23 I have provided a rotating handle it.
When both doors 3 and 4 are opened, by rotating the handle i l, the loop antenna may be swung out into the position Door 4 may then be shut and latched in position, door 3 remaining in the down position.
Mounted on the upper end of the casing is a closure 3| (see Figs. 2 and 4). This comprises on three sides an offset recess 32 which is adapted to engage the resilient strip I3 carried on the inside of the fuselage l adjacent the door opening. On the other side the closure 3| is provided with a resilient member 34 which is held clamped in position by means of a strip 36. This member 34 bears against the projecting side of a bracket 31, which is carried by the door 4.
Thus in the position shown in Figures 1 and 4 where the antenna is in out position, the door 4 is closed and held in place by the spring pin latches; the door 3 is in the down position but the closure means 3! causes a substantially leakproof fit around the aperture through which the loop antenna 22 projects.
In the position shown in Figures 1 and 4, the loop antenna 22 can be turned by means of the operating end or disk 2| into any desired position, yet the fuselage presents a relatively smooth surface to the air stream passing thereover.
By opening the door 4 and revolving the handle 30 in the proper direction the antenna may be swung downwardly in the position shown in Figure 2, in which case the door 3 is closed and held by means of the spring pin latch l6, and the door 4 is closed after having been opened to admit the antenna, this last door, as previously explained, being held by spring pin latch H.
The housing is strong and sturdy. When the antenna is within the fuselage the surface of the fuselage is substantially unbroken (see Figure 2). Even in the out position, as shown in Figures 1 and 4, the drag is minimized by reason of the relatively smooth surface presented by the fuselage adjacent the point of egress of the loop antenna. The loop antenna in the out position of course in itself presents a considerable drag, but after use it may be quickly and easily moved back into inoperative position.
While I have shown and described the preferred embodiment of my invention, I wish it to be understood that I do not confine myself to the precise details of construction herein set forth by way of illustration, as it is apparent that many changes and variations may be made therein, by those skilled in the art, without departing from the spirit of the invention, or exceeding the scope of the appended claims.
I claim:
1. In a retractable antenna construction, a housing, an antenna mounted therein, a base for the antenna, means to move the antenna to a point outside of the housing, said means being situated within the housing, two doors mounted in the housing, one through which the antenna proper is adapted to move and the other through which the base of the antenna is adapted to move, means to hold the first mentioned door closed when the antenna is outside of the housing, said second mentioned door remaining open until the antenna is withdrawn into the housing, resilient means between the doors and the housing to insure a tight fit, and a closure member associated with the antenna which closes the aperture left in the housing when the second mentioned door is open, said closure member being provided with a flanged edge which engages the resilient means, thereby aiding the closure member to tightly close the aperture left by the open door when the antenna is in a position outside the housing.
2. In a retractable antenna construction, a housing, an antenna mounted therein, a base for the antenna, means to move the antenna to a point outside of the housing, said means being situated within the housing, two doors mounted in the housing, one through which the antenna proper is adapted to move and the other through which the base of the antenna is adapted to move, means to hold the first mentioned door closed when the antenna is outside of the housing, a bracket for said door, said second mentioned door remaining open until the antenna is with drawn into the housing, resilient means between the doors and the housing to insure a tight fit, and a closure member associated with the antenna which closes the aperture left in the housing when the second mentioned door is open, three sides of said closure member being provided with a flanged edge which engages the resilient means, and the fourth side being provided with a resilient member which bears against the said door bracket, thereby aiding the closure member to tightly close the aperture left by the open door when the antenna is in a position outside the door.
3. In a retractable antenna construction, a housing, an antenna provided with a base, a casing in which the antenna is mounted, a support for said casing, a mount within the housing on which the support is pivotally mounted, means to transmit a swinging movement to the said support thereby causing an arcuate movement of the antenna to a point outside of the housing, two doors mounted in the housing, one through which the antenna proper is adapted to move and the other through which the means for supporting the antenna is adapted to move, means to hold the first mentioned door closed when the antenna is outside of the housing, said second mentioned door remaining open until the antenna is withdrawn into the housing, resilient means between the doors and the housing to insure a tight fit, and a closure member mounted on the casing which closes the aperture left in the housing when the second mentioned door is open, said closure member being provided with a flanged edge which engages the resilient means, thereby aiding the closure member to tightly close the aperture left by the open door when the antenna is in a position outside the housing.
4. In a retractable antenna construction, a housing, an antenna provided with a base, a casing in which the antenna is mounted, a support for said casing, a mount within the housing on which the support is pivotally mounted, means to transmit a swinging movement to the said support thereby causing an arcuate movement of the antenna to a point outside of the housing, two doors mounted in the housing, one through which the antenna proper is adapted to move and the other through which the means for supporting the antenna is adapted to move, means to hold the first mentioned door closed when the antenna is outside of the housing, a bracket for said door, said second mentioned door remaining open until the antenna is withdrawn into the housing, resilient means between the doors and the housing to insure a tight fit, and a closure member mounted on the casing which closes the aperture left in the housing when the second mentioned door is open, three sides of said closure member being provided with a flanged edge which engages the resilient means, and the fourth side being provided with a resilient member which bears against the said door bracket, thereby aiding the closure member to tightly close the aperture left by the open door when the antenna is in a position outside the door.
5. A retractable antenna construction comprising a housing, an antenna provided with a base, a casing in which the base of the antenna is journalled for rotative movement, a support for said casing, a mount within the housing on which the support is pivotally mounted, means associated with said mount to transmit a swinging movement to the said support, thereby causing an arcuate movement of the antenna to a point outside of the housing, two doors mounted in the housing, one through which the antenna proper is adapted to move and the other through Which the means for supporting the antenna is adapted to move, means to hold the first mentioned door closed when the antenna is outside the housing, said second mentioned door remaining open until the antenna is withdrawn into the housing, resilient means between the doors and the housing to insure a tight fit, and a closure member mounted on the casing which closes the aperture left in the housing when the second mentioned door is open, said closure member being provided with a flanged edge which engages the resilient means, thereby aiding the closure member to tightly close the aperture left by the open door when the antenna is in a position out-.
side the housing.
6. A retractable antenna construction comprising a housing, an antenna provided with a base, a casing in which the base of the antenna is journalled for rotative movement, a support for said casing, a mount within the housing on which the support is pivotally mounted, means associated with said mount to transmit a swinging movement to the said support, thereby causing an arcuate movement of the antenna to a point outside of the housing, two doors mounted in the housing, one through which the antenna proper is adapted to move and the other through which the means for supporting the antenna is adapted to move, means to hold the first mentioned door closed when the antenna is outside the housing, a bracket for said door, said second mentioned door remaining open until the antenna is withdrawn into the housing, resilient means between the doors and the housing to insure a tight fit, and a closure member mounted on the casing which closes the aperture left in the housing when the second mentioned door is open, three sides of said closure member being provided with a flanged edge which engages the resilient means, and the fourth side being provided with a resilient member which bears against the said door bracket, thereby aiding the closure member to tightly close the aperture left by the open door when the antenna is in a position outside the door.
HERBERT L. BOWERS.
US253014A 1939-01-26 1939-01-26 Retractable antenna Expired - Lifetime US2207084A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2969543A (en) * 1957-03-29 1961-01-24 Warwick Mfg Corp Antenna for a signal-receiving device
US3602088A (en) * 1968-04-03 1971-08-31 Contraves Ag Armored tank vehicle with antiaircraft armament
WO2008119144A3 (en) * 2007-04-02 2010-02-04 EMBRAER-Empresa Brasileira de Aeronáutica S.A. Retractable system for aeronautical sensors
US20130263514A1 (en) * 2012-04-09 2013-10-10 John Parsley Multi-Purpose Hatch System

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2969543A (en) * 1957-03-29 1961-01-24 Warwick Mfg Corp Antenna for a signal-receiving device
US3602088A (en) * 1968-04-03 1971-08-31 Contraves Ag Armored tank vehicle with antiaircraft armament
WO2008119144A3 (en) * 2007-04-02 2010-02-04 EMBRAER-Empresa Brasileira de Aeronáutica S.A. Retractable system for aeronautical sensors
US20100219295A1 (en) * 2007-04-02 2010-09-02 Mario Sergio Dias Ferraz Retractable system for aeronautical sensors
US8453968B2 (en) 2007-04-02 2013-06-04 Embraer S.A. System for retracting and extending airborne sensors
US20130263514A1 (en) * 2012-04-09 2013-10-10 John Parsley Multi-Purpose Hatch System
US9016631B2 (en) * 2012-04-09 2015-04-28 R4 Integration, Inc. Multi-purpose hatch system

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