WO2005083647A1 - Improvements in aircraft doors - Google Patents
Improvements in aircraft doors Download PDFInfo
- Publication number
- WO2005083647A1 WO2005083647A1 PCT/GB2005/000607 GB2005000607W WO2005083647A1 WO 2005083647 A1 WO2005083647 A1 WO 2005083647A1 GB 2005000607 W GB2005000607 W GB 2005000607W WO 2005083647 A1 WO2005083647 A1 WO 2005083647A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- alarm system
- sensor
- alarm
- door
- arming
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
- B64C1/1407—Doors; surrounding frames
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- E05B41/00—Locks with visible indication as to whether the lock is locked or unlocked
Definitions
- This invention relates to aircraft doors of the type typically used on passenger transport aircraft, in particular the invention relates to an alarm system for alerting cabin crew when a door is "armed”.
- Doors of passenger transport aircraft are commonly fitted with inflatable slides to assist passenger evacuation in an emergency situation.
- Slides are typically stored in a bustle within the aircraft door. Such slides may be detachable from the aircraft to be used as life rafts.
- Prior to take off of an aircraft it is usual to "arm" the doors. This means a door is configured such that if it is opened, the emergency evacuation slide is released from the bustle. On release of the slide, gravity causes discharge of an associated gas pressurised cylinder which inflates the slide.
- a door might include a light which displays in one colour when the door is armed and a different colour when the door is unarmed.
- a door might include a slidable or rotatable handle which can be moved between a position marked "ARMED” and a position marked “DISARMED” and/or a slide placard which displays when the door is armed and is hidden when the door is not armed.
- the inventors have recognised that in some circumstances a person might not register the indicator prior to acting to open the door.
- the visual indicator may become obscured by another body, or a cabin crew member may be distracted when approaching the door and forget to check its status.
- a cabin crew member operating on an aircraft of a type they have not previously encountered may misinterpret a visual indicator assuming a door to be disarmed when it is, in fact, armed.
- the present invention provides an alarm system for an aircraft door comprising; a sensor for sensing when the door operating handle is about to be gripped by an operator, an aural alarm associated with the sensor and operable to sound when the sensor detects that the handle is about to be gripped, means for arming the sensor and/or aural alarm when the aircraft door is armed.
- the sensor may be a contactless type or alternatively may be a pressure sensor.
- the term "about to be gripped” covers a situation where the sensor senses the hand of an operator prior to the handle being touched and a situation where the sensor senses pressure on the handle at the point where the handle is first touched.
- the system may be incorporated into an operating handle for the door or may be retrofittable to an existing door handle.
- the sensor may comprise a pressure sensor located on or in the handle which sensor responds to hand pressure of an operator gripping the handle.
- a sensor could be light, heat, humidity or chemically sensitive responding to contact with a characteristic of an operators hand.
- the aural alarm is desirably electrically operated.
- the sound made by the alarm may be one or more tones, optionally a repeating sequence of tones.
- the alarm may broadcast a pre-recorded voice message indicating that the door is armed.
- the means for arming the sensor and/or aural alarm may be manual or automatic. Desirably, arming is automatically effected when the door is armed.
- the arming means may be mechanically, electrically, optically or magnetically coupled to an existing means for arming the door or an existing visual indicator for indicating the status of the door.
- the arming means may include a sensor which is activated following a change in the status of the door.
- the sensor may be a light sensor obscurable by an operating switch or handle for arming the door when the position of the switch or handle is changed.
- the arming means may include a magnetically sensitive switch such as a Reed switch which is responsive to a magnetic field which changes when a door is switched between an armed and an unarmed configuration.
- the alarm system may include its own power source, for example but not strictly limited to a dry cell.
- the alarm system may tap power from an existing power source used to power the door and/or aircraft.
- the alarm system includes its own indicator that it has been armed.
- an indicator may, for example, be a light emitting diode which lights or pulses when the system is armed.
- the system may be completely hard wired or may use one or more wireless connections between various of its components and/or existing components of the aircraft door. For example, there may be a blue tooth link between the sensor and alarm or between the means for activating the sensor and the sensor.
- the invention comprises a handle for an aircraft door incorporating the previously described alarm system.
- the invention comprises an aircraft door equipped with an alarm system as previously described.
- an alarm system as previously described.
- Figure 1 illustrates the front face of an aircraft door as is known in the prior art.
- Figure 2 illustrates a handle for an aircraft door incorporating an embodiment of the alarm system of the invention.
- Figure 3 illustrates a circuit diagram for an embodiment of an alarm system in accordance with the invention.
- a typical aircraft door 1 (in this case a door used on a Boeing 757 aircraft) includes a viewing window 2, an operating handle 3 for opening and locking the door 1 and a door mode select panel 4a, 4b for arming and disarming the door 1.
- a bustle 5 At the bottom of the door 1 is a bustle 5 in which an emergency evacuation slide (not shown) is stowed.
- a container of pressurised gas for inflating the slide in the event of an emergency.
- a pressure gauge 6 displays the pressure of the gas on the front of the door 1.
- a pair of handles 7 are provided towards the top and right of the door 1 which an operator can use to manoeuvre the door 1.
- the door mode select panel 4a, 4b comprises an operating switch 4a and a position indicator 4b.
- the position indicator 4b illustrates the direction in which the switch 4a need be switched to respectively arm and disarm the door 1.
- a slide placard 8 Just above the operating handle 3 is a slide placard 8.
- the slide placard When the door 1 is disarmed, the slide placard is retained in the body of the door 1, flush with the surface of the door 1.
- the switch 4a When the door 1 is armed by appropriate operation of the switch 4a, the slide placard is caused to pop out of the door and display an indicator that the door is armed.
- At the top of the door 1 is an LED 9 which is lit when the door 1 is armed and not lit when the door 1 is disarmed.
- LED 9 which is lit when the door 1 is armed and not lit when the door 1 is disarmed.
- FIG. 2 shows the reverse side of a door operating handle 20 similar to that referenced 3 in Figure 1.
- the handle has a substantially C shaped cross section made up of walls 21a, 21b and the front surface (not shown) of the handle 20.
- a taller walled section 21b is provided at one end of the handle to allow attachment to the front of a door whilst providing a clearance around the remainder of the handle 20 so that it may be gripped.
- an alarm system in accordance with the invention, 22, 23, 24, 25.
- Extending across a central portion of the handle is a pressure sensitive pad 22 enclosing an electrical circuit supplying the alarm system.
- Adjacent the pressure sensitive pad is an arming device 23 which is responsive to arming of an aircraft door to which the handle 20 is attached to arm the alarm system 22, 23, 24, 25.
- Adjacent the arming device 23 is a speaker 24 of an alarm sounder.
- the system is powered by a battery pack enclosed in a container 25.
- Figure 3 shows a circuit diagram for an alarm system substantially similar to the embodiment illustrated in Figure 2.
- the circuit comprises a 9v dry power cell 31 which powers pressure sensor 37.
- the system is armed through arming device 32, 38 which comprises a Reed switch 32 and ceramic magnet 38.
- the ceramic magnet 38 is associated with a slide placard of an aircraft door, the Reed switch being positioned, in use, in close proximity to the placard and magnet 38.
- the slide placard pops out and the magnetic field near the magnetically sensitive Reed switch 32 is magnified. The change in the field is such as to cause the switch 32 to close.
- the alarm system circuit is now armed. Once the system is armed but not activated (i.e. there is no detection of pressure by sensor 37) a battery saver circuit 33 pulses a low current supply to LED 34 which emits an intermittent light, this provides a visual indicator that the system is armed and in a "stand by" mode.
- a latch circuit 36 is closed and the latch circuit 36 grabs power from the cell 31.
- the active latch circuit 36 triggers the broadcast of a timed, audible alarm, for example a pre-recorded voice message, through speaker/amplifier circuit 35.
- the senor is incorporated into an operating handle for the door.
- the electronic circuitry providing communication between the sensor and the arming means and aural alarm are located or are incorporated into the door structure.
- the senor is incorporated into, or located on, the door structure preferably just behind the handle.
- the sensor is close enough to the handle to sense when the handle is, or is about to be, touched by an operator.
Abstract
Description
Claims
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/590,890 US8121438B2 (en) | 2004-02-27 | 2005-02-12 | Aircraft doors |
DE602005006752T DE602005006752D1 (en) | 2004-02-27 | 2005-02-21 | IMPROVEMENTS ON PLANE DOORS |
CA2557512A CA2557512C (en) | 2004-02-27 | 2005-02-21 | Improvements in aircraft doors |
EP05717752A EP1719084B1 (en) | 2004-02-27 | 2005-02-21 | Improvements in aircraft doors |
AT05717752T ATE495514T1 (en) | 2004-02-27 | 2005-02-21 | IMPROVEMENTS TO AIRCRAFT DOORS |
BRPI0508042-8A BRPI0508042A (en) | 2004-02-27 | 2005-02-21 | alarm system and operating handle for an aircraft door, and, aircraft door |
JP2007500279A JP4589378B2 (en) | 2004-02-27 | 2005-02-21 | Aircraft door improvements |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0404328.7 | 2004-02-27 | ||
GB0404328A GB2416616A (en) | 2004-02-27 | 2004-02-27 | Aircraft door handle alarm |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2005083647A1 true WO2005083647A1 (en) | 2005-09-09 |
WO2005083647A8 WO2005083647A8 (en) | 2007-04-19 |
Family
ID=32050940
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/GB2005/000607 WO2005083647A1 (en) | 2004-02-27 | 2005-02-21 | Improvements in aircraft doors |
Country Status (12)
Country | Link |
---|---|
US (1) | US8121438B2 (en) |
EP (1) | EP1719084B1 (en) |
JP (1) | JP4589378B2 (en) |
CN (1) | CN100543789C (en) |
AT (1) | ATE495514T1 (en) |
BR (1) | BRPI0508042A (en) |
CA (1) | CA2557512C (en) |
DE (1) | DE602005006752D1 (en) |
ES (1) | ES2358909T3 (en) |
GB (1) | GB2416616A (en) |
RU (1) | RU2383930C2 (en) |
WO (1) | WO2005083647A1 (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102005060425A1 (en) * | 2005-12-15 | 2007-06-21 | Primion Technology Ag | Door operating system e.g. for opening door via electronic reading device, has electronic data recognition unit and unit which is intended for expenditure of dynamic signal |
EP2108585B2 (en) † | 2008-04-07 | 2015-02-11 | Airbus Operations GmbH | System and method for prevention of inadvertent escape slide deployment for an aircraft |
EP2679502A3 (en) * | 2012-06-26 | 2017-07-19 | The Boeing Company | Directionally filtered indicator light |
WO2017174119A1 (en) * | 2016-04-05 | 2017-10-12 | Airbus Operations Gmbh | Retrofittable display device for displaying an activation status of an emergency chute in an aircraft |
US9870691B2 (en) | 2014-07-18 | 2018-01-16 | Airbus Operations Gmbh | Apparatus for operating a door of an aircraft, an aircraft having such an apparatus and method for operating a door of an aircraft |
IT201600101548A1 (en) * | 2016-10-12 | 2018-04-12 | Romualdo Cozza | Warning signaling and activation device and remember for everyday objects such as keys and wallet |
RU184400U1 (en) * | 2018-06-19 | 2018-10-24 | Акционерное общество "ЦентрИнформ" | ELECTRONIC RADIO FREQUENCY FILLING |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2416616A (en) * | 2004-02-27 | 2006-02-01 | Christopher Yardley | Aircraft door handle alarm |
GB2425638B (en) * | 2005-04-28 | 2010-06-30 | Christopher Yardley | Aircraft door handle alarm system |
US9809313B2 (en) | 2007-01-22 | 2017-11-07 | Honeywell International Inc. | Cabin altitude alerting systems and methods |
DE102011086454A1 (en) | 2011-11-16 | 2013-05-16 | Airbus Operations Gmbh | Monitoring device and method for monitoring a movement profile of a user in the area of an actuating element of an aircraft or spacecraft |
EP2878530B1 (en) * | 2013-11-27 | 2019-02-27 | Airbus Operations GmbH | Warning circuitry and warning device for an aircraft |
GB2524847A (en) * | 2014-04-06 | 2015-10-07 | Peter John Charles Spurgeon | A door entry device |
DE102015100880A1 (en) * | 2015-01-21 | 2016-07-21 | Airbus Operations Gmbh | Retrofittable display device for indicating an activation status of an escape slide in an aircraft |
DE102019107823B4 (en) | 2019-03-27 | 2021-12-23 | Airbus Operations Gmbh | Cabin door system for an aircraft and an aircraft with at least one such cabin door system |
US11745880B2 (en) | 2020-01-17 | 2023-09-05 | Goodrich Corporation | Readiness indicator lights for evacuation slide |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
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US3824576A (en) | 1972-08-16 | 1974-07-16 | R Pioch | Alarm system activated by touch sensitive door knob intrusior |
GB2066536A (en) * | 1979-01-04 | 1981-07-08 | Bajius T | Alarm Device |
DE19943040A1 (en) * | 1999-09-09 | 2001-03-15 | Geze Gmbh | Building exit device has one or more components, e.g. monitor and alarm, mounted in free-standing housing at distance from door or window |
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GB2416616A (en) * | 2004-02-27 | 2006-02-01 | Christopher Yardley | Aircraft door handle alarm |
-
2004
- 2004-02-27 GB GB0404328A patent/GB2416616A/en not_active Withdrawn
-
2005
- 2005-02-12 CN CNB2005800110937A patent/CN100543789C/en not_active Expired - Fee Related
- 2005-02-12 US US10/590,890 patent/US8121438B2/en not_active Expired - Fee Related
- 2005-02-21 EP EP05717752A patent/EP1719084B1/en active Active
- 2005-02-21 DE DE602005006752T patent/DE602005006752D1/en active Active
- 2005-02-21 JP JP2007500279A patent/JP4589378B2/en not_active Expired - Fee Related
- 2005-02-21 RU RU2006134278/09A patent/RU2383930C2/en not_active IP Right Cessation
- 2005-02-21 ES ES05717752T patent/ES2358909T3/en active Active
- 2005-02-21 AT AT05717752T patent/ATE495514T1/en not_active IP Right Cessation
- 2005-02-21 WO PCT/GB2005/000607 patent/WO2005083647A1/en active Application Filing
- 2005-02-21 BR BRPI0508042-8A patent/BRPI0508042A/en not_active IP Right Cessation
- 2005-02-21 CA CA2557512A patent/CA2557512C/en not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3824576A (en) | 1972-08-16 | 1974-07-16 | R Pioch | Alarm system activated by touch sensitive door knob intrusior |
GB2066536A (en) * | 1979-01-04 | 1981-07-08 | Bajius T | Alarm Device |
DE19943040A1 (en) * | 1999-09-09 | 2001-03-15 | Geze Gmbh | Building exit device has one or more components, e.g. monitor and alarm, mounted in free-standing housing at distance from door or window |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102005060425A1 (en) * | 2005-12-15 | 2007-06-21 | Primion Technology Ag | Door operating system e.g. for opening door via electronic reading device, has electronic data recognition unit and unit which is intended for expenditure of dynamic signal |
DE102005060425B4 (en) * | 2005-12-15 | 2013-03-28 | Primion Technology Ag | Door actuator |
EP2108585B2 (en) † | 2008-04-07 | 2015-02-11 | Airbus Operations GmbH | System and method for prevention of inadvertent escape slide deployment for an aircraft |
US9789970B2 (en) | 2008-04-07 | 2017-10-17 | Airbus Operations Gmbh | System and method for prevention of inadvertent escape slide deployment for an aircraft |
EP2679502A3 (en) * | 2012-06-26 | 2017-07-19 | The Boeing Company | Directionally filtered indicator light |
US9870691B2 (en) | 2014-07-18 | 2018-01-16 | Airbus Operations Gmbh | Apparatus for operating a door of an aircraft, an aircraft having such an apparatus and method for operating a door of an aircraft |
WO2017174119A1 (en) * | 2016-04-05 | 2017-10-12 | Airbus Operations Gmbh | Retrofittable display device for displaying an activation status of an emergency chute in an aircraft |
US10822115B2 (en) | 2016-04-05 | 2020-11-03 | Airbus Operations Gmbh | Retrofittable display device for displaying an activation status of an emergency chute in an aircraft |
IT201600101548A1 (en) * | 2016-10-12 | 2018-04-12 | Romualdo Cozza | Warning signaling and activation device and remember for everyday objects such as keys and wallet |
RU184400U1 (en) * | 2018-06-19 | 2018-10-24 | Акционерное общество "ЦентрИнформ" | ELECTRONIC RADIO FREQUENCY FILLING |
RU184400U9 (en) * | 2018-06-19 | 2018-12-07 | Акционерное общество "ЦентрИнформ" | ELECTRONIC RADIO FREQUENCY SEAL |
Also Published As
Publication number | Publication date |
---|---|
US20080284619A1 (en) | 2008-11-20 |
ATE495514T1 (en) | 2011-01-15 |
GB0404328D0 (en) | 2004-03-31 |
CA2557512C (en) | 2014-01-21 |
CN1942907A (en) | 2007-04-04 |
JP4589378B2 (en) | 2010-12-01 |
US8121438B2 (en) | 2012-02-21 |
EP1719084B1 (en) | 2011-01-12 |
CN100543789C (en) | 2009-09-23 |
DE602005006752D1 (en) | 2011-05-05 |
JP2007524546A (en) | 2007-08-30 |
RU2383930C2 (en) | 2010-03-10 |
ES2358909T3 (en) | 2011-05-16 |
CA2557512A1 (en) | 2005-09-09 |
BRPI0508042A (en) | 2007-07-17 |
EP1719084A1 (en) | 2006-11-08 |
RU2006134278A (en) | 2008-04-20 |
WO2005083647A8 (en) | 2007-04-19 |
GB2416616A (en) | 2006-02-01 |
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