GB868390A - Improvements in doors for pressurized fuselages of aircraft - Google Patents
Improvements in doors for pressurized fuselages of aircraftInfo
- Publication number
- GB868390A GB868390A GB2152358A GB2152358A GB868390A GB 868390 A GB868390 A GB 868390A GB 2152358 A GB2152358 A GB 2152358A GB 2152358 A GB2152358 A GB 2152358A GB 868390 A GB868390 A GB 868390A
- Authority
- GB
- United Kingdom
- Prior art keywords
- door
- lugs
- frame
- cabin
- hinge
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
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
- B64C1/1423—Passenger doors
- B64C1/143—Passenger doors of the plug type
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Hinge Accessories (AREA)
- Lock And Its Accessories (AREA)
Abstract
868,390. Closures for resisting fluid pressure. VICKERS AIRCRAFT HOLDINGS Ltd. June 9, 1959 [July 4, 1958], No. 21523/58. Class 123(1) [Also in Groups XXV and XXXIII] The door and door frame of a pressurised aircraft cabin are each provided about its periphery with a set of spaced lugs, the arrangement of the lugs being such that when the door is closed and the cabin pressurised the lugs on the door abut their outward faces against the inward faces of the lugs on the door frame to positively resist outward pressure on the door, means being provided, operable from within the cabin, whereby after decompression thereof, the door can be raised with respect to the frame to disengage the abutting faces of the opposed lugs, the door lugs being moved to positions intermediate the frame lugs, permitting the door to be opened. The door 10 fits within a frame 11 upon a main hinge 13 so constructed that, under the restraint of a pivoted tie member 26, the door in opening moves bodily outwards from the cabin. The door is connected to hinge 13 through a parallel linkage 21 which permits vertical movement of the door when an operating handle 18 projects spring loaded feet 19 in the base of the door into contact with a sill member 111. During such vertical movement the door is guided at its upper end by spigots 23 which engage slotted plates on the door frame. The door is provided on its peripheral edges with lugs 14 which, when the door is closed, cooperate as shown with matching lugs 15 on the door frame whereby pressure loads on the door are reacted directly by the frame and not the hinge and latching mechanism. The final latching movement causes locking spigots 16 in the door to project into holes in the door frame. Initial movement of handle 18 withdraws such latches and then causes feet 19 to project on to the sill and raise the door to a position in which lugs 14 can pass between lugs 15 when the door is opened. A conventional pressure seal is provided.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2152358A GB868390A (en) | 1958-07-04 | 1958-07-04 | Improvements in doors for pressurized fuselages of aircraft |
| NL240698A NL109892C (en) | 1958-07-04 | 1959-06-29 | |
| ES0250454A ES250454A1 (en) | 1958-07-04 | 1959-07-01 | Improvements in doors for pressurized fuselages of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2152358A GB868390A (en) | 1958-07-04 | 1958-07-04 | Improvements in doors for pressurized fuselages of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB868390A true GB868390A (en) | 1961-05-17 |
Family
ID=10164362
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2152358A Expired GB868390A (en) | 1958-07-04 | 1958-07-04 | Improvements in doors for pressurized fuselages of aircraft |
Country Status (3)
| Country | Link |
|---|---|
| ES (1) | ES250454A1 (en) |
| GB (1) | GB868390A (en) |
| NL (1) | NL109892C (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3164956A (en) * | 1963-03-14 | 1965-01-12 | Boeing Co | Two part thrust reverser |
| EP1550773A2 (en) * | 2003-12-30 | 2005-07-06 | Karl Miller GmbH | Cabin for use with a crane or excavator |
| WO2010001210A2 (en) * | 2008-07-01 | 2010-01-07 | Eurocopter Deutschland Gmbh | Aircraft door with supporting control arm arrangement |
| WO2015109352A1 (en) * | 2014-01-21 | 2015-07-30 | Facc Ag | Device for opening an aircraft door |
| EP2554473A3 (en) * | 2011-08-05 | 2017-06-28 | Airbus Operations GmbH | Carrier arm arrangement, door and transport means |
| EP3219603A1 (en) * | 2016-03-16 | 2017-09-20 | Dassault Aviation | Connecting mechanism between an aircraft door and a structure of the aircraft, related aircraft and method |
| EP3476715A1 (en) * | 2017-10-26 | 2019-05-01 | Pa.Cotte Sa | Mechanism for opening/closing a door leaf relative to a frame |
| EP3620369A1 (en) * | 2018-09-06 | 2020-03-11 | Airbus Operations SAS | Improved door system for aircraft fuselage |
| CN113148223A (en) * | 2021-05-06 | 2021-07-23 | 中航飞机起落架有限责任公司 | Installation method for pretightening force of lock belt of aircraft cabin door |
| EP4335742A1 (en) * | 2022-09-09 | 2024-03-13 | Airbus Operations (Sas) | Aircraft fuselage door comprising an inner panel and an outer panel, and aircraft fuselage part comprising such a door |
-
1958
- 1958-07-04 GB GB2152358A patent/GB868390A/en not_active Expired
-
1959
- 1959-06-29 NL NL240698A patent/NL109892C/xx active
- 1959-07-01 ES ES0250454A patent/ES250454A1/en not_active Expired
Cited By (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3164956A (en) * | 1963-03-14 | 1965-01-12 | Boeing Co | Two part thrust reverser |
| EP1550773A2 (en) * | 2003-12-30 | 2005-07-06 | Karl Miller GmbH | Cabin for use with a crane or excavator |
| EP1550773A3 (en) * | 2003-12-30 | 2005-10-12 | Karl Miller GmbH | Cabin for use with a crane or excavator |
| WO2010001210A2 (en) * | 2008-07-01 | 2010-01-07 | Eurocopter Deutschland Gmbh | Aircraft door with supporting control arm arrangement |
| WO2010001210A3 (en) * | 2008-07-01 | 2010-04-08 | Eurocopter Deutschland Gmbh | Aircraft door with supporting control arm arrangement |
| EP2554473A3 (en) * | 2011-08-05 | 2017-06-28 | Airbus Operations GmbH | Carrier arm arrangement, door and transport means |
| CN105980247A (en) * | 2014-01-21 | 2016-09-28 | Facc股份公司 | Device for opening an aircraft door |
| US9630700B2 (en) | 2014-01-21 | 2017-04-25 | Facc Ag | Device for opening an aircraft door |
| WO2015109352A1 (en) * | 2014-01-21 | 2015-07-30 | Facc Ag | Device for opening an aircraft door |
| US10577072B2 (en) | 2016-03-16 | 2020-03-03 | Dassault Aviation | Connecting mechanism between an aircraft door and a structure of the aircraft, related aircraft and method |
| FR3048952A1 (en) * | 2016-03-16 | 2017-09-22 | Dassault Aviat | CONNECTING MECHANISM BETWEEN AN AIRCRAFT DOOR AND AN AIRCRAFT STRUCTURE, AIRCRAFT AND ASSOCIATED METHOD |
| EP3219603A1 (en) * | 2016-03-16 | 2017-09-20 | Dassault Aviation | Connecting mechanism between an aircraft door and a structure of the aircraft, related aircraft and method |
| EP3476715A1 (en) * | 2017-10-26 | 2019-05-01 | Pa.Cotte Sa | Mechanism for opening/closing a door leaf relative to a frame |
| EP3620369A1 (en) * | 2018-09-06 | 2020-03-11 | Airbus Operations SAS | Improved door system for aircraft fuselage |
| FR3085664A1 (en) * | 2018-09-06 | 2020-03-13 | Airbus Operations | IMPROVED DOOR SYSTEM FOR AIRCRAFT FUSELAGE |
| US11548611B2 (en) | 2018-09-06 | 2023-01-10 | Airbus Operations Sas | Door system for aircraft fuselage |
| CN113148223A (en) * | 2021-05-06 | 2021-07-23 | 中航飞机起落架有限责任公司 | Installation method for pretightening force of lock belt of aircraft cabin door |
| CN113148223B (en) * | 2021-05-06 | 2023-11-28 | 中航飞机起落架有限责任公司 | Installation method for door lock belt pretightening force of aircraft cabin |
| EP4335742A1 (en) * | 2022-09-09 | 2024-03-13 | Airbus Operations (Sas) | Aircraft fuselage door comprising an inner panel and an outer panel, and aircraft fuselage part comprising such a door |
Also Published As
| Publication number | Publication date |
|---|---|
| ES250454A1 (en) | 1959-12-16 |
| NL109892C (en) | 1964-11-16 |
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