GB1175097A - Retractable Undercarriage for Aircraft - Google Patents
Retractable Undercarriage for AircraftInfo
- Publication number
- GB1175097A GB1175097A GB2866967A GB2866967A GB1175097A GB 1175097 A GB1175097 A GB 1175097A GB 2866967 A GB2866967 A GB 2866967A GB 2866967 A GB2866967 A GB 2866967A GB 1175097 A GB1175097 A GB 1175097A
- Authority
- GB
- United Kingdom
- Prior art keywords
- latch
- undercarriage
- pin
- aircraft
- cam
- 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
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/18—Operating mechanisms
- B64C25/26—Control or locking systems therefor
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
Abstract
1,175,097. Aircraft undercarriages. ELECTRO-HYDRAULICS Ltd. 18 June, 1968 [21 June, 1967], No. 28669/67. Heading B7G. [Also in Division E2] An aircraft retractable undercarriage comprises a latch 12, pivotally connected to the aircraft at 13, which engages a locking pin 4 located on a lug 5 on a leg member 1. A cam follower 15 on the latch 12 has a clearance from the upper surface 20 of a cam 3 so that deflections of the undercarriage due to ground manoeuvres will not cause the latch to be unlocked. The undercarriage is retracted by extending the jack 7; when this is done piston rod 6 cannot move since pin 4 is locked by the latch 12. Accordingly the cylinder 8 moves to the right as permitted by a pin and slot lost motion connection 10,11, and link 16 also moves to the right releasing latch 12 from the pin 4 whereupon the piston rod 6 pivots the member 1 about pivot 2. The profile 22 of the cam 3 passes under the cam follower 15, eliminating the lost motion during the retraction operation. The undercarriage is lowered by closing the jack, the locking occurring at the end of lowering when the cam follower 15 leaves the profile 22. In another embodiment locking is aided by a compression spring 17 which urges the latch 12 into the locked position. The device may be adapted for use as an up lock.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2866967A GB1175097A (en) | 1967-06-21 | 1967-06-21 | Retractable Undercarriage for Aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2866967A GB1175097A (en) | 1967-06-21 | 1967-06-21 | Retractable Undercarriage for Aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1175097A true GB1175097A (en) | 1969-12-23 |
Family
ID=10279264
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2866967A Expired GB1175097A (en) | 1967-06-21 | 1967-06-21 | Retractable Undercarriage for Aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1175097A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8770514B2 (en) | 2005-06-03 | 2014-07-08 | Airbus Operations Limited | Landing gear |
US10457383B2 (en) | 2016-01-19 | 2019-10-29 | Safran Landing Systems Uk Ltd | Aircraft landing gear assembly |
US10569863B2 (en) | 2013-09-10 | 2020-02-25 | Safran Landing Systems Uk Ltd | Lock and aircraft landing gear assembly |
-
1967
- 1967-06-21 GB GB2866967A patent/GB1175097A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8770514B2 (en) | 2005-06-03 | 2014-07-08 | Airbus Operations Limited | Landing gear |
US10569863B2 (en) | 2013-09-10 | 2020-02-25 | Safran Landing Systems Uk Ltd | Lock and aircraft landing gear assembly |
US11242137B2 (en) | 2013-09-10 | 2022-02-08 | Safran Landing Systems Uk Ltd | Lock and aircraft landing gear assembly |
US10457383B2 (en) | 2016-01-19 | 2019-10-29 | Safran Landing Systems Uk Ltd | Aircraft landing gear assembly |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PLNP | Patent lapsed through nonpayment of renewal fees |