GB984775A - Improvements in or relating to retractable undercarriages for aircraft - Google Patents
Improvements in or relating to retractable undercarriages for aircraftInfo
- Publication number
- GB984775A GB984775A GB454762A GB454762A GB984775A GB 984775 A GB984775 A GB 984775A GB 454762 A GB454762 A GB 454762A GB 454762 A GB454762 A GB 454762A GB 984775 A GB984775 A GB 984775A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pivoted
- aircraft
- airframe
- undercarriage
- relating
- 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
- B64C25/14—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like fore-and-aft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vehicle Body Suspensions (AREA)
Abstract
984,775. Aircraft undercarriages. SOC. HISPANO-SUIZA-LALLEMANT. Feb. 6, 1962 [Aug. 8, 1961], No. 4547/62. Headings B7G and B7W. An aircraft undercarriage comprises a shock absorber 2 pivoted at A to the wheel (or pair of wheels) support 5 and at B to a connecting member 4 pivoted at C to the airframe, the pivots A, B and C being in substantially vertical alignment when the undercarriage is down, as in Fig. 1, and a fluid retraction jack 8 pivoted at H to the airframe and at I to member 4, a link 7 extending between a pivot G on member 4 and a pivot F on a rod 6 having one end pivoted to the airframe at E and the other end pivoted to the wheel support 5 at D. A down lock and a pilot's " undercarriage down " indicator are provided.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR870329A FR1304121A (en) | 1961-08-08 | 1961-08-08 | Improvements to retractable landing gears for aerodynes, in particular for high-wing aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB984775A true GB984775A (en) | 1965-03-03 |
Family
ID=8760929
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB454762A Expired GB984775A (en) | 1961-08-08 | 1962-02-06 | Improvements in or relating to retractable undercarriages for aircraft |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR1304121A (en) |
GB (1) | GB984775A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4272366A (en) * | 1979-08-16 | 1981-06-09 | Fmc Corporation | Heavy duty two mass vibratory machine |
WO2005028304A2 (en) * | 2003-08-15 | 2005-03-31 | The Boeing Company | Airplane landing gear |
EP3366579A1 (en) * | 2017-02-28 | 2018-08-29 | The Boeing Company | Aircraft landing gear, aircraft, and related methods |
EP3366578A1 (en) * | 2017-02-28 | 2018-08-29 | The Boeing Company | Aircraft landing gear, aircraft, and related methods |
US20190077499A1 (en) * | 2017-09-13 | 2019-03-14 | General Atomics Aeronautical Systems, Inc. | Folding trailing arm landing gear |
-
1961
- 1961-08-08 FR FR870329A patent/FR1304121A/en not_active Expired
-
1962
- 1962-02-06 GB GB454762A patent/GB984775A/en not_active Expired
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4272366A (en) * | 1979-08-16 | 1981-06-09 | Fmc Corporation | Heavy duty two mass vibratory machine |
WO2005028304A2 (en) * | 2003-08-15 | 2005-03-31 | The Boeing Company | Airplane landing gear |
WO2005028304A3 (en) * | 2003-08-15 | 2005-06-09 | Boeing Co | Airplane landing gear |
EP3366579A1 (en) * | 2017-02-28 | 2018-08-29 | The Boeing Company | Aircraft landing gear, aircraft, and related methods |
EP3366578A1 (en) * | 2017-02-28 | 2018-08-29 | The Boeing Company | Aircraft landing gear, aircraft, and related methods |
CN108502143A (en) * | 2017-02-28 | 2018-09-07 | 波音公司 | Aircraft landing gear structures, aircraft and correlation technique for aircraft |
CN108502143B (en) * | 2017-02-28 | 2023-03-10 | 波音公司 | Aircraft landing gear structure for an aircraft, aircraft and associated method |
US20190077499A1 (en) * | 2017-09-13 | 2019-03-14 | General Atomics Aeronautical Systems, Inc. | Folding trailing arm landing gear |
US10967959B2 (en) * | 2017-09-13 | 2021-04-06 | General Atomics Aeronautical Systems, Inc. | Folding trailing arm landing gear |
US11530031B2 (en) | 2017-09-13 | 2022-12-20 | General Atomics Aeronautical Systems, Inc. | Folding trailing arm landing gear |
US11932379B2 (en) | 2017-09-13 | 2024-03-19 | General Atomics Aeronautical Systems, Inc. | Folding trailing arm landing gear |
Also Published As
Publication number | Publication date |
---|---|
FR1304121A (en) | 1962-09-21 |
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