GB791101A - Improvements in or relating to steering mechanism for aircraft nose wheels, or the like - Google Patents
Improvements in or relating to steering mechanism for aircraft nose wheels, or the likeInfo
- Publication number
- GB791101A GB791101A GB8284/56A GB828456A GB791101A GB 791101 A GB791101 A GB 791101A GB 8284/56 A GB8284/56 A GB 8284/56A GB 828456 A GB828456 A GB 828456A GB 791101 A GB791101 A GB 791101A
- Authority
- GB
- United Kingdom
- Prior art keywords
- link
- block
- pivoted
- steering mechanism
- aircraft nose
- 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
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/50—Steerable undercarriages; Shimmy-damping
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fluid-Damping Devices (AREA)
- Vehicle Body Suspensions (AREA)
Abstract
791,101. Steering vehicles. JARRY AUTOMOBILE LIMITEE. March 16, 1956 [Nov. 16, 1955], No. 8284/56. Class 79(5) [Also in Group XXXIII] A steering mechanism for an aircraft nose wheel mounted on a leg comprising a first part 17 and a second relatively rotatable part 19 comprises a block member 6 pivoted to the first part 17, a first link 4 pivoted to the block, a second link 1 pivoted to the second part 19 and universally jointed to the first link at 5, and an actuating means 11 to rotate the block and thereby to rotate the second part 19. As shown, an axle 18 bears twin wheels (not shown) and is secured to the part 19 by a twin collar 20. The parts 17, 19 form a shock absorber. The link 11 is connected to the piston of a hydraulic actuator mounted on the part 17. Fig. 1 (not shown) discloses a similar arrangement for a lever suspension type of nosewheel. The shock absorber preferably allows only a small telescoping of parts 17, 19, whereby the amount of rotation of part 19 for a given movement of block 6 is substantially predetermined.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US791101XA | 1955-11-16 | 1955-11-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB791101A true GB791101A (en) | 1958-02-26 |
Family
ID=22148492
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8284/56A Expired GB791101A (en) | 1955-11-16 | 1956-03-16 | Improvements in or relating to steering mechanism for aircraft nose wheels, or the like |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB791101A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2887517A1 (en) * | 2005-06-28 | 2006-12-29 | Airbus France Sas | STEERING DEVICE WITH REDUCED SIZE FOR AIRCRAFT LANDFILL |
DE102009003834A1 (en) | 2008-05-02 | 2009-11-05 | Ge Aviation Uk | Aircraft landing gear steering system |
CN103523217A (en) * | 2012-07-06 | 2014-01-22 | 哈尔滨飞机工业集团有限责任公司 | Nose-wheel steering system of aircraft |
WO2016162119A1 (en) * | 2015-04-08 | 2016-10-13 | Liebherr-Aerospace Lindenberg Gmbh | Steerable aircraft landing gear |
-
1956
- 1956-03-16 GB GB8284/56A patent/GB791101A/en not_active Expired
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2887517A1 (en) * | 2005-06-28 | 2006-12-29 | Airbus France Sas | STEERING DEVICE WITH REDUCED SIZE FOR AIRCRAFT LANDFILL |
WO2007000411A1 (en) * | 2005-06-28 | 2007-01-04 | Airbus France | Compact steering device for the landing gear of an aircraft |
CN101208241B (en) * | 2005-06-28 | 2011-08-10 | 空中客车法国公司 | Compact steering device for the landing gear of an aircraft |
US8136754B2 (en) | 2005-06-28 | 2012-03-20 | Airbus Operations Sas | Compact steering device for the landing gear of an aircraft |
DE102009003834A1 (en) | 2008-05-02 | 2009-11-05 | Ge Aviation Uk | Aircraft landing gear steering system |
US8752790B2 (en) | 2008-05-02 | 2014-06-17 | Ge Aviation Systems Limited | Aircraft landing gear steering system |
CN103523217A (en) * | 2012-07-06 | 2014-01-22 | 哈尔滨飞机工业集团有限责任公司 | Nose-wheel steering system of aircraft |
WO2016162119A1 (en) * | 2015-04-08 | 2016-10-13 | Liebherr-Aerospace Lindenberg Gmbh | Steerable aircraft landing gear |
DE102015004525A1 (en) * | 2015-04-08 | 2016-10-13 | Liebherr-Aerospace Lindenberg Gmbh | Steerable aircraft landing gear |
DE102015004525B4 (en) | 2015-04-08 | 2019-09-26 | Liebherr-Aerospace Lindenberg Gmbh | Steerable aircraft landing gear |
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