GB527111A - Improvements relating to aircraft with retractable undercarriages - Google Patents
Improvements relating to aircraft with retractable undercarriagesInfo
- Publication number
- GB527111A GB527111A GB1014139A GB1014139A GB527111A GB 527111 A GB527111 A GB 527111A GB 1014139 A GB1014139 A GB 1014139A GB 1014139 A GB1014139 A GB 1014139A GB 527111 A GB527111 A GB 527111A
- Authority
- GB
- United Kingdom
- Prior art keywords
- leg
- gear
- landing
- aircraft
- resilient mounting
- 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 Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
Abstract
527,111. Aircraft landing gear. DOWTY, G. H. March 31, 1939, No. 10141. [Class 4] A retractable landing gear comprising a leg 1 and a resilient mounting means 7, 10 for a landing element 9 is so arranged that in the retracted position the parts 7, 9, 10 are mainly housed in a stowage space of an aircraft structure while the leg occupies at most only a marginal portion of the stowage space. The leg is moved by a jack acting upon a breakable strut 13, 15, these parts becoming partially housed in the leg, which is of channel section, when the gear is retracted. The leg may be downwardly bowed to act as a landing-skid should it be impossible to lower the gear. The leg may have a fairing effective in the retracted position of the gear. The resilient mounting may be of the kind described in Specifications 473,756, 473,768, 517,370, 517,373, 517,380, 517,724, 521,219 and 522,833, and may be fitted with means for moving the resilient mounting and landing element during retraction as described in Specification 527,110.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1014139A GB527111A (en) | 1939-03-31 | 1939-03-31 | Improvements relating to aircraft with retractable undercarriages |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1014139A GB527111A (en) | 1939-03-31 | 1939-03-31 | Improvements relating to aircraft with retractable undercarriages |
Publications (1)
Publication Number | Publication Date |
---|---|
GB527111A true GB527111A (en) | 1940-10-02 |
Family
ID=9962259
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1014139A Expired GB527111A (en) | 1939-03-31 | 1939-03-31 | Improvements relating to aircraft with retractable undercarriages |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB527111A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2437219A (en) * | 1944-08-05 | 1948-03-02 | American Steel Foundries | Shock strut |
JP2009516612A (en) * | 2005-11-21 | 2009-04-23 | エアバス・フランス | Wheel casing having separation structure |
US8118259B2 (en) | 2006-07-12 | 2012-02-21 | Airbus Operations Sas | Storage compartment for the nose gear of an aircraft |
CN104760689A (en) * | 2013-12-19 | 2015-07-08 | 空中客车运营简化股份公司 | Landing gear for aircraft |
-
1939
- 1939-03-31 GB GB1014139A patent/GB527111A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2437219A (en) * | 1944-08-05 | 1948-03-02 | American Steel Foundries | Shock strut |
JP2009516612A (en) * | 2005-11-21 | 2009-04-23 | エアバス・フランス | Wheel casing having separation structure |
US8118259B2 (en) | 2006-07-12 | 2012-02-21 | Airbus Operations Sas | Storage compartment for the nose gear of an aircraft |
CN101489867B (en) * | 2006-07-12 | 2013-03-06 | 空中客车运营简化股份公司 | Storage compartment for the nose gear of an aircraft |
CN104760689A (en) * | 2013-12-19 | 2015-07-08 | 空中客车运营简化股份公司 | Landing gear for aircraft |
CN104760689B (en) * | 2013-12-19 | 2018-09-04 | 空中客车运营简化股份公司 | Undercarriage for aircraft |
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