GB558902A - Improvements in or relating to landing gear for aircraft - Google Patents
Improvements in or relating to landing gear for aircraftInfo
- Publication number
- GB558902A GB558902A GB10280/42A GB1028042A GB558902A GB 558902 A GB558902 A GB 558902A GB 10280/42 A GB10280/42 A GB 10280/42A GB 1028042 A GB1028042 A GB 1028042A GB 558902 A GB558902 A GB 558902A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- relating
- landing gear
- messier
- gear
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/001—Devices not provided for in the groups B64C25/02 - B64C25/68
-
- 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
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/60—Oleo legs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/001—Devices not provided for in the groups B64C25/02 - B64C25/68
- B64C2025/006—Landing gear legs comprising torque arms
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tires In General (AREA)
- Braking Arrangements (AREA)
Abstract
558,902. Aircraft landing-gear. MESSIER AIRCRAFT EQUIPMENT, Ltd., (formerly RUBERYOWEN MESSIER, Ltd.), and PERRICHES, A. A. July 22, 1942, No. 10280. [Class 4] The wheel-carriage end of an element 12 of a telescopic strut for an aircraft undercarriage is connected to another element 11 through an intermediate member 18, sliding on element 12 and connected by pairs of links 16, 17 and 19, 20 to the elements 11 and 12 respectively at the lower ends thereof. Specification 412,191 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB10280/42A GB558902A (en) | 1942-07-22 | 1942-07-22 | Improvements in or relating to landing gear for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB10280/42A GB558902A (en) | 1942-07-22 | 1942-07-22 | Improvements in or relating to landing gear for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB558902A true GB558902A (en) | 1944-01-26 |
Family
ID=9964937
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB10280/42A Expired GB558902A (en) | 1942-07-22 | 1942-07-22 | Improvements in or relating to landing gear for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB558902A (en) |
-
1942
- 1942-07-22 GB GB10280/42A patent/GB558902A/en not_active Expired
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