GB860432A - Retractable undercarriages for aircraft - Google Patents
Retractable undercarriages for aircraftInfo
- Publication number
- GB860432A GB860432A GB2214056A GB2214056A GB860432A GB 860432 A GB860432 A GB 860432A GB 2214056 A GB2214056 A GB 2214056A GB 2214056 A GB2214056 A GB 2214056A GB 860432 A GB860432 A GB 860432A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- link
- undercarriage
- sleeve
- fore
- 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
-
- 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
- B64C25/12—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like sideways
- B64C2025/125—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like sideways into the fuselage, e.g. main landing gear pivotally retracting into or extending out of the fuselage
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
Abstract
860,432. Aircraft undercarriages. ELECTROHYDRAULICS Ltd. May 16, 1957 [July 17, 1956], No. 22140/56. Class 4. In an aircraft undercarriage mounted for retraction into the fuselage by fore-and-aft and inward movement, linkage is provided to maintain the wheel bogie parallel to the aircraft fore-and-aft axis to reduce drag during retraction. The undercarriage comprises a main leg 3 extended by a cranked portion 1 mounted by a skewed pivot 2 in the fuselage. The leg 3 carries a rotatable sleeve 6, 7 which houses the sliding tube assembly 4 on which the bogie 9 is mounted. A break-joint bracing strut 12 locks the undercarriage in the down position and the sleeve part 6 is pivotally connected to one end of a link 14 secured to the airframe. During retraction and extension of the undercarriage by a jack 16, the link 14, through sleeve 6, 7 and scissors linkage 11 serves to maintain the bogie 9 parallel to the fore and aft axis of the aircraft. The sleeve 6, 7 and link 14 may be dispensed with and the scissors linkage connected by a link to the strut 12.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2214056A GB860432A (en) | 1956-07-17 | 1956-07-17 | Retractable undercarriages for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2214056A GB860432A (en) | 1956-07-17 | 1956-07-17 | Retractable undercarriages for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB860432A true GB860432A (en) | 1961-02-08 |
Family
ID=10174540
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2214056A Expired GB860432A (en) | 1956-07-17 | 1956-07-17 | Retractable undercarriages for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB860432A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3346218A (en) * | 1965-03-15 | 1967-10-10 | Rech Etudes Prod | Retraction of fuselage under-carriages with wheels arranged in diabolo mounting |
US3357659A (en) * | 1965-04-16 | 1967-12-12 | Rech Etudes Prod | Retraction devices for fuselage undercarriages with wheels arranged in diabolo mounting |
US3372892A (en) * | 1965-01-19 | 1968-03-12 | Hawker Siddeley Dynamics Ltd | Retractable wheel mountings |
DE1281854B (en) * | 1965-04-16 | 1968-10-31 | Messier Sa | Retraction system for a landing gear that can be retracted into an aircraft fuselage |
EP0031601A1 (en) * | 1979-12-26 | 1981-07-08 | The Boeing Company | Body-braced main airplane landing gear |
US4328939A (en) * | 1979-12-26 | 1982-05-11 | The Boeing Company | Airplane main landing gear assembly |
JP2012101784A (en) * | 2010-11-05 | 2012-05-31 | Goodrich Corp | Vertically retracting side articulating landing gear for aircraft |
-
1956
- 1956-07-17 GB GB2214056A patent/GB860432A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3372892A (en) * | 1965-01-19 | 1968-03-12 | Hawker Siddeley Dynamics Ltd | Retractable wheel mountings |
US3346218A (en) * | 1965-03-15 | 1967-10-10 | Rech Etudes Prod | Retraction of fuselage under-carriages with wheels arranged in diabolo mounting |
US3357659A (en) * | 1965-04-16 | 1967-12-12 | Rech Etudes Prod | Retraction devices for fuselage undercarriages with wheels arranged in diabolo mounting |
DE1281854B (en) * | 1965-04-16 | 1968-10-31 | Messier Sa | Retraction system for a landing gear that can be retracted into an aircraft fuselage |
EP0031601A1 (en) * | 1979-12-26 | 1981-07-08 | The Boeing Company | Body-braced main airplane landing gear |
US4328939A (en) * | 1979-12-26 | 1982-05-11 | The Boeing Company | Airplane main landing gear assembly |
JP2012101784A (en) * | 2010-11-05 | 2012-05-31 | Goodrich Corp | Vertically retracting side articulating landing gear for aircraft |
US9205917B2 (en) | 2010-11-05 | 2015-12-08 | Goodrich Corporation | Vertically retracting side articulating landing gear for aircraft |
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