GB676964A - Aeroplane landing gear - Google Patents

Aeroplane landing gear

Info

Publication number
GB676964A
GB676964A GB1157/49A GB115749A GB676964A GB 676964 A GB676964 A GB 676964A GB 1157/49 A GB1157/49 A GB 1157/49A GB 115749 A GB115749 A GB 115749A GB 676964 A GB676964 A GB 676964A
Authority
GB
United Kingdom
Prior art keywords
cylinder
aircraft
discs
jan
boss
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
Application number
GB1157/49A
Inventor
George Warrener Bryan
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Electro Hydraulics Ltd
Original Assignee
Electro Hydraulics Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Electro Hydraulics Ltd filed Critical Electro Hydraulics Ltd
Priority to GB1157/49A priority Critical patent/GB676964A/en
Publication of GB676964A publication Critical patent/GB676964A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/50Steerable undercarriages; Shimmy-damping
    • B64C25/505Shimmy damping

Abstract

676,964. Shimmy dampers for aircraft undercarriages. ELECTRO - HYDRAULICS, Ltd. Jan. 9, 1950 [Jan. 14, 1949], No. 1157/49. Class 4. An aircraft undercarriage comprises an outer cylinder 1 pivotally attached to the aircraft by cross-arms 2 which engage bearings 3, an inner cylinder 6 rotatably mounted in the outer cylinder 1, a tube 11 carrying the landing wheel or wheels and connected to the cylinder 6 by torque links 8, 9, a shockabsorber for damping the wheel loads, and a shimmy damper in the form of a friction device 21 between the outer and inner cylinders 1 and 6. As shown the friction member comprises one or more discs 21 in a recess in the lower cylinder bearing 5, and engaged by a boss 19 at the lower end of the cylinder 6. Drainage grooves 20 are provided in the boss 19. When the aircraft is airborne the friction members disengage and allow the operation of the centring mechanism which comprises a cam 14 engaged by a roller 15 loaded by a spring 17. In a further arrangement, Fig. 3 (not shown), the shimmy damper consists of alternate discs of steel and material known under the Registered Trade Mark "Bakelite'' or "Carobronze," grease being inserted between the contacting surfaces of the discs.
GB1157/49A 1949-01-14 1949-01-14 Aeroplane landing gear Expired GB676964A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1157/49A GB676964A (en) 1949-01-14 1949-01-14 Aeroplane landing gear

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1157/49A GB676964A (en) 1949-01-14 1949-01-14 Aeroplane landing gear

Publications (1)

Publication Number Publication Date
GB676964A true GB676964A (en) 1952-08-06

Family

ID=9717175

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1157/49A Expired GB676964A (en) 1949-01-14 1949-01-14 Aeroplane landing gear

Country Status (1)

Country Link
GB (1) GB676964A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109204788A (en) * 2017-07-03 2019-01-15 广元公正科技有限公司 The shock-damping structure of aircraft nose wheel
CN112124571A (en) * 2020-09-10 2020-12-25 中国航空工业集团公司沈阳飞机设计研究所 Outer cylinder of aircraft landing gear, manufacturing method and aircraft landing gear
CN113548176A (en) * 2021-09-01 2021-10-26 许通量 Active control variable damping unmanned aerial vehicle shimmy damper based on electrorheological fluid

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109204788A (en) * 2017-07-03 2019-01-15 广元公正科技有限公司 The shock-damping structure of aircraft nose wheel
CN112124571A (en) * 2020-09-10 2020-12-25 中国航空工业集团公司沈阳飞机设计研究所 Outer cylinder of aircraft landing gear, manufacturing method and aircraft landing gear
CN113548176A (en) * 2021-09-01 2021-10-26 许通量 Active control variable damping unmanned aerial vehicle shimmy damper based on electrorheological fluid

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