GB527191A - Improvements relating to retractible undercarriages for aircraft - Google Patents

Improvements relating to retractible undercarriages for aircraft

Info

Publication number
GB527191A
GB527191A GB1037439A GB1037439A GB527191A GB 527191 A GB527191 A GB 527191A GB 1037439 A GB1037439 A GB 1037439A GB 1037439 A GB1037439 A GB 1037439A GB 527191 A GB527191 A GB 527191A
Authority
GB
United Kingdom
Prior art keywords
cylinder
wheel
collar
aircraft
undercarriages
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
GB1037439A
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.)
Boulton Paul Aircraft Ltd
Original Assignee
Boulton Paul Aircraft 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 Boulton Paul Aircraft Ltd filed Critical Boulton Paul Aircraft Ltd
Priority to GB1037439A priority Critical patent/GB527191A/en
Publication of GB527191A publication Critical patent/GB527191A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/02Undercarriages
    • B64C25/08Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/14Undercarriages 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)
  • Fluid-Damping Devices (AREA)

Abstract

527,191. Retractable undercarriages. BOUL- ,TON PAUL AIRCRAFT, Ltd., and NORTH, J. D. April 3, 1939, No. 10374. [Class 4] In retractable undercarriages of the kind in which the landing wheel is turned through a rightangle about a diameter while it is being swung backwardly and upwardly into a housing such as a recess in an engine nacelle, additional bearing is provided at or near the lower end of the undercarriage leg by a triangular pyramidal, or conical supporting structure hinged at its upper end to the aircraft frame. As shown in Fig. 2, the wheel is carried by a plunger 12 telescopically mounted under elastic and damping restraint in a cylinder 10. Struts 22 are connected to a collar 32 and a horizontal tubular member 20 having journals 40 for pivoting to the framework. The collar 32 and a collar 24 on the member 20 are provided with thrust and journal ball bearings on the cylinder 10. A toothed wheel or sector secured to the cylinder meshes with a similar element mounted on a shaft that passes through one end of the member 20 and is secured to the framework. The cylinder 10 may be locked in the operative position of the wheel by an hydraulicallycontrolled bolt.
GB1037439A 1939-04-03 1939-04-03 Improvements relating to retractible undercarriages for aircraft Expired GB527191A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1037439A GB527191A (en) 1939-04-03 1939-04-03 Improvements relating to retractible undercarriages for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1037439A GB527191A (en) 1939-04-03 1939-04-03 Improvements relating to retractible undercarriages for aircraft

Publications (1)

Publication Number Publication Date
GB527191A true GB527191A (en) 1940-10-03

Family

ID=9966665

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1037439A Expired GB527191A (en) 1939-04-03 1939-04-03 Improvements relating to retractible undercarriages for aircraft

Country Status (1)

Country Link
GB (1) GB527191A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2529377A (en) * 1947-12-03 1950-11-07 Electro Hydraulics Ltd Undercarriage suspension for aircraft
US2667316A (en) * 1951-04-25 1954-01-26 Bell Aircraft Corp Retractable aircraft undercarriage
FR2599103A1 (en) * 1986-05-20 1987-11-27 Valmet Oy SUPPORT AND FIXING STRUCTURE FOR A PISTON-CYLINDER OR EQUIVALENT ASSEMBLY
EP3196117A1 (en) * 2016-01-14 2017-07-26 Embraer S.A. Retractable self-aligning aircraft stabilizer strut assembly and aircraft including the same
GB2551380A (en) * 2016-06-16 2017-12-20 Airbus Operations Ltd Aircraft landing gear

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2529377A (en) * 1947-12-03 1950-11-07 Electro Hydraulics Ltd Undercarriage suspension for aircraft
US2667316A (en) * 1951-04-25 1954-01-26 Bell Aircraft Corp Retractable aircraft undercarriage
FR2599103A1 (en) * 1986-05-20 1987-11-27 Valmet Oy SUPPORT AND FIXING STRUCTURE FOR A PISTON-CYLINDER OR EQUIVALENT ASSEMBLY
EP3196117A1 (en) * 2016-01-14 2017-07-26 Embraer S.A. Retractable self-aligning aircraft stabilizer strut assembly and aircraft including the same
GB2551380A (en) * 2016-06-16 2017-12-20 Airbus Operations Ltd Aircraft landing gear
US11377205B2 (en) 2016-06-16 2022-07-05 Airbus Operations Limited Aircraft landing gear

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