GB742309A - A retractable undercarriage for aircraft - Google Patents

A retractable undercarriage for aircraft

Info

Publication number
GB742309A
GB742309A GB2177652A GB2177652A GB742309A GB 742309 A GB742309 A GB 742309A GB 2177652 A GB2177652 A GB 2177652A GB 2177652 A GB2177652 A GB 2177652A GB 742309 A GB742309 A GB 742309A
Authority
GB
United Kingdom
Prior art keywords
leg
aircraft
undercarriage
bogie
strut
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
GB2177652A
Inventor
Jack Perdue
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 GB2177652A priority Critical patent/GB742309A/en
Publication of GB742309A publication Critical patent/GB742309A/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 
    • B64C25/34Alighting gear characterised by elements which contact the ground or similar surface  wheeled type, e.g. multi-wheeled bogies

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Handcart (AREA)

Abstract

742,309. Aircraft undercarriages. ELECTRO-HYDRAULICS, Ltd. Oct. 23, 1953 [Aug. 29, 1952]. No. 21776/52. Class 4. A retractable aircraft undercarriage includes ground contacting elements comprising at least one wheel or set of wheels in tandem with another wheel or set of wheels, and also a member articulated to the undercarriage structure and carrying said wheel or wheels, and means carried by said elements which means on retraction, are adapted to co-operate with means on the aircraft or undercarriage to alter the articulated relation of the ground contacting elements to the undercarriage structure to facilitate storage of the undercarriage. In one embodiment (Fig. 1) the invention is applied to an undercarriage constructed as described in Figs. 4 and 5 of Specification 674,237, and provides rollers 61, 59 on the bogie 52 adapted to co-operate with cam surfaces 62, 63 on strut 4 to tilt bogie 52 to lie parallel with the leg 2 when retracted. In the embodiment of Figs. 6 and 9, the main undercarriage leg 1 is supported by a rigid strut 4 pivoted to the aircraft at 6 and to the leg at 5, and by a bearing 22 abutting stops on the aircraft (not shown) and locked by levers 41 spring-biased by spring-box 70 to engage studs 42 on the aircraft. On retraction, a jack 66 extending between the strut 4 and lug 67 contracts, and an auxiliary jack (not shown) removes lever 41 from studs 42, and as the main jack contracts, bearing 22 pivots on bars 39 about pivot 40, so that bars 39 and leg 1 jackknife to the retracted position. As shown in Fig. 9, rollers 61 on the bogie 52 contact a recess 76 in a resiliently mounted hook 75.so that as leg 1 and strut 4 become parallel, the bogie 52 is constrained to tilt parallel to leg 1. Brake torque reaction devices 73 are provided as described in Specification 635,842. An auxiliary shock-absorber 56, 57 is pivoted to a lug 50 on the leg and slides in a sleeve (not shown) pivoted at 71 to the bogie so as to bias the rear wheel to touch down first, and allow the bogie to tilt relatively to the leg. Specification 635,885 also is referred to.
GB2177652A 1952-08-29 1952-08-29 A retractable undercarriage for aircraft Expired GB742309A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2177652A GB742309A (en) 1952-08-29 1952-08-29 A retractable undercarriage for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2177652A GB742309A (en) 1952-08-29 1952-08-29 A retractable undercarriage for aircraft

Publications (1)

Publication Number Publication Date
GB742309A true GB742309A (en) 1955-12-21

Family

ID=10168598

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2177652A Expired GB742309A (en) 1952-08-29 1952-08-29 A retractable undercarriage for aircraft

Country Status (1)

Country Link
GB (1) GB742309A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3261574A (en) * 1965-01-15 1966-07-19 Boeing Co Aircraft universally jointed retractable landing gear
CN110001936A (en) * 2019-05-17 2019-07-12 中国科学院合肥物质科学研究院 A kind of imitative bird multi-rotor unmanned aerial vehicle undercarriage
EP4155199A1 (en) * 2021-09-28 2023-03-29 Airbus Operations Limited Landing gear stay

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3261574A (en) * 1965-01-15 1966-07-19 Boeing Co Aircraft universally jointed retractable landing gear
CN110001936A (en) * 2019-05-17 2019-07-12 中国科学院合肥物质科学研究院 A kind of imitative bird multi-rotor unmanned aerial vehicle undercarriage
CN110001936B (en) * 2019-05-17 2023-11-21 中国科学院合肥物质科学研究院 Bird-like multi-rotor unmanned aerial vehicle landing gear
EP4155199A1 (en) * 2021-09-28 2023-03-29 Airbus Operations Limited Landing gear stay
GB2611099A (en) * 2021-09-28 2023-03-29 Airbus Operations Ltd Landing gear stay
US11912400B2 (en) 2021-09-28 2024-02-27 Airbus Operations Limited Landing gear stay

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