GB1287099A - Improvements in or relating to aircraft ground-wheel steering mechanisms - Google Patents

Improvements in or relating to aircraft ground-wheel steering mechanisms

Info

Publication number
GB1287099A
GB1287099A GB5950768A GB5950768A GB1287099A GB 1287099 A GB1287099 A GB 1287099A GB 5950768 A GB5950768 A GB 5950768A GB 5950768 A GB5950768 A GB 5950768A GB 1287099 A GB1287099 A GB 1287099A
Authority
GB
United Kingdom
Prior art keywords
rack
pinion
recess
steering
detents
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
GB5950768A
Inventor
Cyril Spalding
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.)
Hawker Siddeley Dynamics Ltd
Original Assignee
Hawker Siddeley Dynamics 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 Hawker Siddeley Dynamics Ltd filed Critical Hawker Siddeley Dynamics Ltd
Priority to GB5950768A priority Critical patent/GB1287099A/en
Publication of GB1287099A publication Critical patent/GB1287099A/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

Abstract

1287099 Steering aircraft ground wheels HAWKER SIDDELEY DYNAMICS Ltd 15 Dec 1969 [13 Dec 1968] 59507/68 Heading B7H An aircraft ground wheel e.g. nosewheel, steering mechanism includes a rack-and-pinion assembly in which the pinion has around a minor portion of its periphery so that when the pinion 1 runs out of mesh with the rack 4 castoring is possible, provision being made to lock the rack in the position, in either direction of steering, at which it ceases to be in driving engagement with the pinion. As shown the rack 4, connected to power pistons 5, 5a is movable to the left or right by its engagement with teeth 11 of the rotatable pinion 1. At the position at which the rack and pinion run out of mesh during steering a recess 16 is provided in the rack housing. The rack is provided with a pair of detents 6, 6a co-operable with the recess to lock the rack at that position. The detents are biased by springs such as to oppose any tendency for them to enter the recess, pressure being exerted, to oppose this bias, during rotation of the pinion, by cut-aways 17 and a cam surface 19 on the pinion acting on the head of a detent as the rack moves. Once engaged in the recess, a detent is retained therein by the cam surface 19 until the pinion returns to re-engage with the rack. The rack is constructed in two halves bolted together. In modifications (not shown), the detents and co-operating cam are arranged away from the plane of rotation of the teeth 11 and the cam is separate from the gear, and the rack is a one-piece part.
GB5950768A 1968-12-13 1968-12-13 Improvements in or relating to aircraft ground-wheel steering mechanisms Expired GB1287099A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB5950768A GB1287099A (en) 1968-12-13 1968-12-13 Improvements in or relating to aircraft ground-wheel steering mechanisms

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5950768A GB1287099A (en) 1968-12-13 1968-12-13 Improvements in or relating to aircraft ground-wheel steering mechanisms

Publications (1)

Publication Number Publication Date
GB1287099A true GB1287099A (en) 1972-08-31

Family

ID=10483884

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5950768A Expired GB1287099A (en) 1968-12-13 1968-12-13 Improvements in or relating to aircraft ground-wheel steering mechanisms

Country Status (1)

Country Link
GB (1) GB1287099A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2568218A1 (en) * 1984-07-30 1986-01-31 Messier Hispano Bugatti Sa AIRCRAFT AIRCRAFT LIFT WITH RELEASE AND AUTOMATIC SAFETY CLUTCH
EP2366623A3 (en) * 2010-03-05 2014-01-01 Goodrich Corporation Landing gear steering systems
US8944368B2 (en) 2010-01-26 2015-02-03 Airbus Operations Limited Aircraft steering actuator

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2568218A1 (en) * 1984-07-30 1986-01-31 Messier Hispano Bugatti Sa AIRCRAFT AIRCRAFT LIFT WITH RELEASE AND AUTOMATIC SAFETY CLUTCH
US4610411A (en) * 1984-07-30 1986-09-09 Messier-Hispano-Bugatti (S.A.) Steerable aircraft landing gear having automatic safety declutching and enclutching
US8944368B2 (en) 2010-01-26 2015-02-03 Airbus Operations Limited Aircraft steering actuator
EP2366623A3 (en) * 2010-03-05 2014-01-01 Goodrich Corporation Landing gear steering systems

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Legal Events

Date Code Title Description
PS Patent sealed
PLNP Patent lapsed through nonpayment of renewal fees