GB808438A - Mechanism for controlling the direction of rotation of a rotatable element - Google Patents

Mechanism for controlling the direction of rotation of a rotatable element

Info

Publication number
GB808438A
GB808438A GB1455956A GB1455956A GB808438A GB 808438 A GB808438 A GB 808438A GB 1455956 A GB1455956 A GB 1455956A GB 1455956 A GB1455956 A GB 1455956A GB 808438 A GB808438 A GB 808438A
Authority
GB
United Kingdom
Prior art keywords
cylinder
collar
pivots
pivot
cylinders
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
GB1455956A
Inventor
Walter Henry Hogan
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.)
Cleveland Pneumatic Tool Co
Original Assignee
Cleveland Pneumatic Tool Co
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 Cleveland Pneumatic Tool Co filed Critical Cleveland Pneumatic Tool Co
Priority to GB1455956A priority Critical patent/GB808438A/en
Publication of GB808438A publication Critical patent/GB808438A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Steering-Linkage Mechanisms And Four-Wheel Steering (AREA)

Abstract

808,438. Vehicle power steering. CLEVELAND PNEUMATIC TOOL CO. May 10, 1956, No. 14559/56. Class 79(5) [Also in Group XXXIII] Mechanism for controlling the direction of rotation of a rotatable element, e.g. a steerable aircraft undercarriage leg comprises a support element for the rotatable element, first and second cylinder members and associated fluid actuated piston members, a mounting portion on each member extending generally in the same direction, each cylinder mounting portion being connected to one of said elements and each piston mounting portion to the other element, at least one cylinder pivot and its associated piston pivot being equally spaced from the axis of rotation of the rotatable element, and stabilizing means between the cylinder members to prevent uncontrolled rotation thereof. In Figs. 2 and 3 twin-aircraft ground wheels are mounted at the foot of an inner cylinder 11 forming a shock absorber with an outer cylinder 10. A collar 14 is rotatably mounted on the cylinder 10, and is connected to the cylinder 11 by a scissors linkage 16, so that the wheel may be steered by rotating collar 14. Two mounting portions 19 on cylinders 17, 18 are pivoted at 22 to lugs 21 on cylinder 10, and two mounting portions on the piston rods 26 are pivoted at 31, 32 to lugs 29 on the collar 14. The cylinders have fluid pressure ports 33 and 34. The collar is rotated by admitting fluid under pressure to the port 33 of one cylinder and the port 34 of the other. At some point in the steering range, pivot 32 will be aligned with its associated piston rod pivot 22, whereupon the cylinder 18 will be free to swing about these pivots. To prevent this a bar 36 is pivoted to the cylinders at 37, 38. Similarly, when pivot 31 is aligned with its associated piston rod pivot 22, the cylinder 18 and bar 36 prevents cylinder 17 from swinging. The pivots 37, 38 are equidistant from the associated pivots 22. In Fig. 9, the arrangement is such that when the wheel is in the neutral position, the associated cylinder and piston rod pivots of cylinder 119 coincide at 136, and those of cylinder 121 at 138 and both cylinders are free to swing. To prevent this, a bar 143 is pivoted to the cylinders at 144, 146, and is formed with a tooth 147 engaging a notch 148 formed in the collar. Each cylinder rotates relatively to the fixed cylinder 10 with half the angular velocity of the collar, and the tooth 147 and notch 148 are located half way between the axis of bar 143 and the axis of the collar, whereby the tooth and notch have the same velocity when the wheel is turned from the neutral position, and their successive positions are shown in chain dot lines in Fig. 9. Fig. 10 (not shown) shows a modification in which the two pivots associated with cylinder 119 are further from the axis 137 than those of cylinder 121, though the pivots of each associated pair are equidistant from axis 137. Co-operating abutments on the collar and fixed cylinder limit the range of steering.
GB1455956A 1956-05-10 1956-05-10 Mechanism for controlling the direction of rotation of a rotatable element Expired GB808438A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1455956A GB808438A (en) 1956-05-10 1956-05-10 Mechanism for controlling the direction of rotation of a rotatable element

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1455956A GB808438A (en) 1956-05-10 1956-05-10 Mechanism for controlling the direction of rotation of a rotatable element

Publications (1)

Publication Number Publication Date
GB808438A true GB808438A (en) 1959-02-04

Family

ID=10043418

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1455956A Expired GB808438A (en) 1956-05-10 1956-05-10 Mechanism for controlling the direction of rotation of a rotatable element

Country Status (1)

Country Link
GB (1) GB808438A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2536500A (en) * 2015-03-20 2016-09-21 Airbus Operations Ltd Steering Device for an aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2536500A (en) * 2015-03-20 2016-09-21 Airbus Operations Ltd Steering Device for an aircraft
US9988144B2 (en) 2015-03-20 2018-06-05 Airbus Operations Limited Steering device for an aircraft

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