GB412191A - An improved damping and suspension device for landing gears of aeroplanes - Google Patents

An improved damping and suspension device for landing gears of aeroplanes

Info

Publication number
GB412191A
GB412191A GB29067/33A GB2906733A GB412191A GB 412191 A GB412191 A GB 412191A GB 29067/33 A GB29067/33 A GB 29067/33A GB 2906733 A GB2906733 A GB 2906733A GB 412191 A GB412191 A GB 412191A
Authority
GB
United Kingdom
Prior art keywords
aeroplanes
suspension device
landing gears
improved damping
piston
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
GB29067/33A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB412191A publication Critical patent/GB412191A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/06—Undercarriages fixed
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/58—Arrangements or adaptations of shock-absorbers or springs
    • B64C25/60—Oleo legs

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid-Damping Devices (AREA)

Abstract

412,191. Piston rods. MESSIER, Y. L., 179, Boulevard Brune, Paris. Oct. 20, 1933, No. 29067. Convention date, Dec. 24, 1932. [Class 122 (i).] Relative rotation between a cylinder connected directly or indirectly to an aeroplane fusilage, and a piston-rod to which is connected a landing wheel is prevented by rigid links V<1>, V<2> hinged together at D and having their outer ends hinged respectively to the cylinder and piston rod. The hinge D may incorporate a universal joint.
GB29067/33A 1932-12-24 1933-10-20 An improved damping and suspension device for landing gears of aeroplanes Expired GB412191A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR412191X 1932-12-24

Publications (1)

Publication Number Publication Date
GB412191A true GB412191A (en) 1934-06-19

Family

ID=8897763

Family Applications (1)

Application Number Title Priority Date Filing Date
GB29067/33A Expired GB412191A (en) 1932-12-24 1933-10-20 An improved damping and suspension device for landing gears of aeroplanes

Country Status (1)

Country Link
GB (1) GB412191A (en)

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