GB350784A - Improvements in or relating to landing gear of aeroplanes - Google Patents

Improvements in or relating to landing gear of aeroplanes

Info

Publication number
GB350784A
GB350784A GB21907/30A GB2190730A GB350784A GB 350784 A GB350784 A GB 350784A GB 21907/30 A GB21907/30 A GB 21907/30A GB 2190730 A GB2190730 A GB 2190730A GB 350784 A GB350784 A GB 350784A
Authority
GB
United Kingdom
Prior art keywords
torque
absorber
shock
landing gear
brake
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
GB21907/30A
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.)
Fiat SpA
Original Assignee
Fiat SpA
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 Fiat SpA filed Critical Fiat SpA
Priority to GB21907/30A priority Critical patent/GB350784A/en
Publication of GB350784A publication Critical patent/GB350784A/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 
    • B64C25/42—Arrangement or adaptation of brakes
    • 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)
  • Braking Arrangements (AREA)
  • Vehicle Body Suspensions (AREA)

Abstract

350,784. Aeroplane landing gear. SOKAL, S., 1, Great James Street, Bedford Row, London.-(Fiat Soc. Anon. ; 250, Via Nizza, Turin. Italy.) July 19, 1930, No. 21907. [Class 4.] A device for compensating the torque acting upon the struts and caused by the wheel braking is provided in which a torque counteracting the torque of the brake is produced by a lateral displacement of the point of connection of a shock absorber or elastic strut connected to the wheel axle. The point of connection or application of the strut of the shock-absorber 4, 5 with the wheel axle 2 is displaced laterally in order to give a torque countering that due to the application of the brake 6. The shock-absorber is adjusted laterally by means of a wing-nut 3.
GB21907/30A 1930-07-19 1930-07-19 Improvements in or relating to landing gear of aeroplanes Expired GB350784A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB21907/30A GB350784A (en) 1930-07-19 1930-07-19 Improvements in or relating to landing gear of aeroplanes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB21907/30A GB350784A (en) 1930-07-19 1930-07-19 Improvements in or relating to landing gear of aeroplanes

Publications (1)

Publication Number Publication Date
GB350784A true GB350784A (en) 1931-06-18

Family

ID=10170810

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21907/30A Expired GB350784A (en) 1930-07-19 1930-07-19 Improvements in or relating to landing gear of aeroplanes

Country Status (1)

Country Link
GB (1) GB350784A (en)

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