GB653891A - Undercarriage or landing gear for airplanes - Google Patents

Undercarriage or landing gear for airplanes

Info

Publication number
GB653891A
GB653891A GB2561848A GB2561848A GB653891A GB 653891 A GB653891 A GB 653891A GB 2561848 A GB2561848 A GB 2561848A GB 2561848 A GB2561848 A GB 2561848A GB 653891 A GB653891 A GB 653891A
Authority
GB
United Kingdom
Prior art keywords
undercarriage
airplanes
landing gear
movement
during toe
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
GB2561848A
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
Priority to GB2561848A priority Critical patent/GB653891A/en
Publication of GB653891A publication Critical patent/GB653891A/en
Expired legal-status Critical Current

Links

Classifications

    • 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 
    • B64C25/50—Steerable undercarriages; Shimmy-damping

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

653,891. Undercarriages for aircraft. GEISSE, J. H. Oct. 1, 1948, No. 25618. [Class 4] In an undercarriage with transversely-spaced castoring landing wheels the resistance imposed upon the wheels during toe-in movement is greater than during toe-out movement. As shown, each wheel spindle at 3 carries a crosshead 5 subject to the action of opposed springs a, b which are of different strengths. In the case of a three-wheeled undercarriage the nose or tail wheel may be coupled to the ailerons.
GB2561848A 1948-10-01 1948-10-01 Undercarriage or landing gear for airplanes Expired GB653891A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2561848A GB653891A (en) 1948-10-01 1948-10-01 Undercarriage or landing gear for airplanes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2561848A GB653891A (en) 1948-10-01 1948-10-01 Undercarriage or landing gear for airplanes

Publications (1)

Publication Number Publication Date
GB653891A true GB653891A (en) 1951-05-30

Family

ID=10230577

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2561848A Expired GB653891A (en) 1948-10-01 1948-10-01 Undercarriage or landing gear for airplanes

Country Status (1)

Country Link
GB (1) GB653891A (en)

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