GB109146A - Improved Construction and Arrangement of Axle for Aeroplanes and the like. - Google Patents

Improved Construction and Arrangement of Axle for Aeroplanes and the like.

Info

Publication number
GB109146A
GB109146A GB15617/16A GB1561716A GB109146A GB 109146 A GB109146 A GB 109146A GB 15617/16 A GB15617/16 A GB 15617/16A GB 1561716 A GB1561716 A GB 1561716A GB 109146 A GB109146 A GB 109146A
Authority
GB
United Kingdom
Prior art keywords
axle
aeroplanes
sopwith
axles
pivoted
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
GB15617/16A
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.)
SOPWITH AVIAT Co Ltd
Original Assignee
SOPWITH AVIAT Co 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 SOPWITH AVIAT Co Ltd filed Critical SOPWITH AVIAT Co Ltd
Priority to GB15617/16A priority Critical patent/GB109146A/en
Publication of GB109146A publication Critical patent/GB109146A/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
    • B64C25/62—Spring shock-absorbers; Springs
    • B64C25/64—Spring shock-absorbers; Springs using rubber or like elements

Abstract

109,146. Sopwith Aviation Co., and Sopwith, T. Nov. 1, 1916. Shock of landing, deadening.-A landing chassis for aeroplanes comprises two V-shaped side frames B, B<1>, C, C<1> connected together by a stream-lined strut A having a groove in its upper surface to take two axles E, E' pivoted at their inner ends and bearing at their outer ends beneath rubber bands K wound around studs X, X<1> on the side frames. Flanges M, H, H<1> are provided respectively oh the ends of the axles and the studs X, X<1>. A triangular piece 0 is secured in the apex of each side frame to guide the axleend. The central part of the groove in the strut A, where the axle-ends are pivoted, is reinforced by a metal plate and is provided with an eyebolt for the attachment of a cable Q.
GB15617/16A 1916-11-01 1916-11-01 Improved Construction and Arrangement of Axle for Aeroplanes and the like. Expired GB109146A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB15617/16A GB109146A (en) 1916-11-01 1916-11-01 Improved Construction and Arrangement of Axle for Aeroplanes and the like.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB15617/16A GB109146A (en) 1916-11-01 1916-11-01 Improved Construction and Arrangement of Axle for Aeroplanes and the like.

Publications (1)

Publication Number Publication Date
GB109146A true GB109146A (en) 1917-09-06

Family

ID=32249581

Family Applications (1)

Application Number Title Priority Date Filing Date
GB15617/16A Expired GB109146A (en) 1916-11-01 1916-11-01 Improved Construction and Arrangement of Axle for Aeroplanes and the like.

Country Status (1)

Country Link
GB (1) GB109146A (en)

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