GB191111139A - Improvements in and relating to Aeroplanes. - Google Patents

Improvements in and relating to Aeroplanes.

Info

Publication number
GB191111139A
GB191111139A GB191111139DA GB191111139A GB 191111139 A GB191111139 A GB 191111139A GB 191111139D A GB191111139D A GB 191111139DA GB 191111139 A GB191111139 A GB 191111139A
Authority
GB
United Kingdom
Prior art keywords
uprights
skids
collars
hull
girder
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
Inventor
Armand Jean August Deperdussin
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
Application granted granted Critical
Publication of GB191111139A publication Critical patent/GB191111139A/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

11,139. Deperdusain, A. J. A. Nov. 29, 1910. Aerial machines without aerostats; shock of landing, deadening. - In a monoplane flying- machine, the lattice girder frame A is cut away at its front lower part to accommodate the aviator, the motor, and accessories, and this part is strengthened by a detachable hull B consisting of sheets of wood or metal laid upon ribs. A tail-piece and rudder are carried at the rear by the girder, as described in Specification 27,792/10. The body is supported at the front by an undercarriage having two protecting- crutches A<2> forming the diagonals of rigid quadrilaterals comprising the girder A, uprights C, D, and skids E. The uprights C, D are provided with collars c which engage with bolts on the hull. The collars also clamp to the uprights cables c' passing under the hull and engaging a groove in the top of the uprights. Wheels F are mounted on an axle G, connected to the skids E by elastic members g<3> and radius rods g. The elastic members g<3>, Fig. 5, are pinned upon the axle. The members g<3> can be replaced or removed from position by withconnected to collars g<7> on the skids'and to pins g<4> carried in the ends of V-shaped brackets g<5> drawing the pins g<4>, g<6>. At the rear, the fuselage is supported by a single central runner.
GB191111139D 1910-11-29 1910-11-29 Improvements in and relating to Aeroplanes. Expired GB191111139A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191111139T 1910-11-29

Publications (1)

Publication Number Publication Date
GB191111139A true GB191111139A (en) 1911-10-05

Family

ID=32639068

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191111139D Expired GB191111139A (en) 1910-11-29 1910-11-29 Improvements in and relating to Aeroplanes.

Country Status (1)

Country Link
GB (1) GB191111139A (en)

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