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GB454198A - Improvements in and relating to tail skids and tail wheels for aircraft - Google Patents

Improvements in and relating to tail skids and tail wheels for aircraft

Info

Publication number
GB454198A
GB454198A GB35309/35A GB3530935A GB454198A GB 454198 A GB454198 A GB 454198A GB 35309/35 A GB35309/35 A GB 35309/35A GB 3530935 A GB3530935 A GB 3530935A GB 454198 A GB454198 A GB 454198A
Authority
GB
United Kingdom
Prior art keywords
tail
aircraft
shock
absorber
wheel
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
GB35309/35A
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.)
Mahle GmbH
Original Assignee
Elektronmetall GmbH
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 Elektronmetall GmbH filed Critical Elektronmetall GmbH
Publication of GB454198A publication Critical patent/GB454198A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/50Steerable undercarriages; Shimmy-damping

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vehicle Body Suspensions (AREA)

Abstract

454,198. Aircraft tail -wheels and tail-skids. ELEKTRONMETALL GES., 26, Pragstrasse, Cannstatt, Stuttgart, Germany. Dec. 20, 1935, No. 35309. Convention date, Feb. 19. [Class 4] In a tail-wheel or tailskid mounting in which a shock-absorber 2 is built into the rear of the aircraft fuselage so as to rise rearwardly, and the tail wheel 7 or skid element is arranged to swing about an axis C C vertical or inclined towards the bow of the aircraft with respect to the surface on which the aircraft taxies, the support bearing 5 which carries the tail-wheel or tail - skid is connected with the lower end of the shock-absorber so as to move in a straight line in the direction of the shock-absorber axis. The angle which the shock-absorber axis makes with the vertical may be about 20‹.
GB35309/35A 1935-02-19 1935-12-20 Improvements in and relating to tail skids and tail wheels for aircraft Expired GB454198A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE454198X 1935-02-19

Publications (1)

Publication Number Publication Date
GB454198A true GB454198A (en) 1936-09-25

Family

ID=6538881

Family Applications (1)

Application Number Title Priority Date Filing Date
GB35309/35A Expired GB454198A (en) 1935-02-19 1935-12-20 Improvements in and relating to tail skids and tail wheels for aircraft

Country Status (1)

Country Link
GB (1) GB454198A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2421914A (en) * 1942-06-08 1947-06-10 Boeing Aircraft Co Nose wheel

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2421914A (en) * 1942-06-08 1947-06-10 Boeing Aircraft Co Nose wheel

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