GB252433A - Improvements in and relating to the control of aeroplanes and the like - Google Patents

Improvements in and relating to the control of aeroplanes and the like

Info

Publication number
GB252433A
GB252433A GB4849/25A GB484925A GB252433A GB 252433 A GB252433 A GB 252433A GB 4849/25 A GB4849/25 A GB 4849/25A GB 484925 A GB484925 A GB 484925A GB 252433 A GB252433 A GB 252433A
Authority
GB
United Kingdom
Prior art keywords
shaft
chain
wheel
tail plane
fuselage
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
GB4849/25A
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.)
GEORGE ARTHUR REEDER
THOMAS FREDERICK ROBERTS
Original Assignee
GEORGE ARTHUR REEDER
THOMAS FREDERICK ROBERTS
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 GEORGE ARTHUR REEDER, THOMAS FREDERICK ROBERTS filed Critical GEORGE ARTHUR REEDER
Priority to GB4849/25A priority Critical patent/GB252433A/en
Publication of GB252433A publication Critical patent/GB252433A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Non-Deflectable Wheels, Steering Of Trailers, Or Other Steering (AREA)

Abstract

252,433. Roberts, T. F., and Reeder, G. A. Feb. 21, 1925. Steering and balancing.-An aeroplane has its wings and a tail plane simultaneously adjustable about horizontal transverse axes, the tail plane also having an independent adjustment about the longitudinal axis of the machine. Means for locking the wings and leaving the tail plane to be used independently may be provided. The wings are mounted on a transverse shaft 2 which carries two chain wheels 4 connected by chains 5 to wheels 6 on a transverse shaft 7 which is connected through chain gearing 8, 9, 10, 13, 14, 15 to a handle 16. The shaft 2 has a chain wheel 17 connected by a crossed chain 18 to a wheel 19 on a shaft 20 journaled in a cap 21 on the end of the fuselage. The tail plane 22 is secured to this shaft 20 and flexible extensions 36 extend between loops 35 on this shaft and spring connections 37 on the fuselage. The cap 21 rotates on ball bearings in the end of the fuselage and has a toothed rim 23 engaged by a gear wheel on a vertical shaft having a second wheel 26 connected by a chain 27 to a wheel 28 on a vertical shaft 29. This shaft is connected by the chain gearing shown to a second shaft 33 provided with a hand wheel 34. Cords and grooved pulleys may be used instead of chains and chain wheels.
GB4849/25A 1925-02-21 1925-02-21 Improvements in and relating to the control of aeroplanes and the like Expired GB252433A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB4849/25A GB252433A (en) 1925-02-21 1925-02-21 Improvements in and relating to the control of aeroplanes and the like

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4849/25A GB252433A (en) 1925-02-21 1925-02-21 Improvements in and relating to the control of aeroplanes and the like

Publications (1)

Publication Number Publication Date
GB252433A true GB252433A (en) 1926-05-21

Family

ID=9784945

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4849/25A Expired GB252433A (en) 1925-02-21 1925-02-21 Improvements in and relating to the control of aeroplanes and the like

Country Status (1)

Country Link
GB (1) GB252433A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6073880A (en) * 1998-05-18 2000-06-13 Versatron, Inc. Integrated missile fin deployment system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6073880A (en) * 1998-05-18 2000-06-13 Versatron, Inc. Integrated missile fin deployment system

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