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GB351914A - Improvements in engines, particularly for aircraft - Google Patents

Improvements in engines, particularly for aircraft

Info

Publication number
GB351914A
GB351914A GB39346/29A GB3934629A GB351914A GB 351914 A GB351914 A GB 351914A GB 39346/29 A GB39346/29 A GB 39346/29A GB 3934629 A GB3934629 A GB 3934629A GB 351914 A GB351914 A GB 351914A
Authority
GB
United Kingdom
Prior art keywords
axis
propeller
engine
aircraft
tilted
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
GB39346/29A
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
Publication of GB351914A publication Critical patent/GB351914A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/04—Aircraft characterised by the type or position of power plants of piston type

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Retarders (AREA)
  • Transmission Devices (AREA)
  • Toys (AREA)

Abstract

351,914. Controlling aircraft. CAUDRON, R., 52, Rue Guynemer, Issy-les- Moulineaux, Seine, France. Dec. 23, 1929, No. 39346. Convention date, Jan. 9. Void [Published under Sect. 91 of the Acts]. [Class 4.] To counteract a tendency to turn when a single propeller is used or when one of a number of separately driven propellers, particularly of an aircraft, fails, the axis of any or each of the propellers is angularly adjusted. The Figure shows an engine and propeller pivoted about an axis f<1>, f<2> in a frame pivoted about an axis e<1>, e<2> at right-angles to the first axis, tilting about the two axes being controlled by the two sets of screw gear shown. A modification is described in which an engine not on the centre line of the machine is tilted about a vertical axis, which does not intersect the propeller axis, by a rod and bell-crank lever connected to screw gear operated from the central fuselage. Another modification is described in which an engine with its propeller is tilted by worm-gear about a vertical axis intersecting the propeller axis.
GB39346/29A 1929-01-09 1929-12-23 Improvements in engines, particularly for aircraft Expired GB351914A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BE351914X 1929-01-09

Publications (1)

Publication Number Publication Date
GB351914A true GB351914A (en) 1931-07-02

Family

ID=3868227

Family Applications (1)

Application Number Title Priority Date Filing Date
GB39346/29A Expired GB351914A (en) 1929-01-09 1929-12-23 Improvements in engines, particularly for aircraft

Country Status (1)

Country Link
GB (1) GB351914A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3031157A (en) * 1958-11-05 1962-04-24 Billie J Varden Controllable mount for aircraft power plant

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3031157A (en) * 1958-11-05 1962-04-24 Billie J Varden Controllable mount for aircraft power plant

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