GB251592A - Improvements in aircraft - Google Patents

Improvements in aircraft

Info

Publication number
GB251592A
GB251592A GB3540/26A GB354026A GB251592A GB 251592 A GB251592 A GB 251592A GB 3540/26 A GB3540/26 A GB 3540/26A GB 354026 A GB354026 A GB 354026A GB 251592 A GB251592 A GB 251592A
Authority
GB
United Kingdom
Prior art keywords
shaft
propeller
planes
bevel gear
transverse
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
GB3540/26A
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 GB251592A publication Critical patent/GB251592A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C23/00Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/005Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Agricultural Machines (AREA)
  • Catching Or Destruction (AREA)

Abstract

251,592. Watson, F. L. April 28, 1925, [Convention date]. Aeroplanes; helicopters; propelling; steering; planes, construction of.-A machine, adapted to fly vertically or horizontally, has a tractor propeller adapted to be swung from a horizontal to a vertical position, supporting planes provided with shutters on transverse axes which can be set in a vertical position during vertical flight, a lifting propeller at the tail. and means for retarding forward flight. The shaft 34 of the tractor 36 swings in a slot in the fuselage when moved by a quadrant 29 and worm 30. The shaft 34 is driven by bevel gear from the common transverse shaft of two laterally placed engines 24. The engine shaft is also connected by bevel gear and a clutch 40 to a longitudinal shaft 39 which drives through bevel gear a propeller 46 for supporting the tail during vertical flight. A brake 47 on the shaft of the propeller 46 becomes operative as the clutch 40 is released. The propeller shaft 34 is held at either end of the slot in the fuselage by catches operated from a lever 54. The planes 14, 15 have series of transverse shutters 17, Fig. 3, on shafts, moved by pinions 18 which engage racks 19 operated by levers 20 and controlled by a lever 21, Fig. 2. Stopping way.-To check forward motion a roller curtain 50 is pulled down by a cord 51 controlled by a hand wheel 52 to close the gap between the planes.
GB3540/26A 1925-04-28 1926-02-08 Improvements in aircraft Expired GB251592A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US251592XA 1925-04-28 1925-04-28

Publications (1)

Publication Number Publication Date
GB251592A true GB251592A (en) 1927-04-28

Family

ID=21824375

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3540/26A Expired GB251592A (en) 1925-04-28 1926-02-08 Improvements in aircraft

Country Status (1)

Country Link
GB (1) GB251592A (en)

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