GB437447A - Improvements in aeroplanes - Google Patents

Improvements in aeroplanes

Info

Publication number
GB437447A
GB437447A GB12678/34A GB1267834A GB437447A GB 437447 A GB437447 A GB 437447A GB 12678/34 A GB12678/34 A GB 12678/34A GB 1267834 A GB1267834 A GB 1267834A GB 437447 A GB437447 A GB 437447A
Authority
GB
United Kingdom
Prior art keywords
parts
movable
centre
gravity
adjusted
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
GB12678/34A
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 GB437447A publication Critical patent/GB437447A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Escalators And Moving Walkways (AREA)

Abstract

437,447. Aeroplanes modified for vertical flight. FUJIMOTO, B., 6, 3-chome, Kagura-cho, Ushigome-ku, Tokio. April 26, 1934, No. 12678. Convention date, May 23, 1933. [Class 4] In an aeroplane comprising a wing extending from each side of the fuselage, each of the wings include fixed parts 2 and movable parts 1 carrying the propelling mechanism and provided at their trailing edges with movable flaps 11 which may be adjusted so that due to aerodynamic forces the movable parts may be adjusted from a horizontal to a vertical position. Stop pins 7 and 8 and beams 4 limit movement of the movable parts. Axles 6, which may be inclined to one another, of the parts 1, may be situated, at about three-tenths of the length of the chord from the leading edge, or to the rear of and below the centre of gravity of the parts 1, or in front of and above the centre of gravity of the fixed parts of the machine.
GB12678/34A 1933-05-23 1934-04-26 Improvements in aeroplanes Expired GB437447A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP437447X 1933-05-23

Publications (1)

Publication Number Publication Date
GB437447A true GB437447A (en) 1935-10-28

Family

ID=12672260

Family Applications (1)

Application Number Title Priority Date Filing Date
GB12678/34A Expired GB437447A (en) 1933-05-23 1934-04-26 Improvements in aeroplanes

Country Status (1)

Country Link
GB (1) GB437447A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2993464A (en) * 1957-08-05 1961-07-25 Outboard Marine Corp Propeller assisted steering and automatic torque compensation for an outboard motor
US3029043A (en) * 1958-01-27 1962-04-10 Robert D Lindeman Free floating wing structure and control system for convertible aircraft
US3039719A (en) * 1956-11-16 1962-06-19 Haviland H Platt Vertical take-off airplane
US3166271A (en) * 1962-08-20 1965-01-19 Daniel R Zuck Airplane having non-stalling wings and wing-mounted propellers
US3284027A (en) * 1964-01-09 1966-11-08 Nord Aviation Vtol aircraft having freely pivoted propulsion means
CN110087992A (en) * 2016-12-30 2019-08-02 泗川航空航天工业制造有限公司 The type that verts rotor

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3039719A (en) * 1956-11-16 1962-06-19 Haviland H Platt Vertical take-off airplane
US2993464A (en) * 1957-08-05 1961-07-25 Outboard Marine Corp Propeller assisted steering and automatic torque compensation for an outboard motor
US3029043A (en) * 1958-01-27 1962-04-10 Robert D Lindeman Free floating wing structure and control system for convertible aircraft
US3166271A (en) * 1962-08-20 1965-01-19 Daniel R Zuck Airplane having non-stalling wings and wing-mounted propellers
US3284027A (en) * 1964-01-09 1966-11-08 Nord Aviation Vtol aircraft having freely pivoted propulsion means
CN110087992A (en) * 2016-12-30 2019-08-02 泗川航空航天工业制造有限公司 The type that verts rotor
US11220333B2 (en) * 2016-12-30 2022-01-11 Samco Co., Ltd Tilting type rotor

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