GB319613A - Improvements in or relating to aircraft - Google Patents

Improvements in or relating to aircraft

Info

Publication number
GB319613A
GB319613A GB27555/29A GB2755529A GB319613A GB 319613 A GB319613 A GB 319613A GB 27555/29 A GB27555/29 A GB 27555/29A GB 2755529 A GB2755529 A GB 2755529A GB 319613 A GB319613 A GB 319613A
Authority
GB
United Kingdom
Prior art keywords
airscrew
fuselage
slipstream
aeroplane
propelling
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
GB27555/29A
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 GB319613A publication Critical patent/GB319613A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/02—Gyroplanes

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

319,613. Bavay, A. J. F. de. Sept. 24, 1928, [Convention date]. Aeroplanes,. helicopters and machines supported by rotary propellers; starting; stopping way; propelling; controlling. - An aeroplane is provided with one or more horizontal lifting airscrews adapted to be rotated when taking-off or landing by energy derived from the slipstream of one or more propelling airscrews. Fig. 1 shows an aeroplane having a fuselage 4 and propelling airscrew 6 normally supported in flight by wings 5. A horizontal airscrew 7 is mounted on a spindle 8 supported in bearings in the fuselage and coupled to the rotor of an air turbine 9 having an intake 11 and discharge pipe 10. Hinged annular baffles 13, 14 under the control of the pilot are arranged in the space between the fuselage 4 and an open-ended guide cylinder 12 in such a manner that when closed they direct the slipstream from the airscrew 6 to the intake 11 of the turbine 9. When the baffles 13, 14 are open they lie parallel with the guide cylinder and fuselage respectively permitting the free passage of air therebetween. Alternatively one or more baffles arranged to direct the slipstream directly to the lifting airscrew may be employed in lieu of the air turbine. When more than one lifting airscrew is provided they are arranged symmetrically about the longitudinal axis of the aeroplane. Specification 28907/10 is referred to.
GB27555/29A 1928-09-24 1929-09-10 Improvements in or relating to aircraft Expired GB319613A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AU319613X 1928-09-24

Publications (1)

Publication Number Publication Date
GB319613A true GB319613A (en) 1930-12-10

Family

ID=3719588

Family Applications (1)

Application Number Title Priority Date Filing Date
GB27555/29A Expired GB319613A (en) 1928-09-24 1929-09-10 Improvements in or relating to aircraft

Country Status (1)

Country Link
GB (1) GB319613A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019056756A1 (en) * 2017-09-21 2019-03-28 深圳市道通智能航空技术有限公司 Propeller, power assembly and unmanned aerial vehicle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019056756A1 (en) * 2017-09-21 2019-03-28 深圳市道通智能航空技术有限公司 Propeller, power assembly and unmanned aerial vehicle

Similar Documents

Publication Publication Date Title
US2420323A (en) Wing-mounted jet-propulsion system with controllable discharge outlet
US2964264A (en) Power flap for aircraft
US4125232A (en) Vertical take-off and landing (VTOL) aircraft with fixed horizontal variable-pitched rotors
GB618475A (en) Improvements in or relating to aircraft of the gyroplane type
RU2550589C1 (en) Convertible vertical take-off and landing aircraft (versions)
US2584961A (en) Jet-propelled airplane with jettisonable wing-tip fuel tanks
US3231038A (en) Fixed wing ground effect craft
GB518663A (en) Improvements in or relating to aircraft, hydroplanes and the like
GB753970A (en) Improvements in or relating to helicopters
US3563497A (en) Flight control means for rotorcraft
US2532481A (en) Multiple channel wing airplane
GB319613A (en) Improvements in or relating to aircraft
GB167068A (en) Improvements in and relating to aeroplanes for commercial purposes
US2069047A (en) Aircraft control
US2564370A (en) Aircraft
US2974899A (en) Single propeller convertible vtol aircraft
GB636045A (en) Improvements in aircraft equipped with reaction jet propulsion means
GB900095A (en) Air-craft having an annular wing and a propulsion means fitted into the latter
GB375530A (en) Improvements in aeroplanes
US1840152A (en) Flying machine
US1870119A (en) Airplane
GB606088A (en) Improvements relating to aeroplanes
US1484632A (en) Helicopter flying machine
GB865524A (en) Improvements in or relating to annular-wing aircraft
GB424140A (en) Improvements relating to air-craft of the gyroplane type