GB531834A - Improved helicopter - Google Patents

Improved helicopter

Info

Publication number
GB531834A
GB531834A GB21583/39A GB2158339A GB531834A GB 531834 A GB531834 A GB 531834A GB 21583/39 A GB21583/39 A GB 21583/39A GB 2158339 A GB2158339 A GB 2158339A GB 531834 A GB531834 A GB 531834A
Authority
GB
United Kingdom
Prior art keywords
nacelle
shock
power unit
propeller
tanks
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
GB21583/39A
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
Priority to GB21583/39A priority Critical patent/GB531834A/en
Publication of GB531834A publication Critical patent/GB531834A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)

Abstract

531,834. Helicopters. POPOVICI, S. July 25,1939, No. 21583. [Class 4] A power unit 2 adapted to operate a propeller 36 is suspended by a ball and socket 3, 4 in the upper part of a dome-shaped nacelle 1 of a helicopter and is adjusted by hand-operated gearing 8-12 to move the axis of the propeller relatively to the nacelle. The power unit is enclosed in a part-spherical carrier 7. The engine may be provided with a resilient gimbal mounting. Fuel and oil tanks 14, 15 and oil coolers 16 are arranged symmetrically around the upper part of the nacelle and compressed air tanks 27 supplied by a compressor 26 have nozzles 28 arranged beneath steadying fins 23. The floor has pivoted sections, the pilot's seat 13 being carried by a section 29a adapted to fall downwardly in case of emergency. Fans 34 for removing hot air and exhaust gases, and a shock-absorber 33 for deadening the shock on landing, are provided.
GB21583/39A 1939-07-25 1939-07-25 Improved helicopter Expired GB531834A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB21583/39A GB531834A (en) 1939-07-25 1939-07-25 Improved helicopter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB21583/39A GB531834A (en) 1939-07-25 1939-07-25 Improved helicopter

Publications (1)

Publication Number Publication Date
GB531834A true GB531834A (en) 1941-01-13

Family

ID=10165346

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21583/39A Expired GB531834A (en) 1939-07-25 1939-07-25 Improved helicopter

Country Status (1)

Country Link
GB (1) GB531834A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2806662A (en) * 1954-03-05 1957-09-17 Meredith L Yonkers Helicopter with tiltable lift rotor and coaxial counter-torque rotor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2806662A (en) * 1954-03-05 1957-09-17 Meredith L Yonkers Helicopter with tiltable lift rotor and coaxial counter-torque rotor

Similar Documents

Publication Publication Date Title
US2486272A (en) Helicopter with antitorque reaction jet
CN201457738U (en) Dishing aircraft
GB891064A (en) New or improved aircraft propulsion installation
GB531834A (en) Improved helicopter
GB8406446D0 (en) Turbo-propellor aircraft engines
US3065936A (en) Aircraft having a power unit for the generation of lift for vertical takeoff
CN105966607A (en) Delta parallel mechanism-based unmanned aerial vehicle damping platform
GB521218A (en) Improvements in helicopters
US1885392A (en) Aeroplane
FR2349495A1 (en) Vtol aircraft with circular wing - forces air radially outwards over ring of aerofoil section
US1980980A (en) Aircraft having sustaining rotors and method of operating the same
GB796400A (en) Improvements relating to air intakes for aircraft power plant installations
GB588092A (en) Improvements in or relating to internal combustion turbine power plants
GB793928A (en) Improvements relating to methods and means of operating aircraft
GB348528A (en) Improvements relating to aeroplanes
GB422621A (en) Improvements in arrangements for starting flight requiring no gliding
GB898358A (en) Vertical take-off aircraft
GB942285A (en) Aircraft
GB920875A (en) Improvements in aircraft
GB823592A (en) Aircraft powered by turbo-prop engines
GB890703A (en) An improved tiltable pod for jet power units on aircraft
GB574873A (en) Propulsion of aircraft
SU62531A1 (en) The method of supplying a mixture of air and oxygen in the suit of the pilot
CN106342057C (en) unmanned helicopter
Sparks A New Technical Profession