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GB900939A - Improvements in or relating to helicopters - Google Patents

Improvements in or relating to helicopters

Info

Publication number
GB900939A
GB900939A GB1152961A GB1152961A GB900939A GB 900939 A GB900939 A GB 900939A GB 1152961 A GB1152961 A GB 1152961A GB 1152961 A GB1152961 A GB 1152961A GB 900939 A GB900939 A GB 900939A
Authority
GB
United Kingdom
Prior art keywords
blade
extension
helicopters
generator
nozzle
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
GB1152961A
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 GB1152961A priority Critical patent/GB900939A/en
Publication of GB900939A publication Critical patent/GB900939A/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
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • B64C27/16—Drive of rotors by means, e.g. propellers, mounted on rotor blades
    • B64C27/18—Drive of rotors by means, e.g. propellers, mounted on rotor blades the means being jet-reaction apparatus

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

900,939. Helicopters. WELLS, A. A. March 29, 1961, No. 11529/61. Class 4. A jet-propelled single-blade helicopter rotor comprises a blade 1, provided with a tip nozzle 5, and an extension 2 extending on opposite sides of the rotor axis X, the extension supporting a gas generator 3 from which gas is delivered to the nozzle 5 through the interior of blade 1 and extension 2. A controllable fuel supply 4 is provided between generator 3 and the helicopter body and it is stated that the blade may flap about two axes Y 1 and Y 2
GB1152961A 1961-03-29 1961-03-29 Improvements in or relating to helicopters Expired GB900939A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1152961A GB900939A (en) 1961-03-29 1961-03-29 Improvements in or relating to helicopters

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1152961A GB900939A (en) 1961-03-29 1961-03-29 Improvements in or relating to helicopters

Publications (1)

Publication Number Publication Date
GB900939A true GB900939A (en) 1962-07-11

Family

ID=9987910

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1152961A Expired GB900939A (en) 1961-03-29 1961-03-29 Improvements in or relating to helicopters

Country Status (1)

Country Link
GB (1) GB900939A (en)

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