GB495176A - Improvements in rotating-wing aircraft with side-by-side rotors - Google Patents

Improvements in rotating-wing aircraft with side-by-side rotors

Info

Publication number
GB495176A
GB495176A GB21163/38A GB2116338A GB495176A GB 495176 A GB495176 A GB 495176A GB 21163/38 A GB21163/38 A GB 21163/38A GB 2116338 A GB2116338 A GB 2116338A GB 495176 A GB495176 A GB 495176A
Authority
GB
United Kingdom
Prior art keywords
fuselage
rotating
rotors
aircraft
wing aircraft
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
GB21163/38A
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.)
HENRICH FOCKE PROF DIPL ING
Original Assignee
HENRICH FOCKE PROF DIPL ING
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 HENRICH FOCKE PROF DIPL ING filed Critical HENRICH FOCKE PROF DIPL ING
Publication of GB495176A publication Critical patent/GB495176A/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
    • B64C27/08—Helicopters with two or more rotors

Landscapes

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

Abstract

495,176. Aircraft with rotary-wing systems. FOCKE, H. July 16, 1938, No. 21163. Convention date, May 24. [Class 4] In aircraft having side-by-side rotors, a separate fuselage d is located under the axis of rotation of each rotor and the fuselages are connected by structural parts e, e<1> which may be of streamlined cross - section. Each rotor is driven by mechanism arranged in its appropriate fuselage and synchronized by mechanical, electrical, or hydraulic means. Each fuselage has a single, preferably, retractable landing-wheel and each fuselage may be constructed as a boat hull.
GB21163/38A 1938-05-24 1938-07-16 Improvements in rotating-wing aircraft with side-by-side rotors Expired GB495176A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE495176X 1938-05-24

Publications (1)

Publication Number Publication Date
GB495176A true GB495176A (en) 1938-11-08

Family

ID=6544848

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21163/38A Expired GB495176A (en) 1938-05-24 1938-07-16 Improvements in rotating-wing aircraft with side-by-side rotors

Country Status (1)

Country Link
GB (1) GB495176A (en)

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