GB359087A - Improvements in or relating to aeroplanes or like aircraft - Google Patents

Improvements in or relating to aeroplanes or like aircraft

Info

Publication number
GB359087A
GB359087A GB23323/30A GB2332330A GB359087A GB 359087 A GB359087 A GB 359087A GB 23323/30 A GB23323/30 A GB 23323/30A GB 2332330 A GB2332330 A GB 2332330A GB 359087 A GB359087 A GB 359087A
Authority
GB
United Kingdom
Prior art keywords
plane
fuselages
planes
propellers
main
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
GB23323/30A
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.)
HANS ARMIN VON DER MUEHLEN
Original Assignee
HANS ARMIN VON DER MUEHLEN
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 HANS ARMIN VON DER MUEHLEN filed Critical HANS ARMIN VON DER MUEHLEN
Priority to GB23323/30A priority Critical patent/GB359087A/en
Publication of GB359087A publication Critical patent/GB359087A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/04Aircraft not otherwise provided for having multiple fuselages or tail booms

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Earth Drilling (AREA)

Abstract

359,087. Supporting, propelling, and controlling aeroplanes. MUEHLEN, H. A. VON DER, 54, Cambridge Terrace, London. Aug. 2, 1930, No. 23323. [Class 4.] An aeroplane has a main supporting plane 2 secured to two or more fuselages 1 which are braced together by two additional planes 3, 4 arranged below and to the front and rear of the main plane. The rear ends of the fuselages are connected by a stabilizing plane fitted with an elevator 8 and carrying a series of fins and rudders. Hinged flaps 5 movable in unison are provided on the planes 3, 4 for varying the lift. Pusher propellers 12, 13 are provided at the trailing edges of the planes 2, 3 and tractor propellers at the leading edge of the plane 4. Propellers may be provided at the forward ends of the fuselages and the plane 2. The central section of the plane 2 constitutes the main passenger accommodation and access thereto is obtained by stairways leading from doors in the fuselages. The fuselages have lightening spaces 11. The landing gear comprises tandem wheels well forward beneath and partially housed in each fuselage and single wheels spaced sufficiently to the rear to prevent the tail from touching the ground during a normal landing. A three-fuselage machine is described in which the front auxiliary plane does not extend beyond the outer fuselages.
GB23323/30A 1930-08-02 1930-08-02 Improvements in or relating to aeroplanes or like aircraft Expired GB359087A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB23323/30A GB359087A (en) 1930-08-02 1930-08-02 Improvements in or relating to aeroplanes or like aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB23323/30A GB359087A (en) 1930-08-02 1930-08-02 Improvements in or relating to aeroplanes or like aircraft

Publications (1)

Publication Number Publication Date
GB359087A true GB359087A (en) 1931-10-22

Family

ID=10193747

Family Applications (1)

Application Number Title Priority Date Filing Date
GB23323/30A Expired GB359087A (en) 1930-08-02 1930-08-02 Improvements in or relating to aeroplanes or like aircraft

Country Status (1)

Country Link
GB (1) GB359087A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2460804A (en) * 1944-05-22 1949-02-08 Samuel R Brentnall Auxiliary control surface for highspeed aircraft
US2957647A (en) * 1958-02-24 1960-10-25 Glenn B Shew High-lift aircraft
US3041014A (en) * 1957-05-13 1962-06-26 Gerin Jacques Jean-Marie Jules High lift, highly extensible device for aircraft wings

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2460804A (en) * 1944-05-22 1949-02-08 Samuel R Brentnall Auxiliary control surface for highspeed aircraft
US3041014A (en) * 1957-05-13 1962-06-26 Gerin Jacques Jean-Marie Jules High lift, highly extensible device for aircraft wings
US2957647A (en) * 1958-02-24 1960-10-25 Glenn B Shew High-lift aircraft

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