GB527432A - All-wing airplane - Google Patents

All-wing airplane

Info

Publication number
GB527432A
GB527432A GB9954/39A GB995439A GB527432A GB 527432 A GB527432 A GB 527432A GB 9954/39 A GB9954/39 A GB 9954/39A GB 995439 A GB995439 A GB 995439A GB 527432 A GB527432 A GB 527432A
Authority
GB
United Kingdom
Prior art keywords
wing section
central wing
hatch
fuselages
passenger
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
GB9954/39A
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.)
BURNELLI AIRCRAFT CORP
Original Assignee
BURNELLI AIRCRAFT CORP
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 BURNELLI AIRCRAFT CORP filed Critical BURNELLI AIRCRAFT CORP
Publication of GB527432A publication Critical patent/GB527432A/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)
  • Vehicle Waterproofing, Decoration, And Sanitation Devices (AREA)

Abstract

527,432. Twin, fuselage aeroplanes. BURNELLI AIRCRAFT CORPORATION. March 30, 1939, No. 9954. Convention date, April 7, 1938. [Class 4] An aeroplane comprises a central wing section affording the major lift, twin fuselages, and lateral wing sections, engines being mounted at the leading edge of the central wing section, and doors for passenger use being provided in the fuselages rearwardly of the central wing section. Passenger accommodation is provided in the central wing section and in the fuselages. In the form shown, the central wing section 1 merges into rearwardly extending hollow booms 6 and 7 that carry the empennage 8 and serve as passenger passageways, being provided with doors 9 and 10. Seating accommodation is indicated at 11, toilet facilities at 15 and 16 and ventilation means at V. The pilot's cockpit 17 has a hatch 18 disposed above the engines to permit of lateral vision. The hatch may be telescopic so that the pilot may raise the hatch and stand or raise his seat to increase; his range of vision. Two sets of landing wheels, 21 and 24, are shown having oleo struts and retracting means. The outer wing sections 2 and 3 are provided with ailerons 29 and flaps, and fuel may be carried in the tanks 31.
GB9954/39A 1938-04-07 1939-03-30 All-wing airplane Expired GB527432A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US527432XA 1938-04-07 1938-04-07

Publications (1)

Publication Number Publication Date
GB527432A true GB527432A (en) 1940-10-09

Family

ID=21979615

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9954/39A Expired GB527432A (en) 1938-04-07 1939-03-30 All-wing airplane

Country Status (1)

Country Link
GB (1) GB527432A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2434785A (en) * 2003-06-24 2007-08-08 John Edward Randell Twin fuselage aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2434785A (en) * 2003-06-24 2007-08-08 John Edward Randell Twin fuselage aircraft

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