GB527432A - All-wing airplane - Google Patents
All-wing airplaneInfo
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/04—Aircraft 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.
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)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2434785A (en) * | 2003-06-24 | 2007-08-08 | John Edward Randell | Twin fuselage aircraft |
-
1939
- 1939-03-30 GB GB9954/39A patent/GB527432A/en not_active Expired
Cited By (1)
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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