GB1041048A - Improvements in aircraft having jet-propulsion power-plants - Google Patents
Improvements in aircraft having jet-propulsion power-plantsInfo
- Publication number
- GB1041048A GB1041048A GB36415/62A GB3641562A GB1041048A GB 1041048 A GB1041048 A GB 1041048A GB 36415/62 A GB36415/62 A GB 36415/62A GB 3641562 A GB3641562 A GB 3641562A GB 1041048 A GB1041048 A GB 1041048A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuselage
- aircraft
- cowl
- jet
- plants
- 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
- 239000007789 gas Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
- B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
1,041,048. Aircraft power plant. VICKERSARMSTRONGS (AIRCRAFT) Ltd. Sept. 2, 1963 [Sept. 25, 1962], No; 36415/62. Heading B7G. [Also in Division F2] The aft end of an aircraft fuselage 10 (Fig. 2, not shown) carries a cowl 12 spaced from the fuselage to form an intake 15 for boundary layer air drawn from the fuselage surface, the cowl being extended laterally at 14 to enclose on each side of the fuselage a pair of gas-turbine engines 11 which discharge into a volute 19. A fan 18 is mounted within cowl 12 on each side of the fuselage and is driven by jet gases from volute 19 impinging on tip turbine blades 181 of the fan, whereby the fans draw fuselage boundary layer air through intake 15.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB36415/62A GB1041048A (en) | 1962-09-25 | 1962-09-25 | Improvements in aircraft having jet-propulsion power-plants |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB36415/62A GB1041048A (en) | 1962-09-25 | 1962-09-25 | Improvements in aircraft having jet-propulsion power-plants |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1041048A true GB1041048A (en) | 1966-09-01 |
Family
ID=10387929
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB36415/62A Expired GB1041048A (en) | 1962-09-25 | 1962-09-25 | Improvements in aircraft having jet-propulsion power-plants |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1041048A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2176570A (en) * | 1985-06-14 | 1986-12-31 | Messerschmitt Boelkow Blohm | Vortex generator and/or boundary-layer separator arrangements |
DE4310017A1 (en) * | 1993-03-27 | 1994-09-29 | Deutsche Aerospace | Transport aircraft having a blunt tail |
GB2285669A (en) * | 1994-01-13 | 1995-07-19 | Short Brothers Plc | Boundary layer control in aerodynamic structures |
CN104781143A (en) * | 2012-11-08 | 2015-07-15 | 斯内克马公司 | Aircraft propelled by a turbojet engine with contrarotating fans |
-
1962
- 1962-09-25 GB GB36415/62A patent/GB1041048A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2176570A (en) * | 1985-06-14 | 1986-12-31 | Messerschmitt Boelkow Blohm | Vortex generator and/or boundary-layer separator arrangements |
DE4310017A1 (en) * | 1993-03-27 | 1994-09-29 | Deutsche Aerospace | Transport aircraft having a blunt tail |
US5480110A (en) * | 1993-03-27 | 1996-01-02 | Daimler-Benz Aerospace Ag | Transport plane with stub tail |
GB2285669A (en) * | 1994-01-13 | 1995-07-19 | Short Brothers Plc | Boundary layer control in aerodynamic structures |
US5743493A (en) * | 1994-01-13 | 1998-04-28 | Short Brothers Plc | Boundary layer control in aerodynamic low drag structures |
GB2285669B (en) * | 1994-01-13 | 1998-06-10 | Short Brothers Plc | Boundary layer control in aerodynamic low drag structures |
CN104781143A (en) * | 2012-11-08 | 2015-07-15 | 斯内克马公司 | Aircraft propelled by a turbojet engine with contrarotating fans |
CN104781143B (en) * | 2012-11-08 | 2017-09-01 | 斯内克马公司 | The aircraft promoted by the turbojet of the fan with reversion |
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