GB801832A - Fuselage structure for jet propelled aircraft - Google Patents
Fuselage structure for jet propelled aircraftInfo
- Publication number
- GB801832A GB801832A GB28522/56A GB2852256A GB801832A GB 801832 A GB801832 A GB 801832A GB 28522/56 A GB28522/56 A GB 28522/56A GB 2852256 A GB2852256 A GB 2852256A GB 801832 A GB801832 A GB 801832A
- Authority
- GB
- United Kingdom
- Prior art keywords
- longerons
- duct
- jet propelled
- secured
- 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
Links
- 238000005452 bending Methods 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)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Abstract
801,832. Jet propelled aircraft. FIAT SOC. PER AZIONI. Sept. 18, 1956 [Sept. 24, 1955], No. 28522/56. Class 4. A jet propelled aircraft having a single engine mounted in the tail comprises an inner air intake duct supplying air to the engine, longerons substantially radially spaced from the duct and connected thereto, the duct taking up torque stresses and the longerons bending stresses, and outer fairings secured to the longerons. As shown, the intake duct 1 is connected to longerons 3, 4 and a third similar longeron on the far side of the aircraft and not shown, by radial plates 6, 6<SP>1</SP>, and a third similar plate (not shown) respectively, each plate being secured to webs on the longeron and duct. Transverse bulkheads 8, 9, 10 and 11 are connected to the duct and the longerons. Auxiliary apparatus may be stowed in the compartments so formed, and fairings 12, 13 are releasably secured to the longerons for easy access. Four longerons may be used instead of three. A tubular section 14 is fitted on extensions of the longerons which are stayed by gussets 15. A tail section C is attached by sockets 17 fitting studs 16.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT801832X | 1955-09-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB801832A true GB801832A (en) | 1958-09-24 |
Family
ID=11316891
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB28522/56A Expired GB801832A (en) | 1955-09-24 | 1956-09-18 | Fuselage structure for jet propelled aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB801832A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3724785A (en) * | 1970-07-04 | 1973-04-03 | Dornier Ag | Arrangement of jet lift engines in aircraft |
EP0849165A3 (en) * | 1996-12-18 | 2000-09-13 | British Aerospace Public Limited Company | Aircraft structure and powerplants for use therein |
FR2934563A1 (en) * | 2008-08-04 | 2010-02-05 | Airbus France | Sailwing for airplane, has upper beam including front end and median part respectively connected to two frames, and hooking pylon for hooking propulsion engine on fuselage, where propulsion engine is fixed on pylon |
-
1956
- 1956-09-18 GB GB28522/56A patent/GB801832A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3724785A (en) * | 1970-07-04 | 1973-04-03 | Dornier Ag | Arrangement of jet lift engines in aircraft |
EP0849165A3 (en) * | 1996-12-18 | 2000-09-13 | British Aerospace Public Limited Company | Aircraft structure and powerplants for use therein |
FR2934563A1 (en) * | 2008-08-04 | 2010-02-05 | Airbus France | Sailwing for airplane, has upper beam including front end and median part respectively connected to two frames, and hooking pylon for hooking propulsion engine on fuselage, where propulsion engine is fixed on pylon |
US8251310B2 (en) | 2008-08-04 | 2012-08-28 | Airbus Operations Sas | Sail wing aircraft which includes an engine mounted on a pylon |
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