GB762785A - Improvements relating to aircraft - Google Patents
Improvements relating to aircraftInfo
- Publication number
- GB762785A GB762785A GB4436/54A GB443654A GB762785A GB 762785 A GB762785 A GB 762785A GB 4436/54 A GB4436/54 A GB 4436/54A GB 443654 A GB443654 A GB 443654A GB 762785 A GB762785 A GB 762785A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuselage
- engine
- entrant
- frames
- bomb
- 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
- 239000000446 fuel 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)
- Mutual Connection Of Rods And Tubes (AREA)
- Toys (AREA)
- Connection Of Plates (AREA)
Abstract
762,785. Aircraft framework. FAIREY AVIATION CO., Ltd. May 13, 1955 [Feb. 15, 1954], No. 4436/54. Class 4. [Also in Group XXVI] The fuselage of a twin-engined jetpropelled aircraft includes a number of transverse frames each shaped with re-entrant portions of its opposite sides curved convexly inwards with the engines mounted on either side of the fuselage frames partly within the re-entrant portions. The fuselage comprises upper and lower longerons 1 and 2 and longitudinally spaced frames each comprising a top piece 3 secured to longeron 1 and a plate 4 having flanges secured to longerons 1 and 2 and sides of re-entrant shape as shown at 5. The bottom of the fuselage is formed as a bomb-bay 6 closed by doors 7. The wings comprise two main spars 10 which are curved upwardly within the fuselage above the bomb-bay and connected together. Each engine 13 is carried by a mounting structure 16, 17 pivotally connected to the respective wing at 15 and attached to the engine at 18 and 19 whereby the engine may be swung outwardly from the re-entrant portion 5 for easy removal by a sling attached to slinging points 24. A releasable connection 20, 21 is provided between the fuselage and the engine and a conduit 22 contains easily detachable fuel and electrical connections. A hinged fairing 26 completes the outer profile between the fuselage and the respective wing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4436/54A GB762785A (en) | 1954-02-15 | 1954-02-15 | Improvements relating to aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4436/54A GB762785A (en) | 1954-02-15 | 1954-02-15 | Improvements relating to aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB762785A true GB762785A (en) | 1956-12-05 |
Family
ID=9777142
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4436/54A Expired GB762785A (en) | 1954-02-15 | 1954-02-15 | Improvements relating to aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB762785A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2008480A1 (en) * | 1968-05-14 | 1970-01-23 | British Aircraft Corp Ltd | |
US4213585A (en) * | 1978-05-22 | 1980-07-22 | The Boeing Company | Mounting system for a wing mounted aircraft engine |
US4603821A (en) * | 1983-12-30 | 1986-08-05 | The Boeing Company | System for mounting a jet engine |
EP1975064A1 (en) * | 2007-03-28 | 2008-10-01 | EADS Deutschland GmbH | Aircraft |
US20180170563A1 (en) * | 2016-12-20 | 2018-06-21 | Airbus Operations Sas | Rear portion of an aircraft comprising a fuselage frame supporting two partly buried engines |
-
1954
- 1954-02-15 GB GB4436/54A patent/GB762785A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2008480A1 (en) * | 1968-05-14 | 1970-01-23 | British Aircraft Corp Ltd | |
US4213585A (en) * | 1978-05-22 | 1980-07-22 | The Boeing Company | Mounting system for a wing mounted aircraft engine |
US4603821A (en) * | 1983-12-30 | 1986-08-05 | The Boeing Company | System for mounting a jet engine |
EP1975064A1 (en) * | 2007-03-28 | 2008-10-01 | EADS Deutschland GmbH | Aircraft |
US20180170563A1 (en) * | 2016-12-20 | 2018-06-21 | Airbus Operations Sas | Rear portion of an aircraft comprising a fuselage frame supporting two partly buried engines |
FR3060531A1 (en) * | 2016-12-20 | 2018-06-22 | Airbus Operations | REAR AIRCRAFT PART COMPRISING A FUSELAGE FRAME SUPPORTING TWO PARTIALLY BITTED ENGINES |
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