GB910350A - Improvements in and relating to aircraft wings incorporating power installations forpropulsion - Google Patents
Improvements in and relating to aircraft wings incorporating power installations forpropulsionInfo
- Publication number
- GB910350A GB910350A GB8682/59A GB868259A GB910350A GB 910350 A GB910350 A GB 910350A GB 8682/59 A GB8682/59 A GB 8682/59A GB 868259 A GB868259 A GB 868259A GB 910350 A GB910350 A GB 910350A
- Authority
- GB
- United Kingdom
- Prior art keywords
- tube
- spanwise
- cover
- attached
- jet
- 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
- 238000009434 installation Methods 0.000 title abstract 2
- 238000001816 cooling Methods 0.000 abstract 1
- 230000003014 reinforcing effect Effects 0.000 abstract 1
- 239000003351 stiffener 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
- B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
910,350. Jet-propulsion plant. ENGLISH ELECTRIC CO. Ltd. Feb. 26, 1960 [March 12, 1959], No. 8682/59. Addition to 854,859. Class 110 (3). [Also in Group XXXIII] In the jet-propulsion plant installation in an aircraft wing of the parent Specification, each chordwise extending square tube 119 (tube 159 of the parent Specification) is attached to a splitter plate 114 by vertical dowel pins 115 and by bolts 116 passing through the tube and through a strip 117 attached to the splitter plate 114. A further strip 118 connects each tube 119 to the adjacent ram-jet compartment cover 233. Spanwise extending stiffeners 227 on the adjacent turbo-jet compartment cover 230 are attached by fastenings 229 to brackets 231 secured to the tube by bolts 116, fastenings 229 allowing spanwise thermal expansion. A strip 228 attached to the cover 230 lies on a joggled part of cover 233, also to allow thermal expansion. The tube 119 has a reinforcing web 119a. The joints 273 between the covers 230, 233 and the forward ring portion allow spanwise thermal expansion of the covers. The cover 233 is a sandwich comprising spanwise corrugations, and the splitter plate 114 has vertical corrugations. The cooling air which flows rearwardly through tube 119 is tapped off to flow through these corrugations through ports 119b, 119c, respectively in the tube.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8682/59A GB910350A (en) | 1959-03-12 | 1959-03-12 | Improvements in and relating to aircraft wings incorporating power installations forpropulsion |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8682/59A GB910350A (en) | 1959-03-12 | 1959-03-12 | Improvements in and relating to aircraft wings incorporating power installations forpropulsion |
Publications (1)
Publication Number | Publication Date |
---|---|
GB910350A true GB910350A (en) | 1962-11-14 |
Family
ID=9857206
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8682/59A Expired GB910350A (en) | 1959-03-12 | 1959-03-12 | Improvements in and relating to aircraft wings incorporating power installations forpropulsion |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB910350A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4544115A (en) * | 1979-05-01 | 1985-10-01 | Edgley Aircraft Limited | Ducted propeller aircraft |
-
1959
- 1959-03-12 GB GB8682/59A patent/GB910350A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4544115A (en) * | 1979-05-01 | 1985-10-01 | Edgley Aircraft Limited | Ducted propeller aircraft |
US4657209A (en) * | 1979-05-01 | 1987-04-14 | Optica Industries Limited | Ducted propeller aircraft |
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