GB910350A - Improvements in and relating to aircraft wings incorporating power installations forpropulsion - Google Patents

Improvements in and relating to aircraft wings incorporating power installations forpropulsion

Info

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
Application number
GB8682/59A
Inventor
Raymond Frederick Creasey
Bernard Oliver Heath
Sidney Walmsley
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
English Electric Co Ltd
Original Assignee
English Electric Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by English Electric Co Ltd filed Critical English Electric Co Ltd
Priority to GB8682/59A priority Critical patent/GB910350A/en
Publication of GB910350A publication Critical patent/GB910350A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/16Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18Aircraft 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.
GB8682/59A 1959-03-12 1959-03-12 Improvements in and relating to aircraft wings incorporating power installations forpropulsion Expired GB910350A (en)

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)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4544115A (en) * 1979-05-01 1985-10-01 Edgley Aircraft Limited Ducted propeller aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
GB1024952A (en) Diverter valve assembly
GB1214892A (en) Improvements in nuclear power plant suitable for use in aircraft propulsion systems
GB1483813A (en) Aircraft multi-engine configuration
US3212731A (en) Fan powered aircraft
GB1411601A (en) Ducted fan gas turbine engine supported by an aircraft wing mainspar
GB923557A (en) Improvements in thrust diverting means for vtol and stol aircraft
GB1166396A (en) Improvements in Power Plant with Thrust Reverser.
GB910350A (en) Improvements in and relating to aircraft wings incorporating power installations forpropulsion
GB861480A (en) Improvements in aircraft
GB817507A (en) Improvements in or relating to aircraft
US2956759A (en) Aircraft wings incorporating power installation for propulsion
GB882424A (en) Improvements in or relating to aircraft jet propulsion apparatus
GB877838A (en) Improvements relating to gas turbine engine air intakes
GB921013A (en) Aircraft
GB1364692A (en) Thrust spoilers of ducted fan gas turbine engines
GB851379A (en) Aircraft
GB1030521A (en) Mounting arrangement for gas turbine engines in aircraft
GB1195027A (en) Improvements relating to Cowls for Turbo-Fan Aircraft Engines.
GB629143A (en) Improvements in or relating to aircraft power unit installations
GB844748A (en) Improvements in and relating to aircraft wings incorporating a power installation for propulsion
GB847868A (en) Improvements relating to vertical take-off aircraft
GB1253834A (en) Improvements relating to jet-propelled aeroplanes
DYBAN et al. High-temperature gas turbine blade
GB756319A (en) Improvements in aircraft
GB890703A (en) An improved tiltable pod for jet power units on aircraft