GB585557A - Improvements in jet propelled aircraft - Google Patents

Improvements in jet propelled aircraft

Info

Publication number
GB585557A
GB585557A GB5184/45A GB518445A GB585557A GB 585557 A GB585557 A GB 585557A GB 5184/45 A GB5184/45 A GB 5184/45A GB 518445 A GB518445 A GB 518445A GB 585557 A GB585557 A GB 585557A
Authority
GB
United Kingdom
Prior art keywords
fuselage
jet
nozzles
aircraft
power unit
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
GB5184/45A
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.)
JOHN VIVIAN STANBURY
Hawker Aircraft Ltd
Original Assignee
JOHN VIVIAN STANBURY
Hawker Aircraft 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 JOHN VIVIAN STANBURY, Hawker Aircraft Ltd filed Critical JOHN VIVIAN STANBURY
Priority to GB5184/45A priority Critical patent/GB585557A/en
Publication of GB585557A publication Critical patent/GB585557A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/52—Nozzles specially constructed for positioning adjacent to another nozzle or to a fixed member, e.g. fairing
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

585,557. Propelling aircraft. HAWKER AIRCRAFT, Ltd., and STANBURY, J. V. March 1, 1945, No. 5184. [Class 4] In a jet-propelled aircraft the power unit or units are housed in the fuselage and connected by rearwardly extending divergent jet pipes to jet nozzles located alongside the fuselage and preferably in the neighbourhood of the trailing edges of the wing roots. Fig. shows an arrangement in which a single power unit 12 is located on the axis of the fuselage 14, the jet pipe being divided into two branches 16 terminating in nozzles 18 at the trailing edges 20 of the wing roots. The air inlets 30 are located in the leading edges of the wing roots. In the arrangement according to Fig. 7 two power units 36 are disposed side by side in the fuselage, each being provided with a slightly curved jet pipe 38. According to a further embodiment, Fig. 8 (not shown), the nozzles are located one in the upper surface and the other in the lower surface of the fuselage: Such an arrangement may be combined with that of Fig. 1 or Fig. 7 to provide four nozzles, or the'jet pipe from a single power unit may be divided into three or more branches instead of being bifurcated.
GB5184/45A 1945-03-01 1945-03-01 Improvements in jet propelled aircraft Expired GB585557A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB5184/45A GB585557A (en) 1945-03-01 1945-03-01 Improvements in jet propelled aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5184/45A GB585557A (en) 1945-03-01 1945-03-01 Improvements in jet propelled aircraft

Publications (1)

Publication Number Publication Date
GB585557A true GB585557A (en) 1947-02-11

Family

ID=9791288

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5184/45A Expired GB585557A (en) 1945-03-01 1945-03-01 Improvements in jet propelled aircraft

Country Status (1)

Country Link
GB (1) GB585557A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2641422A (en) * 1947-02-18 1953-06-09 Rolls Royce Exhaust system for gas turbine engines in aircraft
US2696079A (en) * 1950-04-17 1954-12-07 Peter G Kappus Dual jet aircraft power plant
US3003316A (en) * 1953-02-10 1961-10-10 Rolls Royce Cooling means for forked exhaust ducts of gas turbine engines

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2641422A (en) * 1947-02-18 1953-06-09 Rolls Royce Exhaust system for gas turbine engines in aircraft
US2696079A (en) * 1950-04-17 1954-12-07 Peter G Kappus Dual jet aircraft power plant
US3003316A (en) * 1953-02-10 1961-10-10 Rolls Royce Cooling means for forked exhaust ducts of gas turbine engines

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