GB735645A - Improvements relating to aircraft reaction propulsion units and installations - Google Patents

Improvements relating to aircraft reaction propulsion units and installations

Info

Publication number
GB735645A
GB735645A GB1615752A GB1615752A GB735645A GB 735645 A GB735645 A GB 735645A GB 1615752 A GB1615752 A GB 1615752A GB 1615752 A GB1615752 A GB 1615752A GB 735645 A GB735645 A GB 735645A
Authority
GB
United Kingdom
Prior art keywords
installations
gas flow
improvements relating
propulsion units
guide vanes
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
GB1615752A
Inventor
Harry Pearson
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB1615752A priority Critical patent/GB735645A/en
Publication of GB735645A publication Critical patent/GB735645A/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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow

Landscapes

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

Abstract

735,645. Jet propulsion plant. ROLLSROYCE, Ltd. Sept. 24, 1953 [June 26, 1952], No. 16157/52. Class 110 (3). [Also in Group XXXIII] Part of the wall of the jet pipe 13 is defined by the inner edges of a series of axially-spaced annular or part annular guide vanes 15 of concave section the inner edges being directed upstream relative to the gas flow and the outer edges being directed forwardly with respect to the direction of flight. Compressed air from the engine may be supplied by a pipe 28 to a body 22 with outlets to direct radial air streams towards the guide vanes to induce a gas flow therethrough. The fairing surrounding the vanes is provided with ports 19 which may be opened or closed by a ported sleeve 20 operable by gearing 25, 26.
GB1615752A 1952-06-26 1952-06-26 Improvements relating to aircraft reaction propulsion units and installations Expired GB735645A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1615752A GB735645A (en) 1952-06-26 1952-06-26 Improvements relating to aircraft reaction propulsion units and installations

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1615752A GB735645A (en) 1952-06-26 1952-06-26 Improvements relating to aircraft reaction propulsion units and installations

Publications (1)

Publication Number Publication Date
GB735645A true GB735645A (en) 1955-08-24

Family

ID=10072191

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1615752A Expired GB735645A (en) 1952-06-26 1952-06-26 Improvements relating to aircraft reaction propulsion units and installations

Country Status (1)

Country Link
GB (1) GB735645A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2865169A (en) * 1956-02-15 1958-12-23 United Aircraft Corp Jet exhaust nozzle
US3031156A (en) * 1957-11-08 1962-04-24 Bristol Siddeley Engines Ltd Exhaust systems for jet propulsion engines
US3224190A (en) * 1959-02-11 1965-12-21 Daimler Benz Ag Jet power plant particularly for aircraft

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2865169A (en) * 1956-02-15 1958-12-23 United Aircraft Corp Jet exhaust nozzle
US3031156A (en) * 1957-11-08 1962-04-24 Bristol Siddeley Engines Ltd Exhaust systems for jet propulsion engines
US3224190A (en) * 1959-02-11 1965-12-21 Daimler Benz Ag Jet power plant particularly for aircraft

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