GB918091A - Improvements in or relating to gas-turbine engines - Google Patents

Improvements in or relating to gas-turbine engines

Info

Publication number
GB918091A
GB918091A GB2925659A GB2925659A GB918091A GB 918091 A GB918091 A GB 918091A GB 2925659 A GB2925659 A GB 2925659A GB 2925659 A GB2925659 A GB 2925659A GB 918091 A GB918091 A GB 918091A
Authority
GB
United Kingdom
Prior art keywords
relating
gas
turbine engines
aug
turbine
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
GB2925659A
Inventor
David Omri Davies
Hugh Francis Cantwell
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 GB2925659A priority Critical patent/GB918091A/en
Publication of GB918091A publication Critical patent/GB918091A/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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • F02K1/16—Control or regulation conjointly with another control

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)

Abstract

918,091. Lubricating. ROLLS-ROYCE Ltd. Aug. 8, 1960 [Aug. 26, 1959], No. 29256/59. Class 12 (3). [Also in Groups XXVI and XXIX] Compressed air from the space between the control valves 33, 34 of an air turbine is used to pressurize the lubricating oil reservoir to force oil through the spring loaded piston valve 55 to a duct 56 leading to a bearing 57. A valve 58 connects the reservoir to atmosphere when the turbine is shut down.
GB2925659A 1959-08-26 1959-08-26 Improvements in or relating to gas-turbine engines Expired GB918091A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2925659A GB918091A (en) 1959-08-26 1959-08-26 Improvements in or relating to gas-turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2925659A GB918091A (en) 1959-08-26 1959-08-26 Improvements in or relating to gas-turbine engines

Publications (1)

Publication Number Publication Date
GB918091A true GB918091A (en) 1963-02-13

Family

ID=10288624

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2925659A Expired GB918091A (en) 1959-08-26 1959-08-26 Improvements in or relating to gas-turbine engines

Country Status (1)

Country Link
GB (1) GB918091A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2241540A (en) * 1990-02-26 1991-09-04 Gen Electric Jet propulsion nozzle having variable contour exhaust flap
US5201800A (en) * 1990-02-26 1993-04-13 General Electric Company Method for discharging combustion gases from an exhaust nozzle

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2241540A (en) * 1990-02-26 1991-09-04 Gen Electric Jet propulsion nozzle having variable contour exhaust flap
US5103639A (en) * 1990-02-26 1992-04-14 General Electric Company Exhaust nozzle having variable contour exhaust flap
US5201800A (en) * 1990-02-26 1993-04-13 General Electric Company Method for discharging combustion gases from an exhaust nozzle

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