FR2184021B1 - - Google Patents

Info

Publication number
FR2184021B1
FR2184021B1 FR7316760A FR7316760A FR2184021B1 FR 2184021 B1 FR2184021 B1 FR 2184021B1 FR 7316760 A FR7316760 A FR 7316760A FR 7316760 A FR7316760 A FR 7316760A FR 2184021 B1 FR2184021 B1 FR 2184021B1
Authority
FR
France
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
FR7316760A
Other versions
FR2184021A1 (fr
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
Publication of FR2184021A1 publication Critical patent/FR2184021A1/fr
Application granted granted Critical
Publication of FR2184021B1 publication Critical patent/FR2184021B1/fr
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
    • F02K1/09—Varying effective area of jet pipe or nozzle by axially moving an external member, e.g. a shroud
    • 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
    • F02K1/64—Reversing fan flow
    • F02K1/66—Reversing fan flow using reversing fan blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Control Of Turbines (AREA)
FR7316760A 1972-05-09 1973-05-09 Expired FR2184021B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2165972A GB1418905A (en) 1972-05-09 1972-05-09 Gas turbine engines

Publications (2)

Publication Number Publication Date
FR2184021A1 FR2184021A1 (fr) 1973-12-21
FR2184021B1 true FR2184021B1 (fr) 1977-12-30

Family

ID=10166655

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7316760A Expired FR2184021B1 (fr) 1972-05-09 1973-05-09

Country Status (5)

Country Link
US (1) US3820719A (fr)
JP (1) JPS5621901B2 (fr)
DE (1) DE2323380C3 (fr)
FR (1) FR2184021B1 (fr)
GB (1) GB1418905A (fr)

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* Cited by examiner, † Cited by third party
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US11486311B2 (en) 2007-08-01 2022-11-01 Raytheon Technologies Corporation Turbine section of high bypass turbofan
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Also Published As

Publication number Publication date
DE2323380A1 (de) 1973-11-29
US3820719A (en) 1974-06-28
GB1418905A (en) 1975-12-24
FR2184021A1 (fr) 1973-12-21
JPS4961510A (fr) 1974-06-14
DE2323380C3 (de) 1981-09-10
JPS5621901B2 (fr) 1981-05-22
DE2323380B2 (de) 1980-12-18

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