FR1452558A - Nozzle nozzle applicable, in particular, to gas turbine engines - Google Patents

Nozzle nozzle applicable, in particular, to gas turbine engines

Info

Publication number
FR1452558A
FR1452558A FR37458A FR37458A FR1452558A FR 1452558 A FR1452558 A FR 1452558A FR 37458 A FR37458 A FR 37458A FR 37458 A FR37458 A FR 37458A FR 1452558 A FR1452558 A FR 1452558A
Authority
FR
France
Prior art keywords
nozzle
gas turbine
turbine engines
applicable
nozzle applicable
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
FR37458A
Other languages
French (fr)
Inventor
Francis Jeffrey Colville
Norman Roberts
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
Priority claimed from GB45424/64A external-priority patent/GB1015450A/en
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to FR37458A priority Critical patent/FR1452558A/en
Application granted granted Critical
Publication of FR1452558A publication Critical patent/FR1452558A/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
    • F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
    • F02K1/085—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone by transversely deforming an internal member
    • 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
    • F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR37458A 1964-11-06 1965-11-05 Nozzle nozzle applicable, in particular, to gas turbine engines Expired FR1452558A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR37458A FR1452558A (en) 1964-11-06 1965-11-05 Nozzle nozzle applicable, in particular, to gas turbine engines

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB45424/64A GB1015450A (en) 1964-11-06 1964-11-06 Jet nozzle
FR37458A FR1452558A (en) 1964-11-06 1965-11-05 Nozzle nozzle applicable, in particular, to gas turbine engines

Publications (1)

Publication Number Publication Date
FR1452558A true FR1452558A (en) 1966-02-25

Family

ID=26167243

Family Applications (1)

Application Number Title Priority Date Filing Date
FR37458A Expired FR1452558A (en) 1964-11-06 1965-11-05 Nozzle nozzle applicable, in particular, to gas turbine engines

Country Status (1)

Country Link
FR (1) FR1452558A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2333964A1 (en) * 1975-12-01 1977-07-01 Gen Electric PROPULSION TUBE FOR GAS TURBINE ENGINE
EP1619489A1 (en) * 2004-07-19 2006-01-25 Techspace Aero Test equipment for the development of an aircraft gas turbine engine
CN114718757A (en) * 2022-03-23 2022-07-08 西北工业大学 Design scheme of tail spray pipe of micro turbojet engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2333964A1 (en) * 1975-12-01 1977-07-01 Gen Electric PROPULSION TUBE FOR GAS TURBINE ENGINE
EP1619489A1 (en) * 2004-07-19 2006-01-25 Techspace Aero Test equipment for the development of an aircraft gas turbine engine
CN114718757A (en) * 2022-03-23 2022-07-08 西北工业大学 Design scheme of tail spray pipe of micro turbojet engine

Similar Documents

Publication Publication Date Title
FR1382232A (en) Improvements to gas turbine engines
FR1477813A (en) Combustion apparatus, applicable to gas turbine engines
CH452998A (en) Gas turbine
CH468557A (en) Gas turbine engine
FR1507523A (en) Gas turbine engine improvements
FR1510762A (en) Gas turbine engine
CH402517A (en) Gas turbine jet engine
FR1377199A (en) Gas turbine engine
FR1452558A (en) Nozzle nozzle applicable, in particular, to gas turbine engines
FR1392694A (en) Improvements made to engine gas autogenerators, in particular free piston autogenerators
CH456251A (en) Control device for gas turbine engines
FR1259348A (en) Gas turbine engine improvements
FR1429834A (en) Improvements made to blades, particularly for gas turbine engines
FR1446066A (en) Improvements to bearings, especially for gas turbine engines
FR1384980A (en) Improvements to bearings intended, in particular, for gas turbine engines
FR1285627A (en) Gas turbine engine group
FR1496841A (en) Gas turbine engine improvements
FR1492590A (en) Gas turbine engine improvements
FR1355379A (en) Gas turbine engine improvements
FR1437136A (en) Development of gas turbine engines
FR1379573A (en) Improvements to gas turbine engines
FR1412683A (en) Gas turbine engine
FR1467556A (en) Gas turbine engine
FR1470246A (en) Gas turbine engine
FR1432316A (en) Improvements to devices intended for cooling, in particular for gas turbine engine flame tubes