FR1103224A - Improvements in fitting the exhaust cone of a gas turbine engine - Google Patents

Improvements in fitting the exhaust cone of a gas turbine engine

Info

Publication number
FR1103224A
FR1103224A FR1103224DA FR1103224A FR 1103224 A FR1103224 A FR 1103224A FR 1103224D A FR1103224D A FR 1103224DA FR 1103224 A FR1103224 A FR 1103224A
Authority
FR
France
Prior art keywords
fitting
gas turbine
turbine engine
exhaust cone
cone
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
Other languages
French (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.)
Armstrong Siddeley Motors Ltd
Original Assignee
Armstrong Siddeley Motors 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 Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Application granted granted Critical
Publication of FR1103224A publication Critical patent/FR1103224A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/04Mounting of an exhaust cone in the jet pipe
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30Exhaust heads, chambers, or the like

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)
FR1103224D 1953-07-03 1954-06-28 Improvements in fitting the exhaust cone of a gas turbine engine Expired FR1103224A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1844653A GB739300A (en) 1953-07-03 1953-07-03 Improvements relating to the exhaust cone assemblies of gas turbine engines

Publications (1)

Publication Number Publication Date
FR1103224A true FR1103224A (en) 1955-10-31

Family

ID=10112568

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1103224D Expired FR1103224A (en) 1953-07-03 1954-06-28 Improvements in fitting the exhaust cone of a gas turbine engine

Country Status (3)

Country Link
DE (1) DE952668C (en)
FR (1) FR1103224A (en)
GB (1) GB739300A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1233209B (en) * 1957-12-26 1967-01-26 Gen Electric Gas turbine engine
FR3043138A1 (en) * 2015-11-04 2017-05-05 Snecma DEGASSING TUBE AND EJECTION CONE FOR A TURBOMACHINE, AND THEIR ASSEMBLY TOOLS

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1069428B (en) * 1959-11-19 General Motors Corporation, Detroit, Mich. (V. St. A.) Gas turbine with bearing and labyrinth seal
DE1058794B (en) * 1958-10-04 1959-06-04 Her Majesty The Queen Fairing for the rear frame housing of a gas turbine engine
GB946597A (en) * 1961-05-29 1964-01-15 Rolls Royce Fluid flow machine
DE4420973A1 (en) * 1994-06-16 1995-12-21 Abb Management Ag Axial gas turbine shaft seal for turbo engine
FR2902838B1 (en) * 2006-06-26 2013-03-15 Snecma EXHAUST CONE FOR THE PIPING OF A GAS VEIN AT THE END OF A TURBINE

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1014336A (en) * 1944-01-28 1952-08-13 United Aircraft Corp Turbine powered by hot gases
GB623615A (en) * 1947-05-06 1949-05-19 Frederick William Walton Morle Improvements in or relating to gas-turbine-engines

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1233209B (en) * 1957-12-26 1967-01-26 Gen Electric Gas turbine engine
FR3043138A1 (en) * 2015-11-04 2017-05-05 Snecma DEGASSING TUBE AND EJECTION CONE FOR A TURBOMACHINE, AND THEIR ASSEMBLY TOOLS
WO2017077219A1 (en) * 2015-11-04 2017-05-11 Safran Aircraft Engines Degassing tube and ejection cone for a turbine engine, as well as tool for assembly thereof
US11306679B2 (en) 2015-11-04 2022-04-19 Safran Aircraft Engines Degassing tube and ejection cone for a turbine engine, as well as tool for assembly thereof

Also Published As

Publication number Publication date
DE952668C (en) 1956-11-22
GB739300A (en) 1955-10-26

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