GB739300A - Improvements relating to the exhaust cone assemblies of gas turbine engines - Google Patents

Improvements relating to the exhaust cone assemblies of gas turbine engines

Info

Publication number
GB739300A
GB739300A GB1844653A GB1844653A GB739300A GB 739300 A GB739300 A GB 739300A GB 1844653 A GB1844653 A GB 1844653A GB 1844653 A GB1844653 A GB 1844653A GB 739300 A GB739300 A GB 739300A
Authority
GB
United Kingdom
Prior art keywords
inner casing
diaphragm
gas turbine
spokes
casing
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
GB1844653A
Other languages
English (en)
Inventor
Horace Sinclair Rainbow
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
Priority to GB1844653A priority Critical patent/GB739300A/en
Priority to DEA20584A priority patent/DE952668C/de
Priority to FR1103224D priority patent/FR1103224A/fr
Publication of GB739300A publication Critical patent/GB739300A/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
    • F02K1/04—Mounting of an exhaust cone in the jet pipe
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30—Exhaust 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)
  • Supercharger (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
GB1844653A 1953-07-03 1953-07-03 Improvements relating to the exhaust cone assemblies of gas turbine engines Expired GB739300A (en)

Priority Applications (3)

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
DEA20584A DE952668C (de) 1953-07-03 1954-06-25 Auspuffkonus fuer Gasturbinen
FR1103224D FR1103224A (fr) 1953-07-03 1954-06-28 Perfectionnements au montage du cône d'échappement d'un moteur à turbine à gaz

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
GB739300A true GB739300A (en) 1955-10-26

Family

ID=10112568

Family Applications (1)

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

Country Status (3)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2902838A1 (fr) * 2006-06-26 2007-12-28 Snecma Sa Cone d'echappement pour la canalisation d'une veine de gaz a l'aval d'une turbine

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1069428B (de) * 1959-11-19 General Motors Corporation, Detroit, Mich. (V. St. A.) Gasturbine mit Lager und Labyrinthdichtung
DE1233209B (de) * 1957-12-26 1967-01-26 Gen Electric Gasturbinentriebwerk
DE1058794B (de) * 1958-10-04 1959-06-04 Her Majesty The Queen Verkleidung fuer das hintere Rahmengehaeuse eines Gasturbinentriebwerkes
GB946597A (en) * 1961-05-29 1964-01-15 Rolls Royce Fluid flow machine
DE4420973A1 (de) * 1994-06-16 1995-12-21 Abb Management Ag Wellendichtung einer thermischen Turbomaschine
FR3043138B1 (fr) * 2015-11-04 2019-09-13 Safran Aircraft Engines Tube de degazage et cone d'ejection pour une turbomachine, ainsi que leur outillage de montage

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1014336A (fr) * 1944-01-28 1952-08-13 United Aircraft Corp Turbine actionnée par des gaz chauds
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
FR2902838A1 (fr) * 2006-06-26 2007-12-28 Snecma Sa Cone d'echappement pour la canalisation d'une veine de gaz a l'aval d'une turbine
EP1873385A2 (fr) * 2006-06-26 2008-01-02 Snecma Cone d'échappement pour la canalisation d'une veine de gaz à l'aval d'une turbine
EP1873385A3 (fr) * 2006-06-26 2008-01-09 Snecma Cone d'échappement pour la canalisation d'une veine de gaz à l'aval d'une turbine
US7866162B2 (en) 2006-06-26 2011-01-11 Snecma Exhaust cone for channeling a stream of gas downstream from a turbine

Also Published As

Publication number Publication date
DE952668C (de) 1956-11-22
FR1103224A (fr) 1955-10-31

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