ATE425346T1 - Turbomaschinenverdichter - Google Patents

Turbomaschinenverdichter

Info

Publication number
ATE425346T1
ATE425346T1 AT06292027T AT06292027T ATE425346T1 AT E425346 T1 ATE425346 T1 AT E425346T1 AT 06292027 T AT06292027 T AT 06292027T AT 06292027 T AT06292027 T AT 06292027T AT E425346 T1 ATE425346 T1 AT E425346T1
Authority
AT
Austria
Prior art keywords
ferrules
annular
edges
turbo machine
machine compressor
Prior art date
Application number
AT06292027T
Other languages
German (de)
English (en)
Inventor
Castro Enrique Penalver
Frederic Gebbia
Original Assignee
Techspace Aero
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 Techspace Aero filed Critical Techspace Aero
Application granted granted Critical
Publication of ATE425346T1 publication Critical patent/ATE425346T1/de

Links

Classifications

    • 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
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/243—Flange connections; Bolting arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
AT06292027T 2006-12-22 2006-12-22 Turbomaschinenverdichter ATE425346T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP06292027A EP1936125B1 (fr) 2006-12-22 2006-12-22 Compresseur de turbomachine

Publications (1)

Publication Number Publication Date
ATE425346T1 true ATE425346T1 (de) 2009-03-15

Family

ID=37913167

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06292027T ATE425346T1 (de) 2006-12-22 2006-12-22 Turbomaschinenverdichter

Country Status (4)

Country Link
EP (1) EP1936125B1 (fr)
AT (1) ATE425346T1 (fr)
DE (1) DE602006005693D1 (fr)
ES (1) ES2323283T3 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201103583D0 (en) 2011-03-03 2011-04-13 Rolls Royce Plc Fan casing for a turbofan engine
US10100674B2 (en) 2012-11-15 2018-10-16 Safran Aero Boosters Sa Radial fixing and positioning flanges for shells of axial turbine compressor housings
EP2733314B1 (fr) * 2012-11-15 2017-04-05 Safran Aero Boosters SA Brides radiales de fixation et de positionnement pour viroles de carter de turbomachine axiale
FR3098241B1 (fr) * 2019-07-04 2021-06-25 Safran Aircraft Engines Tambour pour une turbomachine d’aeronef

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB960812A (en) 1963-04-08 1964-06-17 Rolls Royce Compressor for a gas turbine engine
US5462403A (en) 1994-03-21 1995-10-31 United Technologies Corporation Compressor stator vane assembly

Also Published As

Publication number Publication date
EP1936125A1 (fr) 2008-06-25
DE602006005693D1 (de) 2009-04-23
EP1936125B1 (fr) 2009-03-11
ES2323283T3 (es) 2009-07-10

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Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties