DE602008000360D1 - Leitschaufel eines Gebläses - Google Patents

Leitschaufel eines Gebläses

Info

Publication number
DE602008000360D1
DE602008000360D1 DE602008000360T DE602008000360T DE602008000360D1 DE 602008000360 D1 DE602008000360 D1 DE 602008000360D1 DE 602008000360 T DE602008000360 T DE 602008000360T DE 602008000360 T DE602008000360 T DE 602008000360T DE 602008000360 D1 DE602008000360 D1 DE 602008000360D1
Authority
DE
Germany
Prior art keywords
blower
guide vane
vane
guide
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.)
Active
Application number
DE602008000360T
Other languages
German (de)
English (en)
Inventor
Olivier Belmonte
Bengue Amadou Lamine M
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Publication of DE602008000360D1 publication Critical patent/DE602008000360D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00—Axial-flow pumps
    • F04D19/02—Multi-stage pumps
    • F04D19/022—Multi-stage pumps with concentric rows of vanes
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • F01D5/146—Shape, i.e. outer, aerodynamic form of blades with tandem configuration, split blades or slotted blades
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/326—Application in turbines in gas turbines to drive shrouded, low solidity propeller
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/327—Application in turbines in gas turbines to drive shrouded, high solidity propeller
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Architecture (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE602008000360T 2007-04-13 2008-03-25 Leitschaufel eines Gebläses Active DE602008000360D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0702682A FR2914943B1 (fr) 2007-04-13 2007-04-13 Aube de soufflante

Publications (1)

Publication Number Publication Date
DE602008000360D1 true DE602008000360D1 (de) 2010-01-21

Family

ID=38564352

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602008000360T Active DE602008000360D1 (de) 2007-04-13 2008-03-25 Leitschaufel eines Gebläses

Country Status (8)

Country Link
US (1) US8257023B2 (enExample)
EP (1) EP1980753B1 (enExample)
JP (1) JP2008261332A (enExample)
CN (1) CN101307776B (enExample)
CA (1) CA2628626C (enExample)
DE (1) DE602008000360D1 (enExample)
FR (1) FR2914943B1 (enExample)
RU (1) RU2486346C2 (enExample)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITTO20090522A1 (it) * 2009-07-13 2011-01-14 Avio Spa Turbomacchina con girante a segmenti palettati
US20120324901A1 (en) * 2011-06-23 2012-12-27 United Technologies Corporation Tandem fan-turbine rotor for a tip turbine engine
ITMI20120569A1 (it) * 2012-04-06 2013-10-07 Franco Tosi Meccanica S P A Stadio rotorico di turbina assiale a rapporto corda/passo migliorato
WO2015049548A1 (en) 2013-10-03 2015-04-09 Franco Tosi Meccanica S.P.A. Rotor stage of axial turbine with improved chord/pitch ratio
EP2977549B1 (fr) 2014-07-22 2017-05-31 Safran Aero Boosters SA Aubage de turbomachine axiale et turbomachine associée
EP2977548B1 (fr) 2014-07-22 2021-03-10 Safran Aero Boosters SA Aube et turbomachine associée
EP2977550B1 (fr) 2014-07-22 2017-05-31 Safran Aero Boosters SA Aube de turbomachine axiale et turbomachine associée
WO2016021555A1 (ja) * 2014-08-07 2016-02-11 三菱電機株式会社 軸流ファン、及び、その軸流ファンを有する空気調和機
RU2631850C2 (ru) * 2015-10-30 2017-09-26 Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" Рабочее колесо осевого компрессора газотурбинного двигателя
US10619483B2 (en) 2017-11-21 2020-04-14 United Technologies Corporation Partially shrouded gas turbine engine fan
FR3079007B1 (fr) * 2018-03-14 2020-11-20 Safran Aircraft Engines Ensemble pour une soufflante
FR3107078B1 (fr) * 2020-02-07 2023-01-13 Safran Helicopter Engines Aube de rotor pour une turbomachine

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB189131A (en) * 1921-11-16 1923-03-01 Rateau Soc Improvements in or relating to turbine blades
GB460781A (en) * 1935-08-06 1937-02-04 William Wycliffe Spooner Improvements in or relating to fans, rotors, and the like
US2509442A (en) * 1945-04-17 1950-05-30 Matheisel Rudolph Inverse rotor
US3044559A (en) * 1959-07-14 1962-07-17 Chajmik Joseph Propeller
JPS59183099A (ja) * 1983-03-31 1984-10-18 Nippon Denso Co Ltd 軸流フアン
JPH09133089A (ja) * 1995-11-09 1997-05-20 Fujita Corp 流体駆動装置
US6454535B1 (en) * 2000-10-31 2002-09-24 General Electric Company Blisk
US7216475B2 (en) * 2003-11-21 2007-05-15 General Electric Company Aft FLADE engine
US7144221B2 (en) * 2004-07-30 2006-12-05 General Electric Company Method and apparatus for assembling gas turbine engines
US7631484B2 (en) * 2006-03-13 2009-12-15 Rollin George Giffin High pressure ratio aft fan
US7758303B1 (en) * 2006-07-31 2010-07-20 General Electric Company FLADE fan with different inner and outer airfoil stagger angles at a shroud therebetween

Also Published As

Publication number Publication date
JP2008261332A (ja) 2008-10-30
US8257023B2 (en) 2012-09-04
US20090028717A1 (en) 2009-01-29
FR2914943B1 (fr) 2011-04-01
CA2628626A1 (fr) 2008-10-13
EP1980753A1 (fr) 2008-10-15
EP1980753B1 (fr) 2009-12-09
RU2008114256A (ru) 2009-10-20
CN101307776A (zh) 2008-11-19
CN101307776B (zh) 2011-09-21
CA2628626C (fr) 2014-12-23
RU2486346C2 (ru) 2013-06-27
FR2914943A1 (fr) 2008-10-17

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition