ATE467088T1 - Durchflussbegrenzer mit geteilten schaufeln - Google Patents

Durchflussbegrenzer mit geteilten schaufeln

Info

Publication number
ATE467088T1
ATE467088T1 AT04257871T AT04257871T ATE467088T1 AT E467088 T1 ATE467088 T1 AT E467088T1 AT 04257871 T AT04257871 T AT 04257871T AT 04257871 T AT04257871 T AT 04257871T AT E467088 T1 ATE467088 T1 AT E467088T1
Authority
AT
Austria
Prior art keywords
aft
ring
gas
flow register
split blades
Prior art date
Application number
AT04257871T
Other languages
English (en)
Inventor
Jennifer A Coull
John Nikkanen
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of ATE467088T1 publication Critical patent/ATE467088T1/de

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/26—Controlling the air flow
    • 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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
    • 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
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/075—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type controlling flow ratio between flows
    • 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
    • F05D2250/00—Geometry
    • F05D2250/40—Movement of components
    • F05D2250/41—Movement of components with one degree of freedom
    • F05D2250/411—Movement of components with one degree of freedom in rotation
    • 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)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Fluid Mechanics (AREA)
  • Physics & Mathematics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Rotary Pumps (AREA)
  • External Artificial Organs (AREA)
  • Containers And Packaging Bodies Having A Special Means To Remove Contents (AREA)
  • Seal Device For Vehicle (AREA)
  • Hydraulic Motors (AREA)
AT04257871T 2003-12-16 2004-12-16 Durchflussbegrenzer mit geteilten schaufeln ATE467088T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/737,599 US7101146B2 (en) 2003-12-16 2003-12-16 Split vane flow blocker

Publications (1)

Publication Number Publication Date
ATE467088T1 true ATE467088T1 (de) 2010-05-15

Family

ID=34523152

Family Applications (1)

Application Number Title Priority Date Filing Date
AT04257871T ATE467088T1 (de) 2003-12-16 2004-12-16 Durchflussbegrenzer mit geteilten schaufeln

Country Status (12)

Country Link
US (1) US7101146B2 (de)
EP (1) EP1544545B1 (de)
JP (1) JP4091042B2 (de)
KR (1) KR100686656B1 (de)
AT (1) ATE467088T1 (de)
AU (1) AU2004237914B2 (de)
CA (1) CA2490165C (de)
DE (1) DE602004026988D1 (de)
IL (1) IL165759A (de)
NO (1) NO20045463L (de)
SG (1) SG112974A1 (de)
TW (1) TWI259231B (de)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7988409B2 (en) * 2006-02-17 2011-08-02 Schlumberger Technology Corporation Method and apparatus for extending flow range of a downhole turbine
US9719370B2 (en) 2007-03-30 2017-08-01 United Technologies Corporation Linkage system with wear reduction
US7871242B2 (en) * 2007-05-31 2011-01-18 United Technologies Corporation Single actuator controlled rotational flow balance system
US8845286B2 (en) 2011-08-05 2014-09-30 Honeywell International Inc. Inter-turbine ducts with guide vanes
US8967952B2 (en) * 2011-12-22 2015-03-03 United Technologies Corporation Gas turbine engine duct blocker that includes a duct blocker rotor with a plurality of roller elements
US9011082B2 (en) * 2011-12-22 2015-04-21 United Technologies Corporation Gas turbine engine duct blocker with rotatable vane segments
US10125724B2 (en) * 2012-01-17 2018-11-13 United Technologies Corporation Start system for gas turbine engines
US9534497B2 (en) 2012-05-02 2017-01-03 Honeywell International Inc. Inter-turbine ducts with variable area ratios
US20140105720A1 (en) * 2012-10-11 2014-04-17 Krishna Kumar Bindingnavale Ranga Method and a system for adjusting nozzle area in steam turbines
EP3017169B1 (de) * 2013-07-05 2019-11-27 United Technologies Corporation Gasturbinenantriebsystem zur modulation eines gebläseflusses mithilfe von durchgangsluft und kernmotorluft sowie dazugehöriges verfahren
US9803557B2 (en) 2015-01-20 2017-10-31 United Technologies Corporation Gas turbine engine and blocker door assembly
JP6739417B2 (ja) * 2017-10-31 2020-08-12 Ｄｏｗａサーモテック株式会社 熱処理設備

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US867611A (en) * 1906-03-06 1907-10-08 Richard Schulz Steam-turbine.
US867811A (en) * 1906-10-27 1907-10-08 Jennie V Edgcomb Door-check.
GB2085146B (en) * 1980-10-01 1985-06-12 Gen Electric Flow modifying device
DE4238550A1 (de) * 1992-11-14 1994-05-19 Daimler Benz Ag Abgasturbolader für eine Brennkraftmaschine
FR2754590B1 (fr) 1996-10-16 1998-11-20 Snecma Dispositif d'alimentation en comburant d'une turbine a gaz comprenant des diaphragmes de reglage du debit commandes par paires
WO1999037954A1 (fr) 1998-01-26 1999-07-29 Mitsubishi Heavy Industries, Ltd. Dispositif de reglage du volume d'air de dilution destine au bruleur utilise dans une turbine a gaz

Also Published As

Publication number Publication date
EP1544545A1 (de) 2005-06-22
KR20050061368A (ko) 2005-06-22
SG112974A1 (en) 2005-07-28
TW200525076A (en) 2005-08-01
IL165759A (en) 2007-07-24
IL165759A0 (en) 2006-01-15
DE602004026988D1 (de) 2010-06-17
AU2004237914B2 (en) 2006-06-08
CA2490165A1 (en) 2005-06-16
US20050129501A1 (en) 2005-06-16
US7101146B2 (en) 2006-09-05
KR100686656B1 (ko) 2007-02-27
JP2005180441A (ja) 2005-07-07
AU2004237914A1 (en) 2005-06-30
TWI259231B (en) 2006-08-01
JP4091042B2 (ja) 2008-05-28
EP1544545B1 (de) 2010-05-05
CA2490165C (en) 2008-08-26
NO20045463L (no) 2005-06-17

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