CN1497148B - 控制燃气涡轮发动机的流体流动的方法和装置 - Google Patents

控制燃气涡轮发动机的流体流动的方法和装置 Download PDF

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Publication number
CN1497148B
CN1497148B CN200310102414.7A CN200310102414A CN1497148B CN 1497148 B CN1497148 B CN 1497148B CN 200310102414 A CN200310102414 A CN 200310102414A CN 1497148 B CN1497148 B CN 1497148B
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CN
China
Prior art keywords
valve
intake section
exit portion
valve body
described valve
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 - Lifetime
Application number
CN200310102414.7A
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English (en)
Chinese (zh)
Other versions
CN1497148A (zh
Inventor
M·D·斯温福德
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General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of CN1497148A publication Critical patent/CN1497148A/zh
Application granted granted Critical
Publication of CN1497148B publication Critical patent/CN1497148B/zh
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • 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
    • F01D17/105—Final actuators by passing part of the fluid
    • 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
    • F01D17/145—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 by means of valves, e.g. for steam turbines
    • 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
    • F01D17/148—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of rotatable members, e.g. butterfly valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K1/00—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces
    • F16K1/16—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces with pivoted closure-members
    • F16K1/18—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces with pivoted closure-members with pivoted discs or flaps
    • F16K1/22—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces with pivoted closure-members with pivoted discs or flaps with axis of rotation crossing the valve member, e.g. butterfly valves
    • F16K1/221—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces with pivoted closure-members with pivoted discs or flaps with axis of rotation crossing the valve member, e.g. butterfly valves specially adapted operating means therefor

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Fluid-Driven Valves (AREA)
  • Lift Valve (AREA)
  • Control Of Turbines (AREA)
CN200310102414.7A 2002-10-17 2003-10-17 控制燃气涡轮发动机的流体流动的方法和装置 Expired - Lifetime CN1497148B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/272799 2002-10-17
US10/272,799 US6775990B2 (en) 2002-10-17 2002-10-17 Methods and apparatus for regulating gas turbine engine fluid flow

Publications (2)

Publication Number Publication Date
CN1497148A CN1497148A (zh) 2004-05-19
CN1497148B true CN1497148B (zh) 2010-04-28

Family

ID=32042948

Family Applications (1)

Application Number Title Priority Date Filing Date
CN200310102414.7A Expired - Lifetime CN1497148B (zh) 2002-10-17 2003-10-17 控制燃气涡轮发动机的流体流动的方法和装置

Country Status (5)

Country Link
US (3) US6775990B2 (enExample)
EP (1) EP1411281B1 (enExample)
JP (1) JP4355915B2 (enExample)
CN (1) CN1497148B (enExample)
DE (1) DE60307955T2 (enExample)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7537022B2 (en) * 2005-11-09 2009-05-26 Honeywell International Inc. Valve actuator assembly
GB0613781D0 (en) * 2006-07-12 2006-08-23 Rolls Royce Plc Flow modulation method and apparatus
DE102007015176A1 (de) * 2007-03-27 2008-10-02 Fette Gmbh Vorrichtung zur Abscheidung von Stäuben aus Gasen
US7870741B2 (en) * 2007-05-25 2011-01-18 General Electric Company Turbine engine valve assembly and method of assembling the same
US8157241B2 (en) * 2008-02-29 2012-04-17 General Electric Company Methods and apparatus for regulating gas turbine engine fluid flow
US8128057B2 (en) * 2008-02-29 2012-03-06 General Electric Company Methods and apparatus for regulating gas turbine engine fluid flow
US8613198B2 (en) * 2009-12-23 2013-12-24 Unison Industries, Llc Method and apparatus for controlling compressor bleed airflow of a gas turbine engine using a butterfly valve assembly
US20110259436A1 (en) * 2010-04-27 2011-10-27 Donald Keith Fritts Shear-pin relief valve
CN104040117A (zh) * 2012-01-09 2014-09-10 联合工艺公司 具有齿轮传动架构的燃气涡轮发动机
US10088056B2 (en) 2015-01-26 2018-10-02 Hamilton Sundstrand Corporation Butterfly valve with modified scotch yoke connection
JP6799455B2 (ja) * 2016-12-16 2020-12-16 川崎重工業株式会社 ガスタービンエンジン
US10642288B2 (en) * 2018-03-07 2020-05-05 Vortech Engineering, Inc. Pressure relief valve apparatus, system and method
US11079025B2 (en) 2018-03-07 2021-08-03 Vortech Engineering, Inc. Pressure relief valve apparatus, system and method
WO2021072402A1 (en) * 2019-10-11 2021-04-15 Wright David C Hydraulic low-torque valve conversion apparatus and method
US10907744B1 (en) 2020-07-30 2021-02-02 Vortech Engineering, Inc. Pressure relief valve
US11149867B1 (en) 2020-10-31 2021-10-19 Vortech Engineering, Inc. Pressure relief valve
CN112377272B (zh) * 2020-11-30 2024-04-19 浙江博旭新能源科技有限公司 一种向心式透平轴向力调节装置
USD949922S1 (en) 2021-07-24 2022-04-26 Vortech Engineering, Inc. Pressure relief valve
USD950681S1 (en) 2021-08-13 2022-05-03 Vortech Engineering, Inc. Pressure relief valve

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3545486A (en) * 1969-01-31 1970-12-08 Holley Carburetor Co In-line valving assembly
US5396760A (en) * 1993-11-03 1995-03-14 General Electric Company Gas-side bypass flow system for the air recuperator of a gas turbine engine

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US868182A (en) * 1905-06-17 1907-10-15 Crane Co Radiator-valve.
US1397739A (en) * 1920-06-14 1921-11-22 Malcolm B Moyer Fresh-air valve for buildings
US2837270A (en) * 1952-07-24 1958-06-03 Gen Motors Corp Axial flow compressor
US3108767A (en) * 1960-03-14 1963-10-29 Rolls Royce By-pass gas turbine engine with air bleed means
US3107892A (en) * 1960-12-01 1963-10-22 Gen Motors Corp Compressor air bleed valve
US3642024A (en) * 1970-03-09 1972-02-15 Westinghouse Electric Corp Butterfly valve
US3912223A (en) * 1974-03-15 1975-10-14 Nittan Co Ltd Fireproof smoke damper
US4248051A (en) 1979-10-29 1981-02-03 Darcy Jon J System and method for controlling air conditioning systems
US4576358A (en) * 1983-04-20 1986-03-18 Hydril Company Remotely operable safety valve
US4691689A (en) * 1985-12-06 1987-09-08 B. D. Wait Co. Limited One piece adjustable damper
US4916893A (en) * 1987-09-02 1990-04-17 Sundstrand Corporation Multipurpose auxiliary power unit
US5063963A (en) 1990-08-09 1991-11-12 General Electric Company Engine bleed air supply system
US5151022A (en) 1991-10-03 1992-09-29 Allied-Signal Inc. Environmental control system with catalytic filter
US5327744A (en) 1992-12-18 1994-07-12 United Technologies Corporation Integrated environmental control system for a helicopter
US5327720A (en) 1993-05-03 1994-07-12 Allied-Signal Inc. Differential pressure regulator valve
GB9508043D0 (en) 1995-04-20 1995-06-07 British Aerospace Environmental control system
US5881995A (en) * 1997-12-15 1999-03-16 Pratt & Whitney Canada Inc. Noise attenuating device for butterfly valves
EP1160511B1 (en) 1998-08-03 2013-01-02 Mitsubishi Heavy Industries, Ltd. Gas turbine combustor by-pass valve device
US6481210B1 (en) 2001-05-16 2002-11-19 Honeywell International, Inc. Smart surge bleed valve system and method
US6722137B2 (en) * 2001-08-17 2004-04-20 General Electric Co. Methods and apparatus for regulating turbine clearance control system airflow

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3545486A (en) * 1969-01-31 1970-12-08 Holley Carburetor Co In-line valving assembly
US5396760A (en) * 1993-11-03 1995-03-14 General Electric Company Gas-side bypass flow system for the air recuperator of a gas turbine engine

Also Published As

Publication number Publication date
US6775990B2 (en) 2004-08-17
EP1411281B1 (en) 2006-08-30
EP1411281A1 (en) 2004-04-21
DE60307955D1 (de) 2006-10-12
JP4355915B2 (ja) 2009-11-04
CN1497148A (zh) 2004-05-19
US6986257B2 (en) 2006-01-17
JP2004138065A (ja) 2004-05-13
USRE41229E1 (en) 2010-04-20
US20040074237A1 (en) 2004-04-22
US20050000223A1 (en) 2005-01-06
DE60307955T2 (de) 2007-05-24

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Granted publication date: 20100428