BRPI0307475A2 - válvula de arranque de turbina a ar. - Google Patents

válvula de arranque de turbina a ar.

Info

Publication number
BRPI0307475A2
BRPI0307475A2 BRPI0307475A BR0307475A BRPI0307475A2 BR PI0307475 A2 BRPI0307475 A2 BR PI0307475A2 BR PI0307475 A BRPI0307475 A BR PI0307475A BR 0307475 A BR0307475 A BR 0307475A BR PI0307475 A2 BRPI0307475 A2 BR PI0307475A2
Authority
BR
Brazil
Prior art keywords
air turbine
turbine starter
starter valve
valve
air
Prior art date
Application number
BRPI0307475A
Other languages
English (en)
Inventor
Jimmy D Wiggins
John L Doak
Ronald J Louis
Wiliam H Reed
Original Assignee
Honeywell Int Inc
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 Honeywell Int Inc filed Critical Honeywell Int Inc
Publication of BRPI0307475A2 publication Critical patent/BRPI0307475A2/pt

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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/275—Mechanical drives
    • F02C7/277—Mechanical drives the starter being a separate turbine
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047—Heating to prevent icing
    • 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
    • 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
    • F16K31/00—Actuating devices; Operating means; Releasing devices
    • F16K31/12—Actuating devices; Operating means; Releasing devices actuated by fluid
    • F16K31/16—Actuating devices; Operating means; Releasing devices actuated by fluid with a mechanism, other than pulling-or pushing-rod, between fluid motor and closure member
    • F16K31/163—Actuating devices; Operating means; Releasing devices actuated by fluid with a mechanism, other than pulling-or pushing-rod, between fluid motor and closure member the fluid acting on a piston
    • F16K31/1635—Actuating devices; Operating means; Releasing devices actuated by fluid with a mechanism, other than pulling-or pushing-rod, between fluid motor and closure member the fluid acting on a piston for rotating valves
    • 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
    • F05D2250/10—Two-dimensional
    • F05D2250/18—Two-dimensional patterned
    • F05D2250/182—Two-dimensional patterned crenellated, notched
    • 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
    • F05D2250/10—Two-dimensional
    • F05D2250/19—Two-dimensional machined; miscellaneous
    • F05D2250/192—Two-dimensional machined; miscellaneous bevelled
    • 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
    • F05D2260/00—Function
    • F05D2260/85—Starting
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/7722—Line condition change responsive valves
    • Y10T137/7758—Pilot or servo controlled
    • Y10T137/7762—Fluid pressure type

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Fluid-Driven Valves (AREA)
BRPI0307475A 2002-02-06 2003-02-05 válvula de arranque de turbina a ar. BRPI0307475A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/071,351 US6694746B2 (en) 2002-02-06 2002-02-06 Micro volume actuator for an air turbine starter
PCT/US2003/003379 WO2003067056A1 (en) 2002-02-06 2003-02-05 Actuator for an air turbine starter valve

Publications (1)

Publication Number Publication Date
BRPI0307475A2 true BRPI0307475A2 (pt) 2016-11-08

Family

ID=27659217

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0307475A BRPI0307475A2 (pt) 2002-02-06 2003-02-05 válvula de arranque de turbina a ar.

Country Status (6)

Country Link
US (1) US6694746B2 (pt)
EP (1) EP1472446B1 (pt)
AU (1) AU2003217321A1 (pt)
BR (1) BRPI0307475A2 (pt)
CA (1) CA2481974A1 (pt)
WO (1) WO2003067056A1 (pt)

Families Citing this family (58)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7066710B2 (en) * 2004-05-27 2006-06-27 Honeywell International, Inc. Pneumatic valve control having improved opening characteristics and an air turbine starter incorporating the same
US7147430B2 (en) * 2004-06-10 2006-12-12 Honeywell International, Inc. Pneumatic valve control using downstream pressure feedback and an air turbine starter incorporating the same
US7571742B2 (en) * 2005-03-23 2009-08-11 Honeywell International Inc. Butterfly outflow valve
US7291934B2 (en) * 2005-08-30 2007-11-06 Caterpillar Inc. Machine with an electrical system
US8091862B2 (en) 2006-09-29 2012-01-10 Sikorsky Aircraft Corporation Butterfly valves having sleeve inserts
US8360097B2 (en) * 2008-04-22 2013-01-29 Honeywell International Inc. Valve actuator and throttle valve assembly employing the same
US8047226B2 (en) * 2008-06-18 2011-11-01 Honeywell International Inc. Pressure relief valves and pneumatic control systems
US8286661B2 (en) * 2009-05-26 2012-10-16 Honeywell International Inc. Bi-directional overpressure shut-off valve
US8353729B2 (en) * 2010-02-18 2013-01-15 Apple Inc. Low profile connector system
US9353690B2 (en) 2010-06-21 2016-05-31 Hamilton Sundstrand Corporation Interface with mount features for precise alignment
US8613142B2 (en) 2010-07-30 2013-12-24 Hamilton Sundstrand Corporation Methods for cluster gear timing and manufacturing
US8667803B2 (en) * 2010-09-22 2014-03-11 Hamilton Sundstrand Corporation Turbine starter valve
US20120199211A1 (en) * 2011-02-08 2012-08-09 Hamilton Sundstrand Corporation Airflow control system
US8452516B1 (en) 2012-01-31 2013-05-28 United Technologies Corporation Variable vane scheduling based on flight conditions for inclement weather
US20130276892A1 (en) * 2012-04-23 2013-10-24 Hamilton Sundstrand Corporation Pneumatic butterfly valve
BR112014030200B1 (pt) * 2012-06-20 2021-08-03 Dayco Ip Holdings, Llc Válvula de fluxo variável e sistema para controlar um sistema de turbocarregador acionado por exaustão
JP6149216B2 (ja) * 2013-05-21 2017-06-21 株式会社テージーケー 切替弁
US10309317B2 (en) * 2013-06-21 2019-06-04 Hamilton Sundstrand Corporation Air turbine starter pressure monitor system
US9482346B2 (en) * 2013-09-13 2016-11-01 Clark Equipment Company System and method for controlling a compressor inlet valve
EP2886834A1 (en) * 2013-12-20 2015-06-24 IMI Hydronic Engineering International SA A valve and a method of controlling a valve in a fluid conduit
US9291094B2 (en) 2014-05-05 2016-03-22 Dayco Ip Holdings, Llc Variable flow valve having metered flow orifice
FR3036137B1 (fr) * 2015-05-13 2017-06-02 Snecma Vanne papillon de decharge de pression d'un compresseur pour turbomachine d'aeronef
US10436064B2 (en) 2016-02-12 2019-10-08 United Technologies Corporation Bowed rotor start response damping system
US10539079B2 (en) 2016-02-12 2020-01-21 United Technologies Corporation Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
US10443507B2 (en) 2016-02-12 2019-10-15 United Technologies Corporation Gas turbine engine bowed rotor avoidance system
US10174678B2 (en) 2016-02-12 2019-01-08 United Technologies Corporation Bowed rotor start using direct temperature measurement
US10508567B2 (en) 2016-02-12 2019-12-17 United Technologies Corporation Auxiliary drive bowed rotor prevention system for a gas turbine engine through an engine accessory
US10125636B2 (en) 2016-02-12 2018-11-13 United Technologies Corporation Bowed rotor prevention system using waste heat
US10508601B2 (en) 2016-02-12 2019-12-17 United Technologies Corporation Auxiliary drive bowed rotor prevention system for a gas turbine engine
US10040577B2 (en) * 2016-02-12 2018-08-07 United Technologies Corporation Modified start sequence of a gas turbine engine
US10125691B2 (en) 2016-02-12 2018-11-13 United Technologies Corporation Bowed rotor start using a variable position starter valve
US10443505B2 (en) 2016-02-12 2019-10-15 United Technologies Corporation Bowed rotor start mitigation in a gas turbine engine
US9664070B1 (en) 2016-02-12 2017-05-30 United Technologies Corporation Bowed rotor prevention system
US9849992B2 (en) * 2016-05-23 2017-12-26 United Technologies Corporation Inline pressure regulating valve assembly with inlet pressure bias
US10724443B2 (en) 2016-05-24 2020-07-28 General Electric Company Turbine engine and method of operating
US20170350322A1 (en) * 2016-06-02 2017-12-07 Hamilton Sundstrand Corporation Heated starter air valve
US10358936B2 (en) 2016-07-05 2019-07-23 United Technologies Corporation Bowed rotor sensor system
US10384791B2 (en) 2016-07-21 2019-08-20 United Technologies Corporation Cross engine coordination during gas turbine engine motoring
US10221774B2 (en) 2016-07-21 2019-03-05 United Technologies Corporation Speed control during motoring of a gas turbine engine
EP3273006B1 (en) 2016-07-21 2019-07-03 United Technologies Corporation Alternating starter use during multi-engine motoring
EP3273016B1 (en) 2016-07-21 2020-04-01 United Technologies Corporation Multi-engine coordination during gas turbine engine motoring
US10618666B2 (en) 2016-07-21 2020-04-14 United Technologies Corporation Pre-start motoring synchronization for multiple engines
US10787968B2 (en) * 2016-09-30 2020-09-29 Raytheon Technologies Corporation Gas turbine engine motoring with starter air valve manual override
US10266278B2 (en) 2016-10-11 2019-04-23 Unison Industries, Llc Starter issue detection
US10598095B2 (en) 2016-10-11 2020-03-24 Unison Industries, Llc Integrated starter for aerial vehicle
US10443543B2 (en) 2016-11-04 2019-10-15 United Technologies Corporation High compressor build clearance reduction
US10934885B2 (en) 2016-11-07 2021-03-02 Raytheon Technologies Corporation System and method for controlling dual starter air valve
US10823079B2 (en) * 2016-11-29 2020-11-03 Raytheon Technologies Corporation Metered orifice for motoring of a gas turbine engine
US10781713B2 (en) * 2016-12-28 2020-09-22 Hamilton Sundstrand Corporation Starter air valve systems configured for low speed motoring
US10301963B2 (en) * 2016-12-28 2019-05-28 Hamilton Sundstrand Corporation Starter air valve systems configured for low speed motoring
US10711700B2 (en) * 2017-02-01 2020-07-14 Raytheon Technologies Corporation Gas turbine start system to enable rotor thermal stabilization with backup bleed bypass cooling mode
US10711701B2 (en) * 2017-06-06 2020-07-14 Hamilton Sunstrand Corporation Manual bowed rotor and full override
US10570816B2 (en) 2017-09-19 2020-02-25 Pratt & Whitney Canada Corp. Engine coupling arrangement
US11261796B2 (en) * 2019-12-23 2022-03-01 Hamilton Sundstrand Corporation Air turbine starter air valve
EP3859103A1 (en) 2020-01-29 2021-08-04 Goodrich Actuation Systems Limited Locking systems
FR3107732A1 (fr) * 2020-02-27 2021-09-03 Airbus Operations Systeme de regulation comportant une vanne, un regulateur, un actionneur et un systeme de refroidissement utilisant des tubes caloducs
CN114233478A (zh) * 2021-11-24 2022-03-25 河南航天液压气动技术有限公司 一种大通径通油活门
US20230264132A1 (en) * 2022-02-23 2023-08-24 Hamilton Sundstrand Corporation Motorized valve with washing filter extending from a bleed conduit inlet into valve duct

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2189475A (en) * 1936-09-05 1940-02-06 Siemens App Und Maschinen Gmbh Regulating apparatus
US2938537A (en) * 1953-06-01 1960-05-31 Garrett Corp Shut-off valve rate of operating control
US2993496A (en) 1957-11-19 1961-07-25 Gen Electric Gas turbine flow control arrangement
US3200591A (en) * 1963-09-30 1965-08-17 Itt Polarized solenoid actuating system
US3433251A (en) 1966-09-02 1969-03-18 Garrett Corp Regulator valve mechanism
US3769998A (en) 1971-10-07 1973-11-06 Garrett Corp Regulator and shutoff valve
US4585172A (en) 1983-10-07 1986-04-29 The Garrett Corporation Hydraulic actuation
US4617958A (en) 1985-07-25 1986-10-21 Sundstrand Corporation Control valve
US4702273A (en) 1986-03-07 1987-10-27 Parker Hannifin Corporation Electrically controlled starter air valve
FR2607189B1 (fr) 1986-11-20 1990-05-04 Snecma Dispositif de commande d'une vanne de demarrage de turbomachine d'aviation
US4768555A (en) 1987-04-30 1988-09-06 Allied-Signal Inc. Solenoid valve
US4914906A (en) 1988-05-24 1990-04-10 Allied-Signal Inc. Turbine starter device
US4903578A (en) 1988-07-08 1990-02-27 Allied-Signal Inc. Electropneumatic rotary actuator having proportional fluid valving
US5267433A (en) 1992-03-25 1993-12-07 Allied-Signal, Inc. Air turbine starter having a dual clutch
US5315817A (en) 1992-08-17 1994-05-31 United Technologies Corporation Control system for preventing crash engagement of a ratchet and pawl clutch during restart of a turbine engine
US5389910A (en) 1992-12-08 1995-02-14 Alliedsignal Inc. Solenoid encasement with variable reluctance
FR2709167B1 (fr) 1993-08-18 1995-09-22 Snecma Système de dégivrage d'une vanne à papillon.
US5365210A (en) 1993-09-21 1994-11-15 Alliedsignal Inc. Latching solenoid with manual override
US5463865A (en) 1993-09-30 1995-11-07 General Electric Company Starter air valve position pressure transducer
US5435125A (en) 1994-06-15 1995-07-25 United Technologies Corporation Redundant engine starting system
US5779217A (en) * 1996-03-11 1998-07-14 North American Manufacturing Company Diaphragm actuated air cycle valve
US5752383A (en) 1996-11-14 1998-05-19 Alliedsignal Inc. Air turbine flow restrictor
FR2774357B1 (fr) * 1998-02-05 2000-04-07 Aerospatiale Systeme d'alimentation en air chaud pour aeronef
US6240246B1 (en) 1998-10-30 2001-05-29 Alliedsignal, Inc. Anti-resonance mixing filter
US6211665B1 (en) 1999-04-13 2001-04-03 Alliedsignal Inc. Solenoid motion detection circuit

Also Published As

Publication number Publication date
US20030145603A1 (en) 2003-08-07
EP1472446A1 (en) 2004-11-03
US6694746B2 (en) 2004-02-24
WO2003067056A1 (en) 2003-08-14
EP1472446B1 (en) 2009-12-16
CA2481974A1 (en) 2003-08-14
AU2003217321A1 (en) 2003-09-02

Similar Documents

Publication Publication Date Title
BRPI0307475A2 (pt) válvula de arranque de turbina a ar.
GB0410548D0 (en) A gas turbine engine
GB0211350D0 (en) A gas turbine engine
NO20045028L (no) Vindturbin.
EP1706620A4 (en) TURBO ENGINE ARCHITECTURE
DE60334758D1 (de) Gasventil
BR0203493B1 (pt) aerofólio de turbina para motor de turbina a gás.
GB2401651B (en) A gas turbine engine
FR2858649B1 (fr) Turbine basse-pression de turbomachine
IL173907A0 (en) Gas turbine engine systems
BR0203490B1 (pt) aerofólio de turbina para motor de turbina a gás.
SG119178A1 (en) Valve assembly for gas turbine engine
BR0305668B1 (pt) compressor.
MXPA03002422A (es) Motor.
GB0415376D0 (en) A turbine engine arrangement
DE60300388D1 (de) Gasturbinentriebwerksregelungssystem
GB0415554D0 (en) Turbine engine nozzle
DE50313018D1 (de) Abgasturbine
ITTO20030241A1 (it) Albero a camme.
NO20041762L (no) Kanal omkring eksosjeten i en turbinmotor.
PL373858A1 (en) Turbine engine
GB0211121D0 (en) A striling engine assembly
GB0415187D0 (en) Turbine engine nozzle
GB2402178B (en) Gas turbine engine
ATA9532003A (de) Elektromagnetisch betätigtes gasventil

Legal Events

Date Code Title Description
B06H Technical and formal requirements: requirement cancelled [chapter 6.8 patent gazette]

Free format text: ANULADA A EXIGENCIA 6.7 PUBLICADA NA RPI 1871 DE 14/11/2006 POR TER SIDO INDEVIDA.

B15I Others concerning applications: loss of priority

Free format text: PERDA DA PRIORIDADE US 10/071.351 DE 06/02/2002, CONFORME AS DISPOSICOES PREVISTAS NA LEI 9.279 DE 14/05/1996 (LPI) ART. 16 7O E NO ART. 28 DO ATO NORMATIVO 128/1997, POR NAO ATENDER AO DISPOSTO NO ART. 27 DO ATO NORMATIVO 128/1997, POIS NAO FOI APRESENTADA CESSAO DA REFERIDA PRIORIDADE, QUE POSSUI DEPOSITANTE DIFERENTE DO DEPOSITANTE DA FASE NACIONAL.

B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]