ES257490A1 - Perfeccionamientos en los reguladores de divisiën de corriente en motores de turbina de gas - Google Patents

Perfeccionamientos en los reguladores de divisiën de corriente en motores de turbina de gas

Info

Publication number
ES257490A1
ES257490A1 ES0257490A ES257490A ES257490A1 ES 257490 A1 ES257490 A1 ES 257490A1 ES 0257490 A ES0257490 A ES 0257490A ES 257490 A ES257490 A ES 257490A ES 257490 A1 ES257490 A1 ES 257490A1
Authority
ES
Spain
Prior art keywords
valve
control
fuel
depending
duct
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
Application number
ES0257490A
Other languages
English (en)
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.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation 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 Bendix Aviation Corp filed Critical Bendix Aviation Corp
Publication of ES257490A1 publication Critical patent/ES257490A1/es
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • 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
    • Y10T137/2278—Pressure modulating relays or followers
    • Y10T137/2409—With counter-balancing pressure feedback to the modulating device
    • 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
    • Y10T137/2496—Self-proportioning or correlating systems
    • Y10T137/2499—Mixture condition maintaining or sensing
    • 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
    • Y10T137/2496—Self-proportioning or correlating systems
    • Y10T137/2514—Self-proportioning flow systems
    • 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
    • Y10T137/2496—Self-proportioning or correlating systems
    • Y10T137/2559—Self-controlled branched flow systems
    • Y10T137/2574—Bypass or relief controlled by main line fluid condition
    • Y10T137/2579—Flow rate responsive

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
  • Control Of Fluid Pressure (AREA)

Abstract

Perfeccionamientos en los reguladores de división de corriente en motores de turbina de gas, caracterizados porque estos últimos tienen un compresor, un suministro de combustible calibrado a presión elevada y colectores de postcombustión, primero y segundo y además, por comprender un primer conducto conectado al primer colector por un extremo y que tiene otro extremo en el que se introduce el suministro de combustible calibrada,primeros medios valvulares que funcionan con el primer conducto para controlar la corriente de combustible a través, en función de la posición de la primera válvula, un segundo conducto funcionalmente conectado al segundo colector por un extremo y con el primer conducto en la parte anterior de los primeros medios valvulares, segundos medios valvulares que funcionan con el segundo conducto para controlar al corriente de combustible a su través, en función de la posición de la segunda válvula, medios dependientes de una presión producida por el compresor conectados a los segundos medios valvulares, para controlar la posición de estos que controla la corriente de combustible en función de dicha presión y medios dependientes de la diferencia de presiones del combustible fluido a través de la segunda válvula conectada a la primera, para controlar al posición de la misma reguladora de la corriente de combustible, en función de la mencionada diferencia de presiones.
ES0257490A 1959-04-21 1960-04-20 Perfeccionamientos en los reguladores de divisiën de corriente en motores de turbina de gas Expired ES257490A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US80782659 US3234730A (en) 1959-04-21 1959-04-21 Dual afterburner manifold proportioning control

Publications (1)

Publication Number Publication Date
ES257490A1 true ES257490A1 (es) 1960-07-01

Family

ID=25197245

Family Applications (1)

Application Number Title Priority Date Filing Date
ES0257490A Expired ES257490A1 (es) 1959-04-21 1960-04-20 Perfeccionamientos en los reguladores de divisiën de corriente en motores de turbina de gas

Country Status (3)

Country Link
US (1) US3234730A (es)
ES (1) ES257490A1 (es)
GB (1) GB900139A (es)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116399605A (zh) * 2023-05-10 2023-07-07 中国航发沈阳发动机研究所 航空发动机整机涡轮测试用加力燃烧室气动特性模拟装置

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3643427A (en) * 1969-08-22 1972-02-22 Lucas Industries Ltd Fuel control systems for supplying fuel to primary and main burners in a gas turbine engine
US3591968A (en) * 1969-12-15 1971-07-13 Bendix Corp Afterburner fuel manifold quick fill and flow distribution apparatus
US4229939A (en) * 1978-02-17 1980-10-28 Lucas Industries Limited Fuel control for a gas turbine engine reheat system
US4805658A (en) * 1987-04-24 1989-02-21 United Technologies Corporation Variable pressure regulating valve
US9849992B2 (en) * 2016-05-23 2017-12-26 United Technologies Corporation Inline pressure regulating valve assembly with inlet pressure bias

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2127172A (en) * 1938-08-16 Fcknace bukner
US2590853A (en) * 1945-10-16 1952-04-01 Gen Electric Liquid fuel metering and spraying system
US2683349A (en) * 1949-11-17 1954-07-13 Lucas Ltd Joseph Jet engine combustion system having burner in the jet pipe and controlling means therefor
US2757511A (en) * 1951-01-26 1956-08-07 Armstrong Siddeley Motors Ltd System for regulating the supply of liquid fuel to a gas turbine
US2764868A (en) * 1951-03-27 1956-10-02 Lucas Industries Ltd Servo control of internal combustion prime movers by blower pressure
US2724239A (en) * 1952-04-21 1955-11-22 Samuel S Fox Fuel flow distributing and manifold pressurizing valve for dual orifice fuel injection nozzles
US2712219A (en) * 1952-10-27 1955-07-05 Lucas Industries Ltd Liquid fuel control means for aerial bodies of the ram-jet type
US2770945A (en) * 1953-08-17 1956-11-20 United Aircraft Corp Jump-type flow divider for gas turbine power plant fuel system
US2916876A (en) * 1954-06-28 1959-12-15 Rolls Royce Reheat fuel-system for gas-turbine engine
US2843141A (en) * 1954-11-22 1958-07-15 John Reginald Sharp Metering devices for hydraulic circuits
US3007303A (en) * 1955-07-08 1961-11-07 Bendix Corp Compressor pressure modified fuel schedule for an afterburner

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116399605A (zh) * 2023-05-10 2023-07-07 中国航发沈阳发动机研究所 航空发动机整机涡轮测试用加力燃烧室气动特性模拟装置
CN116399605B (zh) * 2023-05-10 2024-06-07 中国航发沈阳发动机研究所 航空发动机整机涡轮测试用加力燃烧室气动特性模拟装置

Also Published As

Publication number Publication date
GB900139A (en) 1962-07-04
US3234730A (en) 1966-02-15

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