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BR9001664A - Processo e aparelho para proporcionar compensacao dinamica de um regulador de velocidade de controle de passo do propulsor - Google Patents

Processo e aparelho para proporcionar compensacao dinamica de um regulador de velocidade de controle de passo do propulsor

Info

Publication number
BR9001664A
BR9001664A BR909001664A BR9001664A BR9001664A BR 9001664 A BR9001664 A BR 9001664A BR 909001664 A BR909001664 A BR 909001664A BR 9001664 A BR9001664 A BR 9001664A BR 9001664 A BR9001664 A BR 9001664A
Authority
BR
Brazil
Prior art keywords
propeller
control
provide dynamic
dynamic compensation
speed control
Prior art date
Application number
BR909001664A
Other languages
English (en)
Inventor
Roy W Schneider
David E Leenhouts
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
Publication of BR9001664A publication Critical patent/BR9001664A/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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/48—Control of fuel supply conjointly with another control of the plant
    • F02C9/56—Control of fuel supply conjointly with another control of the plant with power transmission control
    • F02C9/58—Control of fuel supply conjointly with another control of the plant with power transmission control with control of a variable-pitch propeller
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30—Blade pitch-changing mechanisms
    • B64C11/303—Blade pitch-changing mechanisms characterised by comprising a governor
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0615—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
    • G05D1/063—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind by acting on the motors

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • Radar, Positioning & Navigation (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Control Of Velocity Or Acceleration (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Control Of Turbines (AREA)
BR909001664A 1989-04-10 1990-04-09 Processo e aparelho para proporcionar compensacao dinamica de um regulador de velocidade de controle de passo do propulsor BR9001664A (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/335,901 US5023793A (en) 1989-04-10 1989-04-10 Apparatus and method for dynamic compensation of a propeller pitch speed control governor

Publications (1)

Publication Number Publication Date
BR9001664A true BR9001664A (pt) 1991-05-14

Family

ID=23313697

Family Applications (1)

Application Number Title Priority Date Filing Date
BR909001664A BR9001664A (pt) 1989-04-10 1990-04-09 Processo e aparelho para proporcionar compensacao dinamica de um regulador de velocidade de controle de passo do propulsor

Country Status (6)

Country Link
US (1) US5023793A (pt)
EP (1) EP0392965A1 (pt)
JP (1) JPH0361623A (pt)
CN (1) CN1046988A (pt)
BR (1) BR9001664A (pt)
CA (1) CA2013708A1 (pt)

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JPH0788241B2 (ja) * 1986-07-03 1995-09-27 住友電気工業株式会社 光フアイバの被覆方法及び被覆装置
US5315819A (en) * 1991-09-17 1994-05-31 Allied-Signal Inc. Power management system for turbine engines
US5274558A (en) * 1991-09-18 1993-12-28 Allied-Signal Inc. Apparatus for decoupling a torque loop from a speed loop in a power management system for turboprop engines
US5331559A (en) * 1991-09-18 1994-07-19 Alliedsignal Inc. Apparatus for preventing propeller overshoot
JP3040611B2 (ja) * 1992-09-17 2000-05-15 三菱重工業株式会社 低騒音ヘリコプタ
US9506405B2 (en) 1998-04-03 2016-11-29 Rockwell Collins Control Technologies, Inc. Apparatus and method for controlling power generation system
US6171055B1 (en) 1998-04-03 2001-01-09 Aurora Flight Sciences Corporation Single lever power controller for manned and unmanned aircraft
US7011498B2 (en) 1998-04-03 2006-03-14 Athena Technologies, Inc. Optimization method for power generation systems
US6289274B1 (en) 1999-08-13 2001-09-11 United Technologies Corporation Fuzzy logic based fuel flow selection system
US7931231B2 (en) * 2007-05-18 2011-04-26 Sikorsky Aircraft Corporation Engine anticipation for rotary-wing aircraft
FR2916421B1 (fr) * 2007-05-22 2010-04-23 Eurocopter France Systeme de commande d'un giravion.
GB2461925A (en) * 2008-07-18 2010-01-20 Rolls Royce Plc Engine fuel control system
US8321104B2 (en) * 2008-07-18 2012-11-27 Rolls-Royce Plc Control system
US8494749B2 (en) 2010-10-14 2013-07-23 Hamilton Sundstrand Corporation Method of operating an electronic engine control (EEC) to compensate for speed changes
US8720201B2 (en) 2010-11-24 2014-05-13 Hamilton Sundstrand Corporation Method of monitoring an electronic engine control (EEC) to detect a loss of fuel screen open area
CA2864821C (en) 2012-02-15 2018-10-09 Rolls-Royce Corporation Gas turbine engine performance seeking control
US9169783B2 (en) 2012-05-30 2015-10-27 Woodward, Inc. Electrohydraulic propeller governor
WO2014143772A1 (en) 2013-03-15 2014-09-18 United Technologies Corporation Compact aero-thermo model base point linear system based state estimator
CN103661925B (zh) * 2013-12-11 2016-08-17 中国航天空气动力技术研究院 一种基于复合材料的自动变桨矩螺旋桨确定方法
CN105620767A (zh) * 2014-10-28 2016-06-01 中国航空工业集团公司西安飞机设计研究所 一种利用油门杆综合控制发动机和螺旋桨的方法
US9771878B2 (en) * 2015-10-19 2017-09-26 General Electric Company Thrust scheduling method for variable pitch fan engines and turbo-shaft, turbo-propeller engines
FR3055029B1 (fr) * 2016-08-12 2018-07-27 Safran Aircraft Engines Systeme de commande d'un turbopropulseur avec gestion des saturations de commande
US10309330B2 (en) 2016-10-27 2019-06-04 Rolls-Royce Corporation Model reference adaptive controller
US10240544B2 (en) 2016-10-27 2019-03-26 Rolls-Royce Corporation Adaptive controller using unmeasured operating parameter
EP3434598B1 (en) 2017-07-28 2021-11-03 GE Avio S.r.l. Method of controlling gas generator power and torque output
US20190155318A1 (en) * 2017-11-23 2019-05-23 Pratt & Whitney Canada Corp. Torque signal dynamic compensation based on sensor location
EP3543112B1 (en) * 2018-03-23 2020-10-21 Ge Avio S.r.l. System and method for combined propeller speed and propeller pitch control for a turbopropeller engine
EP3584429B1 (en) * 2018-06-18 2021-03-31 GE Avio S.r.l. Control system and method for a turbopropeller engine based on inlet temperature sensing
CN110886659B (zh) * 2018-09-11 2025-01-07 普拉特-惠特尼加拿大公司 用于限制发动机功率的方法及系统
US11427304B2 (en) * 2018-10-15 2022-08-30 Pratt & Whitney Canada Corp. System and method for slowing down aircraft
US11635032B2 (en) 2019-12-13 2023-04-25 Pratt & Whitney Canada Corp. System and method for propeller speed governing
CN111252238B (zh) * 2020-03-17 2024-11-26 南京韬讯航空科技有限公司 一种电调控制的变距旋翼系统模块及直升机
US12305537B2 (en) 2023-08-04 2025-05-20 General Electric Company Vane assembly for open fan engine

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US2669312A (en) * 1949-05-24 1954-02-16 Gen Motors Corp Aircraft propeller speed controller
US4206597A (en) * 1976-04-23 1980-06-10 The Boeing Company Fan R.P.M. control loop stabilization using high rotor speed
US4209152A (en) * 1977-11-25 1980-06-24 The Boeing Company Turbulence compensated throttle control system for aircraft having throttle command signal path control means responsive to engine rating control and flare initiation
US4442490A (en) * 1980-09-26 1984-04-10 S-Tec Corporation Aircraft pitch stabilization apparatus
US4488235A (en) * 1981-11-03 1984-12-11 Sperry Corporation Speed control system for aircraft
US4470118A (en) * 1982-04-19 1984-09-04 Chandler Evans Inc. Gas turbine engine fuel control
US4656362A (en) * 1982-11-08 1987-04-07 United Technologies Corporation Blade pitch angle control for large wind turbines
US4533295A (en) * 1982-12-20 1985-08-06 United Technologies Corporation Pitch control system for variable pitch propeller
GB8300101D0 (en) * 1983-01-05 1983-02-09 Short Bros Ltd Control of aerial propeller
US4588354A (en) * 1983-08-05 1986-05-13 United Technologies Corporation Engine speed control in propeller pitch control systems
US4648797A (en) * 1983-12-19 1987-03-10 United Technologies Corporation Torque control system
US4639192A (en) * 1984-04-11 1987-01-27 American Standard Inc. Propeller pitch controlling arrangement having a fuel economizing feature
GB8800904D0 (en) * 1988-01-15 1988-02-17 Rolls Royce Plc Fuel control system

Also Published As

Publication number Publication date
US5023793A (en) 1991-06-11
EP0392965A1 (en) 1990-10-17
CN1046988A (zh) 1990-11-14
CA2013708A1 (en) 1990-10-10
JPH0361623A (ja) 1991-03-18

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