BR8701672A - PROCESS TO DETECT AN ENGINE SHEET IN A MULTIPLE ENGINE AIRCRAFT - Google Patents

PROCESS TO DETECT AN ENGINE SHEET IN A MULTIPLE ENGINE AIRCRAFT

Info

Publication number
BR8701672A
BR8701672A BR8701672A BR8701672A BR8701672A BR 8701672 A BR8701672 A BR 8701672A BR 8701672 A BR8701672 A BR 8701672A BR 8701672 A BR8701672 A BR 8701672A BR 8701672 A BR8701672 A BR 8701672A
Authority
BR
Brazil
Prior art keywords
engine
detect
sheet
aircraft
multiple engine
Prior art date
Application number
BR8701672A
Other languages
Portuguese (pt)
Inventor
Rice Robert Wayne
Sweet David Halbane
Evans Charles Warren
Whight Gregory Paul
Howlett James John
Lappos Nicholas Dean
Johnston Mark Allen
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 BR8701672A publication Critical patent/BR8701672A/en

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
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft
    • 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
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/02—Purpose of the control system to control rotational speed (n)
    • 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
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/05—Purpose of the control system to affect the output of the engine
    • F05D2270/052—Torque
    • 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
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/11—Purpose of the control system to prolong engine life
    • F05D2270/112—Purpose of the control system to prolong engine life by limiting temperatures
BR8701672A 1986-08-04 1987-04-09 PROCESS TO DETECT AN ENGINE SHEET IN A MULTIPLE ENGINE AIRCRAFT BR8701672A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US89268986A 1986-08-04 1986-08-04

Publications (1)

Publication Number Publication Date
BR8701672A true BR8701672A (en) 1988-01-05

Family

ID=25400361

Family Applications (1)

Application Number Title Priority Date Filing Date
BR8701672A BR8701672A (en) 1986-08-04 1987-04-09 PROCESS TO DETECT AN ENGINE SHEET IN A MULTIPLE ENGINE AIRCRAFT

Country Status (6)

Country Link
JP (1) JPS6345429A (en)
BR (1) BR8701672A (en)
DE (1) DE3725687A1 (en)
FR (1) FR2602270A1 (en)
GB (1) GB2193535A (en)
IT (1) IT1228547B (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8730187D0 (en) * 1987-12-24 1988-02-03 Rolls Royce Plc Overspeed limiter for gas turbine aeroengine
US5258505A (en) * 1991-07-26 1993-11-02 Canon Kabushiki Kaisha Trisazo compounds, and dye compositions containing same
GB2262623B (en) * 1991-12-17 1995-04-26 Rolls Royce Plc Aircraft engine management system
US6012676A (en) * 1998-03-31 2000-01-11 Sikorsky Aircraft Corporation Integrated fire and flight control system with automatic engine torque limiting
FR2878288B1 (en) 2004-11-25 2007-01-19 Eurocopter France METHOD AND DEVICE FOR OPTIMIZING THE PERFORMANCE ENVELOPE OF A TURBOMOTEUR
FR2888287B1 (en) * 2005-07-07 2011-04-08 Eurocopter France METHOD OF OPTIMIZING THE PERFOMANCE ENVELOPE OF A TURBOMOTEUR
DE102009016105B4 (en) * 2009-02-20 2017-11-16 Rolls-Royce Deutschland Ltd & Co Kg Method and device for measuring the load of rotating shafts
DE102009016106A1 (en) * 2009-02-20 2010-08-26 Rolls-Royce Deutschland Ltd & Co Kg Method for determining rotational speed of e.g. low pressure shaft of aircraft engine, involves producing rotational speed signals for rotary shaft by magnetic coding of shaft and recognizing and evaluating signals by two signal sensors
FR2966881B1 (en) 2010-10-29 2013-08-30 Eurocopter France MOTOR INSTALLATION OF AN AIRCRAFT, AIRCRAFT AND METHOD FOR CONTROLLING SAID AIRCRAFT.
FR2985715B1 (en) 2012-01-12 2013-12-27 Eurocopter France AIRCRAFT AIRCRAFT INSTALLATION, AIRCRAFT AND METHOD FOR CONTROLLING SAID AIRCRAFT
US9771167B2 (en) 2013-01-16 2017-09-26 Airbus Helicopters Monitor system for monitoring the starting of a rotary wing aircraft, an aircraft, and a method using the system
FR3000989A1 (en) * 2013-01-16 2014-07-18 Eurocopter France SYSTEM FOR MONITORING THE STARTING OF AN AIRCRAFT WITH A TURNING SAIL, AIRCRAFT AND METHOD IMPLEMENTING SAID SYSTEM
FR3034403B1 (en) 2015-03-31 2017-03-31 Airbus Helicopters METHOD AND DEVICE FOR STOPPING A TURBOMOTER IN NOMINAL OPERATION

Also Published As

Publication number Publication date
DE3725687A1 (en) 1988-02-18
JPS6345429A (en) 1988-02-26
GB8718303D0 (en) 1987-09-09
GB2193535A (en) 1988-02-10
IT1228547B (en) 1991-06-20
FR2602270A1 (en) 1988-02-05
IT8721567A0 (en) 1987-08-03

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