IT941155B - Indicatore di prestazione di motore - Google Patents

Indicatore di prestazione di motore

Info

Publication number
IT941155B
IT941155B IT31107/71A IT3110771A IT941155B IT 941155 B IT941155 B IT 941155B IT 31107/71 A IT31107/71 A IT 31107/71A IT 3110771 A IT3110771 A IT 3110771A IT 941155 B IT941155 B IT 941155B
Authority
IT
Italy
Prior art keywords
performance indicator
engine performance
engine
indicator
performance
Prior art date
Application number
IT31107/71A
Other languages
English (en)
Original Assignee
Howell Instruments
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 Howell Instruments filed Critical Howell Instruments
Application granted granted Critical
Publication of IT941155B publication Critical patent/IT941155B/it

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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L3/00—Measuring torque, work, mechanical power, or mechanical efficiency, in general
    • G01L3/24—Devices for determining the value of power, e.g. by measuring and simultaneously multiplying the values of torque and revolutions per unit of time, by multiplying the values of tractive or propulsive force and velocity
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M15/00—Testing of engines
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M15/00—Testing of engines
    • G01M15/04—Testing internal-combustion engines
    • G01M15/05—Testing internal-combustion engines by combined monitoring of two or more different engine parameters

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Testing Of Engines (AREA)
IT31107/71A 1970-11-16 1971-11-15 Indicatore di prestazione di motore IT941155B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US8958070A 1970-11-16 1970-11-16

Publications (1)

Publication Number Publication Date
IT941155B true IT941155B (it) 1973-03-01

Family

ID=22218426

Family Applications (1)

Application Number Title Priority Date Filing Date
IT31107/71A IT941155B (it) 1970-11-16 1971-11-15 Indicatore di prestazione di motore

Country Status (7)

Country Link
US (1) US3721120A (it)
JP (1) JPS5038769B1 (it)
CA (1) CA998472A (it)
DE (1) DE2156670C2 (it)
FR (1) FR2114766A5 (it)
GB (1) GB1351314A (it)
IT (1) IT941155B (it)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4212161A (en) * 1978-05-01 1980-07-15 United Technologies Corporation Simulated parameter control for gas turbine engine
US4249238A (en) * 1978-05-24 1981-02-03 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Apparatus for sensor failure detection and correction in a gas turbine engine control system
US4651563A (en) * 1985-10-16 1987-03-24 Sperry Corporation Jet engine testing apparatus
US4908618A (en) * 1988-12-27 1990-03-13 The Boeing Company Abnormal start advisory system (ASAS) for aircraft engines
US5377112A (en) * 1991-12-19 1994-12-27 Caterpillar Inc. Method for diagnosing an engine using computer based models
US5585553A (en) * 1995-07-28 1996-12-17 Caterpillar Inc. Apparatus and method for diagnosing an engine using a boost pressure model
US5646341A (en) * 1995-07-28 1997-07-08 Caterpillar Inc. Apparatus and method for diagnosing an engine using an oil pressure model
US5604306A (en) * 1995-07-28 1997-02-18 Caterpillar Inc. Apparatus and method for detecting a plugged air filter on an engine
US6459963B1 (en) * 2000-07-31 2002-10-01 General Electric Company Methods and apparatus for trimming engine control systems
US20050193739A1 (en) * 2004-03-02 2005-09-08 General Electric Company Model-based control systems and methods for gas turbine engines
US7826954B2 (en) * 2004-06-25 2010-11-02 Honda Motor Co., Ltd. System for monitoring sensor outputs of a gas turbine engine
EP1655590B1 (de) * 2004-11-09 2016-02-03 Alstom Technology Ltd Verfahren zur Bestimmung einer über einen Strömungsquerschnitt massengemittelten Temperatur einer Gasströmung in einer Gasturbine
FR2888638B1 (fr) * 2005-07-18 2007-09-28 Airbus Sas Indicateur de pilotage pour un aeronef, destine a fournir un parametre de puissance d'au moins un turbopropulseur dudit aeronef
FR2890939B1 (fr) * 2005-09-22 2007-10-19 Airbus Sas Procede et dispositif pour fournir a un pilote d'un aeronef multimoteur des informations relatives auxdits moteurs
US9739167B2 (en) * 2012-07-25 2017-08-22 Siemens Energy, Inc. Method and system for monitoring rotating blade health

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3195349A (en) * 1963-01-07 1965-07-20 Boeing Co Method and apparatus for determining the available power output of an engine
US3238768A (en) * 1963-02-19 1966-03-08 United Aircraft Corp Jet engine analyzer
US3272004A (en) * 1963-09-03 1966-09-13 United Aircraft Corp Horsepower remaining computer
US3287965A (en) * 1963-09-27 1966-11-29 United Aircraft Corp Engine performance indicator
US3485093A (en) * 1965-09-16 1969-12-23 Universal Testproducts Inc Engine performance analyzer
US3522532A (en) * 1965-10-21 1970-08-04 Mc Donnell Douglas Corp Comparison system for testing points in a circuit using a multi-channel analog signal record and playback means
US3538760A (en) * 1968-03-11 1970-11-10 Boeing Co System for indicating gas turbine engine power output control parameter limits

Also Published As

Publication number Publication date
JPS5038769B1 (it) 1975-12-12
DE2156670A1 (de) 1972-07-27
FR2114766A5 (it) 1972-06-30
CA998472A (en) 1976-10-12
DE2156670C2 (de) 1982-06-24
US3721120A (en) 1973-03-20
GB1351314A (en) 1974-04-24

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