[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Guimarães, 2015 - Google Patents

Implementation of an engine condition trend monitoring (ECTM) program in a part M organization: Pratt & Whitney PT6A-67D Engine

Guimarães, 2015

View PDF
Document ID
1685704190836409812
Author
Guimarães D
Publication year

External Links

Snippet

The goal of the present work is to implement an Engine Condition Trend Monitoring (ECTM) program on EASA Part M organization, using an automatic system of data acquisition, ADAS (Aircraft Data Acquisition Unit). The ECTM program will consist on the study of the process …
Continue reading at ubibliorum.ubi.pt (PDF) (other versions)

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • 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
    • F05D2270/70—Type of control algorithm
    • F05D2270/708—Type of control algorithm with comparison tables
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • 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
    • F05D2270/40—Type of control system
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/003—Arrangements for testing or measuring
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • 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
    • F05D2270/30—Control parameters, e.g. input parameters
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • 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
    • F02C7/22—Fuel supply systems

Similar Documents

Publication Publication Date Title
AU2012204053B2 (en) Method for detecting whether performance of aircraft components is in the decline period
Lukachko et al. Effects of engine aging on aircraft NOx emissions
Simon An overview of the NASA aviation safety program propulsion health monitoring element
Martins Off-design performance prediction of the cfm56-3 aircraft engine
Guimarães Implementation of an engine condition trend monitoring (ECTM) program in a part M organization: Pratt & Whitney PT6A-67D Engine
EP4345258A1 (en) Systems and methods for determining gas turbine engine temperatures
de Mesquita Implementation of an Engine Condition Trend Monitoring (ECTM) Program in a Part M Organization: Pratt & Whitney PT6a-67d Engine
Skliros et al. Experimental investigation and simulation of a Boeing 747 auxiliary power unit
Scala et al. Predicting the performance of a gas turbine engine undergoing compressor blade erosion
US11753972B2 (en) System and method for annunciating engine lubricating fluid level
Turgut Effects of ambient air temperature on gaseous emissions of turbofan engines
Mishra et al. Analysis of compressor surge in a military turbojet engine: a case study
Parajuli INSTITUTE OF ENGINEERING
Neporozhniy et al. GRAPHIC SUPPORT FOR THE OPERATION OF AIRCRAFT POWER UNITS.
Непорожній et al. GRAPHIC SUPPORT FOR THE OPERATION OF AIRCRAFT POWER UNITS
Volný et al. Analysis of engine monitoring system report
US20240060426A1 (en) Systems and methods for determining gas turbine engine operating margins
Rajamani Diagnostics and Prognostics of Aerospace Engines
US20240060427A1 (en) Systems and methods for determining gas turbine engine operating margins
Esser “Flying Test Cell” Evaluation and Applications
Vega et al. Prevention of Compressor Stall on Rolls Royce M250 Engines C20 Series Using Trend Monitoring Analysis
Ashby et al. Intelligent Engine Systems Work Element 1.3: Sub System Health Management
Balicki et al. Causes of the powerplants failures installed on Polish civil aviation aircraft
Algellal Diagnosis the flowing path of a helicopter gas turbine engine
Abdul-Aziz et al. Turbofan engine performance simulation study under selected failure scenarios of rotating and hot sections components