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Monday, July 20, 2020 | History

2 edition of Are management problems in the acquisition of aircraft gas turbine engines being corrected? found in the catalog.

Are management problems in the acquisition of aircraft gas turbine engines being corrected?

United States. General Accounting Office

Are management problems in the acquisition of aircraft gas turbine engines being corrected?

report to the Congress

by United States. General Accounting Office

  • 190 Want to read
  • 8 Currently reading

Published by U.S. General Accounting Office in Washington, D.C .
Written in English

    Subjects:
  • Aircraft gas-turbines

  • Edition Notes

    Statementby the Comptroller General of the United States
    The Physical Object
    Paginationvii, 63 p. ;
    Number of Pages63
    ID Numbers
    Open LibraryOL14900667M

    8. Gas Turbine Repair. The techniques of inspection and repair of gas turbines are described in detail, including NDT techniques, cleaning, plating, heat treatment, welding, etc. 9. Gas Turbine Maintenance. Maintenance techniques using borescopes. Spectrum analysis including acoustic monitoring.   This text on aircraft engines and turbines presents the engine as a complete system, with emphasis on the performance of the engine and its dependence on the major design parameters and physical limitations. The system is described at three levels, first by ideal cycle and analysis, then by more refined cycle analysis, and finally as an assembly of components.

      Aircraft or aeroplane history of propulsion started with piston engine. But piston engine can't go beyond certain rotation per minute due its piston reciprocating motion. If output speed increased with gear system than torque become the problem an. Fundamentals of Aircraft Turbine Engine Control Dr. Sanjay Garg Chief, Controls and Dynamics Branch Ph: () Environment within a gas turbine 50 g centrifugal acceleration >g casing vibration to beyond 20kHz +ºC • Corrected parameter techniques used to reduce theFile Size: 1MB.

    The term “turbojet” was used to describe any gas turbine engine used in aircraft. As gas turbine technology evolved, these other engine types were developed to take the place of the pure turbojet engine. A turbojet engine was first developed in Germany and England prior to World War II and is the simplest of all jet engines. or pump. Two-shaft gas turbines are normally applied where load demand variations require a range of power and rotational speed from the gas turbine. These gas turbines are used for marine craft and locomotives, for electrical power generation, and for mechanical drives in the oil and gas, 9.


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Are management problems in the acquisition of aircraft gas turbine engines being corrected? by United States. General Accounting Office Download PDF EPUB FB2

GAO examined the Department of Defense's management approach to the acquisition of gas turbine engines for fighter/attack found that recent problems with fighter/attack aircraft engines have been primarily due to development concepts, procedures, and practices that did not provide the time and money to adequately develop the engines before production and use, and did.

Get this from a library. Are management problems in the acquisition of aircraft gas turbine engines being corrected?: report to the Congress. [United States. General Accounting Office.]. Get this from a library. Are management problems in the acquisition of aircraft gas turbine engines being corrected?: summary: report to the Congress.

[United States. General Accounting Office.]. Because of the magnitude of current engine problems and the criticality of engines in ensuring the success of aircraft systems, the Congress has expressed an increasing interest in the development and management of the Air Force's and Navy's aircraft gas turbine engines.

AIRCRAFT GAS TURBINE ENGINE ACQUiSITION AND LOGISTICS SUPPORT (FEBRUARY ) SCOPE The Procurement Management Review of Aircraft Gas Turbine Fngine Acquisition and Logistics Support was initiated by direction of the Deputy Chief of Staff, Systems and Logistics, Headquarters, the United States Air Size: 3MB.

Report to Congress by the Comptroller General of the U.S. PSAD – Are Management Problems in the Acquisition of Aircraft Gas Turbine Engines Being Corrected?, Septem 5.

Problems In The Acquisition of Aircraft Gas Turbine Engines Being Corrected?, Septem 5 Discussion Background. A number of high profile catastrophic or near-catastrophic instances of uncontained failure of critical engine components provide graphic illustrations of the need to maintain the structural integrity of engines.

Modern condition monitoring-based methods are used to reduce maintenance costs, increase aircraft safety, and reduce fuel consumption. In the literature, parameters such as engine fan speeds, vibration, oil pressure, oil temperature, exhaust gas temperature (EGT), and fuel flow are used to determine performance deterioration in gas turbine engines.

In this study, a new model was developed to Cited by: 4. Aircraft Gas Turbine Engines 1. 11•History•Types Of Engines used on Aircraft•Basic understanding of their operation•Sections / Modules of a Gas Turbine Engine.•Significant Components installed on the Flight Operation OfficersEngr, Zafar I.

Jami 2. Page - Are Management Problems in the Acquisition of Aircraft Gas Turbine Engines Being Corrected. Appears in 12 books from Page - US, Congress, House, Committee on Appropriations, Department of Defense Appropriations forHearings, 96th Cong., ‎.

3 GENERALITIES ABOUT GAS-TURBINE POWER PLANTS The purpose of gas-turbine power plants is to produce mechanical power from the expansion of hot gas in a turbine. In these notes we will focus on stationary plants for electric power generation, however, gas turbines are also used as jet engines in aircraft propulsion.

Aircraft propulsion 2. Taking advantage of moving within a fluid, aircraft propulsion is achieved by air-breathing engines, i.e. engines that take a stream of air and throw it at higher speed backwards. The energy source is the combustion of a fuel (carried onboard) with oxygen in the air, but it might also be solar power or nuclear Size: 1MB.

X.S. Bai TC in Gas Turbines Gas turbine for modern aviation Hans von Ohain and Max Hahn,Germany, submitted a patent for a gas turbine for jet propulsion Ernst Heinkel Aircraft Company made first true jet propulsion aircraft inAug - Sept Secundo Campiri, Italy, made a gasturbine engine for the CC-2 aircraft, File Size: 4MB.

The centrifugal compressor is more common to which type of gas turbine engine--turboshaft or large turbofan. Turboshaft The primary function of a stator vane in an axial flow compressor is to act as.

Start studying Turbine Engines Theory and Construction. Learn vocabulary, terms, and more with flashcards, games, and other study tools. The mass of the air flowing through a gas turbine engine is found by dividing its weight by a constant value that represents the _____ caused by gravity.

An efficient cruising altitude for a turbojet. The combustion process in aircraft engines and gas turbines is one in which heat is added to the compressed air in the combustor or burner.

Thus, the combustion DOI link for Aircraft Propulsion and Gas Turbine Engines. Aircraft Propulsion and Gas Turbine Engines book.

By Ahmed F. El-Sayed. Edition 2nd Edition. FUNDAMENTALS OF GAS TURBINE ENGINES INTRODUCTION The gas turbine is an internal combustion engine that uses air as the working fluid.

The engine extracts chemical energy from fuel and converts it to mechanical energy using the gaseous energy of the working fluid (air) to drive the engine and propeller, which, in turn, propel the airplane. in Aircraft Engines The principle used by a gas turbine engine as it provides force to move an airplane is based on Newton’s law of momentum.

This law states that for every action there is an equal and opposite reaction; therefore, if the engine accelerates a mass of air (action), it applies a force on the aircraft (reaction).

Engine has high exhaust gas temperature, low rpm, and high fuel flow at all engine pressure ratio settings. Engines with damage in turbine section may have tendency to hang up during starting. Engine rumbles during starting and at low power cruise conditions.

Engine has higher than normal exhaust gas temperature during takeoff, climb, and cruise. Gas-turbine engine - Gas-turbine engine - Development of gas turbines: The earliest device for extracting rotary mechanical energy from a flowing gas stream was the windmill (see above).

It was followed by the smokejack, first sketched by Leonardo da Vinci and subsequently described in detail by John Wilkins, an English clergyman, in This device consisted of a number of horizontal sails.

Designed primarily as a resource for technicians preparing for the FAA aircraft powerplant mechanic certification, Aircraft Gas Turbine Engine Technology also may be used a reference. The text also discusses the changing maintenance and overhaul procedures and philosophies and the role of fuel metering in engine operation/5(30).Readers of this book will be able to: utilize the fundamental principles of fluid mechanics and thermodynamics to analyze aircraft engines, understand the common gas turbine aircraft propulsion systems and be able to determine the applicability of each, perform system studies of aircraft engine systems for specified flight conditions, perform preliminary aerothermal design of turbomachinery.For example, many of the helicopters you see, a lot of smaller power plants and even the M-1 Tank use gas turbines.

In today’s world, gas turbine engine is widely used to generate power. It is used not only for aircraft but it is also. used to power trains, ships, electrical generator and tanks.

Gas turbine engine is a combustion engine that.