Gas Turbine Engine Development Partnerships

1987 ◽  
Author(s):  
Jim Korn
Author(s):  
D. M. Croker ◽  
T. P. Psichogios

This paper describes the operation and salient design features of a high-speed reversing gear used with the Solar 1100-hp Saturn gas-turbine Engine. Development history leading to successful marine applications is reviewed.


1970 ◽  
Author(s):  
R. J. Mowill

The philosophy and justifications behind a large all-radial single-shaft gas turbine engine development are discussed. In addition, some of the factors affecting the marketing of a simple and low cost engine are dealt with.


Author(s):  
Y. Sumi ◽  
S. Yamazaki ◽  
K. Kinoshita

This paper describes the later progress of the Nissan YTP-12 gas turbine engine development. The mechanical design and the progress in its development are reviewed. The discussion includes mechanical arrangement, material, fuel control, major problems encountered and their solution. Component test, engine performance and durability test, and vehicle installation test are discussed briefly.


1966 ◽  
Vol 3 (01) ◽  
pp. 42-48
Author(s):  
D. M. Croker ◽  
T. P. Psichogios

This paper describes the operation and salient design features of a high-speed reversing gear used with the Solar 1100-hp Saturn gas-turbine engine. Development history leading to successful marine applications is reviewed.


Author(s):  
Roger Yee ◽  
Lee Myers ◽  
Ken Braccio ◽  
Mike Dvornak

The Navy Landing Craft Air Cushion (LCAC) Service Life Extension Program (SLEP) upgrades the current TF40B gas turbine engine and analog control system on the LCAC to an Enhanced TF40B (ETF40B) gas turbine with a Full Authority Digital Engine Control (FADEC) system. This upgrade and enhancement will provide additional engine horsepower, increased engine reliability, and modern digital engine control equipment to the LCAC. The success of the ETF40B engine development program has been an ongoing effort between the Navy, the LCAC craft builder Textron Marine & Land Systems (TM&LS), and the engine manufacturer Honeywell Engine and Systems. This paper will document and outline the differences between the TF40B and ETF40B and the efforts of the ETF40B 150 hour endurance qualification test.


Author(s):  
P. W. Pichel

This paper summarizes the scope and results to date of a program initiated in 1974 to develop a high-performance, simple-cycle, 10,000-hp engine for application in gas compressor, mechanical drive, and generator set packages. Design philosophy, a detailed description, and component and engine development testing are covered. Future plans for the development program up to the point of production availability in 1978 are also outlined.


1978 ◽  
Author(s):  
E. L. Wheeler

The Garrett GTPF990 gas turbine engine is being developed under a U.S. Navy contract to fulfill both propulsion and generator drive repuirements. This is a unique second-generation marine engine that is not derived from an aircraft engine counterpart. The engine development is nearing completion, endurance testing has started, and all other qualification testing has been conducted. This paper is a development status report. A description of the engine and special maintenance features is presented. Emphasis is placed on qualification test results, development test experience, and the resulting design improvements.


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