Gas Turbine Engine Picture
Report Number: ASD-TDR-62-465 p. 37-40
Author(s): Schumacher, H. E.
Corporate Author(s): Wright Air Development Division
Date of Publication: 1962-05
Pages: 4
Contract: AF 33(616)-7223
DoD Project: 3044
DoD Task: 30169
Identifier: This paper is part of a conference proceedings. See AD0278843
Abstract:
The gas turbine engine continues as a major source of propulsion effort for advanced systems being programmed into the Air Force inventory. Successful operation of these engines will be dependent on several critical improvements in high-temperature operating materials, one such limiting material is the lubricant. In addition, future lubricants will be expected to serve as hydraulic fluid for engine systems. Therefore a major decrease in the rate of internal contaminant generation must also be programmed.
Author(s): Schumacher, H. E.
Corporate Author(s): Wright Air Development Division
Date of Publication: 1962-05
Pages: 4
Contract: AF 33(616)-7223
DoD Project: 3044
DoD Task: 30169
Identifier: This paper is part of a conference proceedings. See AD0278843
Abstract:
The gas turbine engine continues as a major source of propulsion effort for advanced systems being programmed into the Air Force inventory. Successful operation of these engines will be dependent on several critical improvements in high-temperature operating materials, one such limiting material is the lubricant. In addition, future lubricants will be expected to serve as hydraulic fluid for engine systems. Therefore a major decrease in the rate of internal contaminant generation must also be programmed.
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