Accession Number : ADA139457

Title :   Thermal Energy Recovery in Gas Turbine Engine Test Cells.

Descriptive Note : Final rept. Oct 82-Sep 83,

Corporate Author : NAVAL CIVIL ENGINEERING LAB PORT HUENEME CA

Personal Author(s) : Kodres,C A

PDF Url : ADA139457

Report Date : Nov 1983

Pagination or Media Count : 112

Abstract : The economics of thermal energy recovery in jet engine test cells is examined. A numerical model to simulate the test cell augmenter tube is developed. This model is employed to determine the feasibility of installing heat exchangers along the augmenter or at the augmenter exit and using these heat exchangers to generate steam or electricity from the thermal energy in the jet exhaust. In general, energy recovery is not practical. The exhaust is quickly diluted by the entrained augmentation air, decreasing temperature gradients necessary for heat transfer. Most test cells are used too infrequently to warrant the cost of the hardware. (Author)

Descriptors :   *Jet engine exhaust, *Heat recovery, *Test facilities, *Heat exchangers, Installation, Naval shore facilities, Heat transfer, Mathematical models, Mass flow, Air entrainment, Temperature gradients, Flow rate, Energy conversion, Gas turbines, Maintenance, Repair, Cost effectiveness, Mathematical prediction, Feasibility studies, Computer programs

Subject Categories : Non-electrical Energy Conversion
      Air Condition, Heating, Lighting & Ventilating
      Test Facilities, Equipment and Methods

Distribution Statement : APPROVED FOR PUBLIC RELEASE