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SINCE AIR-BREATHING GAS TURBINE ENGINES HAVE BEEN USED FOR A CONSIDERABLE PERIOD OF TIME, THE TECHNOLOGY HAS REACHED THE STAGE WHERE MAJOR IMPROVEMENTS IN EITHER OVERALL PROPULSIVE CYCLE EFFICIENCY, OR THRUST TO WEIGHT REQUIRES NOVEL SYSTEM CONCEPTS.

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: N/A
Agency Tracking Number: 576
Amount: $50,000.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: N/A
Solicitation Number: N/A
Timeline
Solicitation Year: N/A
Award Year: 1983
Award Start Date (Proposal Award Date): N/A
Award End Date (Contract End Date): N/A
Small Business Information
200 Oak Drive
Syosset, NY 11791
United States
DUNS: N/A
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 ANGELO A. FERRARA
 PRINCIPAL INVESTIGATOR
 () -
Business Contact
Phone: () -
Research Institution
N/A
Abstract

SINCE AIR-BREATHING GAS TURBINE ENGINES HAVE BEEN USED FOR A CONSIDERABLE PERIOD OF TIME, THE TECHNOLOGY HAS REACHED THE STAGE WHERE MAJOR IMPROVEMENTS IN EITHER OVERALL PROPULSIVE CYCLE EFFICIENCY, OR THRUST TO WEIGHT REQUIRES NOVEL SYSTEM CONCEPTS. AFTER A CAREFUL REVIEW OF THE STATE- OF-THE-ART, IT APPEARS THAT SEVERAL CONCEPTS UTILIZING HEAT PIPE TECHNOLOGY ARE ATTRACTIVE FOR THIS PURPOSE. THE EFFORT IS TO BUILD ON THE ON-GOING RESEARCH PRESENTLY UNDERWAY AND IS TO CONSIDER COMPLEXITY, SPACE, (PERFORMANCE)IMPROVEMENTS. DESIGN EVALUATIONS ARE BASED ON A STANDARD ENGINE, SUGGESTED BY NASA FOR THIS STUDY. THE COOPERATION OF GAS TURBINE MANUFATURES IS SOLICITED TO ASSURE THAT COMMERCIALLY VIABLE CONCEPTS ARE DEVELOPED. DESIGNS ARE DEVELOPED USING HEAT PIPES TO: COOL TURBINE BLADES, AS HEAT EXCHANGERS, TO RECOVER FROM ENGINE EXHAUSTS AND TO IMPROVE COMBUSTOR DESIGN AND LIFE. CONSIDERATION OF THE (NEGATIVE) IMPACT OF SUGGESTED DESIGN CONCEPTS ON ENGINE AND VEHICLE PERFORMANCE IS MADE. EVERY EFFORT IS MADE TO UTILIZE ENERGY RECOVERY TO IMPROVE ENGINE PERFORMANCE, SUCH AS TO PREHEAT COMBUSTOR OR TURBINE INLET AIR.

* Information listed above is at the time of submission. *

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