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Turbine Burner for Near-Constant Temperature Cycle Gas Turbine Engine

Award Information

Agency:
Department of Defense
Branch:
Air Force
Award ID:
55282
Program Year/Program:
2001 / SBIR
Agency Tracking Number:
001PR-1735
Solicitation Year:
N/A
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Small Business Information
Innovative Scientific Solutions, Inc.
7610 McEwen Rd. Dayton, OH 45459-
View profile »
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
 
Phase 1
Fiscal Year: 2001
Title: Turbine Burner for Near-Constant Temperature Cycle Gas Turbine Engine
Agency / Branch: DOD / USAF
Contract: F33615-01-C-2133
Award Amount: $0.00
 

Abstract:

The proposed Phase II SBIR addresses the question of how the potential performance benefits demonstrated for the constant-temperature cycle aircraft gas turbine may actually be realized in an engine. The approach used is to take the engine design choicesand cycle performance for a constant-temperature cycle high bypass ratio, high thrust turbofan from the Phase I results, and layout the engine using a mean-line design process for component sizing and configuration. The proposal includes an enablingtechnology assessment, combustion component concept definition, sizing and performance evaluation, and an overall engine viability and risk assessment. The overall objective is to demonstrate that the constant-temperature cycle gas turbine engine concepthas the potential to be turned into a viable piece of turbo-machinery while achieving its performance benefits.

Principal Investigator:

Geoffrey Sturgess
Senior Combustion Enginee
9372522706
sturgess@innssi.com

Business Contact:

Larry Goss
President
9374294980
gosslp@innssi.com
Small Business Information at Submission:

INNOVATIVE SCIENTIFIC SOLUTIONS, INC.
2766 Indian Ripple Rd Dayton, OH 45440

EIN/Tax ID: 311437643
DUNS: N/A
Number of Employees:
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No