DAVID SCOTT STAPP
Pilots at Medomak Rd, Medomak, ME

License number
Maine A2146192
Issued Date
Nov 2015
Expiration Date
Nov 2016
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
320 Medomak Rd, Medomak, ME 04551
LicenseFiles verified this license of May 6, 2017 at the Federal Aviation Administration.

Professional information

David Stapp Photo 1

Ceo/Cto At Peregrine Turbine Technologies, Llc
Position:
CEO/CTO at Peregrine Turbine Technologies, LLC, Owner at Ocean Point Aviation, LLC, Owner at Peregrine Consulting, Inc, President at Peregrine Consulting, Inc.
Location:
Bremen, Maine
Industry:
Defense & Space
Work:
Peregrine Turbine Technologies, LLC - Wiscasset, ME since Jan 2012 - CEO/CTO Ocean Point Aviation, LLC since May 2007 - Owner Peregrine Consulting, Inc since May 1996 - Owner Peregrine Consulting, Inc. since May 1996 - President GE Aircraft Engines Lynn 1986 - 1991 - Mechanical Engineer - Rotating Parts Design GE Aircraft Engines 1986 - 1989 - Mech Engineer
Education:
University of Colorado Boulder 1978 - 1985
BSME, Mechanical Engineering, Fine Arts
Skills:
Product Development, Aerospace, Aviation, Aircraft, Airports, Engineering Management, Engineering, Project Management, Systems Engineering, Start-ups, Entrepreneurship, Program Management, Six Sigma, Helicopters, Mechanical Engineering
Languages:
Spanish

David Stapp Photo 2

System And Method For Generating Power Using A Supercritical Fluid

US Patent:
2013018, Jul 18, 2013
Filed:
Nov 16, 2012
Appl. No.:
13/679856
Inventors:
David S. Stapp - Bremen ME, US
International Classification:
F02C 3/04
US Classification:
60773, 60793
Abstract:
A dual cycle system for generating shaft power using a supercritical fluid and a fossil fuel. The first cycle is an open, air breathing Brayton cycle. The second cycle is a closed, supercritical fluid Brayton cycle. After compression of air in the first cycle, the compressed air flows through a first cross cycle heat exchanger through which the supercritical fluid from the second cycle flows after it has been compressed and then expanded in a turbine. In the first cross cycle heat exchanger, the compressed air is heated and the expanded supercritical fluid is cooled. Prior to expansion in a turbine, the compressed supercritical fluid flows through a second cross cycle heat exchanger through which also flows combustion gas, produced by burning a fossil fuel in the compressed air in the first cycle. In the second cross cycle heat exchanger, the combustion gas is cooled and the compressed supercritical fluid is heated.