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John Kusnierek Phones & Addresses

  • Fairborn, OH
  • 3652 Fowler Rd, Springfield, OH 45502 (937) 325-0371
  • Burke, VA
  • 10340 Layton Hall Dr, Fairfax, VA 22030 (703) 865-6077
  • Clifton, VA
  • Oklahoma City, OK
  • 7915 Hill Stream Ct, Springfield, VA 22153 (757) 291-5057

Work

Position: Construction and Extraction Occupations

Education

Degree: Associate degree or higher

Business Records

Name / Title
Company / Classification
Phones & Addresses
John Kusnierek
Owner
John A Kusnierek
Business Consulting Services
5841 Banning Pl, Springfield, VA 22015

Publications

Us Patents

System And Method Of Transferring Power In A Gas Turbine Engine

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US Patent:
20200109669, Apr 9, 2020
Filed:
Dec 10, 2019
Appl. No.:
16/709182
Inventors:
- Indianapolis IN, US
John Kusnierek - Springfield OH, US
Assignee:
Rolls-Royce North American Technologies Inc. - Indianapolis IN
International Classification:
F02C 9/20
F02C 3/113
F02C 3/04
F02K 3/02
Abstract:
A method of extracting work from a convertible gas turbine engine having a core flowpath and a bypass flowpath. The method comprises operating the convertible gas turbine engine at a first volumetric flow rate through the core flowpath and a second volumetric flow rate through the bypass flowpath to produce a first work output of the convertible gas turbine engine; extracting the first work output via an unshrouded fan and a shaft at a first fan to shaft extraction ratio; altering the second volumetric flowrate through the bypass flowpath while maintaining the first work output; and extracting the first work output via an unshrouded fan and a shaft at a second fan to shaft extraction ratio.

Socket Ignition Connector For Model Rockets

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US Patent:
20200049105, Feb 13, 2020
Filed:
Aug 12, 2018
Appl. No.:
16/101494
Inventors:
John Jerome Kusnierek - Springfield OH, US
Jeffrey Richard DeWispelaere - Elk River MN, US
International Classification:
F02K 9/95
Abstract:
One embodiment of an application of micro-electronic socket pin connectors to model rocketry for the purpose of ignition of single or clustered solid model rocket motors. A socket based model rocket ignition connector is created by utilizing an appropriately sized low insertion force machine pin socket connector with electrical leads and potting such that model rocket igniter wires are simply placed into the sockets by hand pressure and sufficiently retained place by the functionality of the machine pin socket. The advantages of this embodiment include elimination of shorting failure modes, long service life, high success rate in clustered model rocket engines and being particularly helpful in educational settings with first time users. Other embodiments are described and shown.

System And Method Of Transferring Power In A Gas Turbine Engine

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US Patent:
20170191427, Jul 6, 2017
Filed:
Jan 4, 2016
Appl. No.:
14/987271
Inventors:
- Indianapolis IN, US
John Kusnierek - Springfield OH, US
Assignee:
Rolls Royce North American Technologies Inc - Indianapolis IN
International Classification:
F02C 9/20
F02C 3/04
F02C 3/113
F02K 3/02
Abstract:
A method of extracting work from a convertible gas turbine engine having a core flowpath and a bypass flowpath. The method comprises operating the convertible gas turbine engine at a first volumetric flow rate through the core flowpath and a second volumetric flow rate through the bypass flowpath to produce a first work output of the convertible gas turbine engine; extracting the first work output via an unshrouded fan and a shaft at a first fan to shaft extraction ratio; altering the second volumetric flowrate through the bypass flowpath while maintaining the first work output; and extracting the first work output via an unshrouded fan and a shaft at a second fan to shaft extraction ratio.
John A Kusnierek from Fairborn, OH, age ~44 Get Report