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Vaughn R Kunze

from Lebanon, OH
Age ~45
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Also known as:
Vaughn Natalie Kunze, Vaughn R Kunzee
Related to:
Alexandra Lang, 31Ann Artrip, 54Douglas Lang, 67Dale Kunze, 57Keith Artrip, 65
Connected to:
Albert J Kunze, 93Anna J Kunze, 75Beth M Kunze, 57Dan Kunze, 66Hannah M Kunze, 34Janet O Kunze, 58Jared Kunze, 35Jarrod S Kunze, 45Jason M Kunze, 51Jennie R Kunze, 52

Vaughn Kunze Phones & Addresses

  • Lebanon, OH
  • Mason, OH
  • Brookfield, WI
  • 7127 County Road 30, Mount Gilead, OH 43338
  • 3537 Emeraldcut Dr, Dayton, OH 45431
  • Beavercreek, OH
  • Ada, OH
  • Lebanon, OH
  • Warren, OH
  • 3712 Township Road 61, Mount Gilead, OH 43338

Publications

Us Patents

Turbofan Engine Mixer Assembly

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US Patent:
20130104555, May 2, 2013
Filed:
Oct 31, 2011
Appl. No.:
13/285826
Inventors:
Mustafa Dindar - Cincinnati OH, US
Vaughn Kunze - Lebanon OH, US
International Classification:
F02C 7/00
US Classification:
60770
Abstract:
A mixer for mixing flows in a turbofan engine is provided. The mixer includes a plurality of chevron lobes, each of the plurality of lobes comprising a crown, a keel, a first trailing edge, a second trailing edge, and a first transverse edge extending between first trailing edge and second trailing edge, said mixer configured to receive two separate incoming exhaust flows and mix the two flows into at least one rotational exhaust flow that is ejected out at least one of said first trailing edge and said second trailing edge.

Variable Immersion Lobe Mixer For Turbofan Jet Engine Exhaust And Method Of Fabricating The Same

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US Patent:
20150107225, Apr 23, 2015
Filed:
Apr 26, 2013
Appl. No.:
14/396800
Inventors:
- Schenectady NY, US
Vaughn Ray Kunze - Cincinnati OH, US
International Classification:
F02K 1/38
F02K 1/48
US Classification:
60262, 29888012
Abstract:
A method of fabricating a mixer for a gas turbine engine is provided. The method includes forming a forward end and an aft end of the mixer, and forming an annularly undulating contour that defines a plurality of core immersion lobes and a plurality of bypass immersion lobes between the forward end and the aft end. The plurality of bypass immersion lobes includes a first bypass immersion lobe and a second bypass immersion lobe. The first bypass immersion lobe has a first crown contour line extending from the forward end to the aft end of the mixer, and the second bypass immersion lobe has a second crown contour line extending from the forward end to the aft end of the mixer. The first crown contour line is different than the second crown contour line.
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Vaughn R Kunze from Lebanon, OH, age ~45 Get Report