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Jeffrey Joshua Shutrump

from Lakeside, CA
Age ~40
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Also known as:
Jeffrey J Shutrump, Joshua Shutrump, Jeffery J Shutrump, Jeffery D Shutrump, Joshua P
Related to:
William G Shutrump, 42John J Ressler, 45Tiffany Shutrump, 41Ashley B Ressler, 36Joleen D Dooley, 48Carline J ShutrumpCynthia M Shutrump, 62Jeremy D Shutrump, 36Linda M Ressler, 71Kenneth ResslerJennifer Jasper, 41Nicole A Kehrli, 44Uletine M ShutrumpKenneth Ressler, 75Kenneth J Ressler, 41
Connected to:
Alexis K Shutrump, 39John M Shutske, 63Alice L Shutt, 66Angela R Shutt, 50Breanna W Shutt, 45Chris L Shutt, 66Claire Shutt, 33Dawn J Shutt, 36Gary L Shutt, 65Gloria J Shutt, 75

Jeffrey Shutrump Phones & Addresses

  • Lakeside, CA
  • 1440 Oakdale Ave #20, El Cajon, CA 92021 (619) 334-8649
  • 1500 E Lexington Ave, El Cajon, CA 92019 (619) 733-7617
  • 1204 Halley Ct, Chula Vista, CA 91911 (619) 733-9536 (619) 482-9516
  • Encinitas, CA
  • Escondido, CA
  • Santee, CA
  • San Diego, CA

Publications

Us Patents

Aircraft Engine Inlet Having Zone Of Deformation

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US Patent:
8438857, May 14, 2013
Filed:
Apr 7, 2010
Appl. No.:
12/755589
Inventors:
Jeffrey D. Shutrump - Chula Vista CA, US
Assignee:
Rohr, Inc. - Chula Vista CA
International Classification:
F02C 1/00
US Classification:
60772, 602261, 244 53 B, 137 151, 4152151
Abstract:
An inlet assembly for an aircraft engine nacelle includes an inner barrel, an outer barrel radially spaced from the inner barrel, and a rear support for supporting the outer barrel relative to the inner barrel. The rear support includes at least one radially extending stiffener and at least one energy absorber defining a zone of deformation adjacent the inner barrel. The rear support is deformable in the zone of deformation in response to forces applied during a fan blade-out event to prevent fracture of the rear support.

Aircraft Engine Inlet Having Zone Of Deformation

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US Patent:
20080016844, Jan 24, 2008
Filed:
Jul 19, 2006
Appl. No.:
11/488980
Inventors:
Jeffrey D. Shutrump - Chula Vista CA, US
International Classification:
F02K 3/02
US Classification:
602261
Abstract:
An inlet assembly for an aircraft engine nacelle includes an inner barrel, an outer barrel radially spaced from the inner barrel, and a rear support for supporting the outer barrel relative to the inner barrel. The rear support includes at least one radially extending stiffener and at least one energy absorber defining a zone of deformation adjacent the inner barrel. The rear support is deformable in the zone of deformation in response to forces applied during a fan blade-out event to prevent fracture of the rear support.
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Jeffrey Joshua Shutrump from Lakeside, CA, age ~40 Get Report