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Kendall J Fowkes

from Provo, UT
Age ~51
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Also known as:
Kendall J Fowke, James Fowkes Kendall, Kendall F
Phone and address:
1676 E 1080 S APT 4, Provo, UT 84606
Related to:
Jerry D Farmer, 74Jonathan FowkesMark A Harris, 48Nanette R Cobbley, 57Ione B Fowkes, 80Sarah Fowkes, 54Rebecca L Fowkes, 48
Connected to:
Heather L Fowkes, 51Jason A Fowkes, 45Jon Fowkes, 72Michelle D Fowkes, 40Samantha J Fowkes, 31Mark W Fowlds, 64Melissa R Fowlds, 53Maria E Fowle, 63Mary I Fowle, 79Ryan J Fowle, 28

Kendall Fowkes Phones & Addresses

  • 1676 E 1080 S APT 4, Provo, UT 84606
  • Layton, UT
  • Rexburg, ID
  • Coalinga, CA
  • Idaho Falls, ID

Work

Company: Fortem technologies Jul 2017 Position: Principal mechanical engineer

Education

Degree: Graduate or professional degree

Skills

Composites • Finite Element Analysis • Cad • Aerospace • Design For Manufacturing • Solidworks • Pro Engineer • Machine Design • Product Development

Industries

Aviation & Aerospace

Professional Records

License Records

Kendall James Fowkes

Address:
Coalinga, CA
License #:
374949-2202 - Expired
Category:
Engineer/Land Surveyor
Type:
Professional Engineer

Resumes

Resumes

Kendall Fowkes Photo 1

Principal Mechanical Engineer

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Location:
Provo, UT
Industry:
Aviation & Aerospace
Work:
Fortem Technologies
Principal Mechanical Engineer
General Atomics Aeronautical Systems
Structural Analyst and Mechanical Engineer
Skills:
Composites
Finite Element Analysis
Cad
Aerospace
Design For Manufacturing
Solidworks
Pro Engineer
Machine Design
Product Development

Publications

Us Patents

Aircraft Door

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US Patent:
20090194637, Aug 6, 2009
Filed:
Feb 4, 2008
Appl. No.:
12/025152
Inventors:
Larry J. Ashton - Mapleton UT, US
Kendall J. Fowkes - Provo UT, US
Michael G. Allman - Spanish Fork UT, US
International Classification:
B64C 1/14
US Classification:
2441295
Abstract:
A cabin door assembly is provided for use with a pressurized aircraft. The assembly includes two door halves for engaging the fuselage of the aircraft. Structurally, each door half includes a waist section integral with an adjoining tapered section. Further, the assembly includes an activator that is mounted on the fuselage and attached to the door halves. Specifically, the activator is attached to each door half to concertedly move each door half between a closed configuration and an open configuration. In the closed configuration, the door halves are sealed to the fuselage and to each other for pressurization of the aircraft. In the open configuration, the door halves extend outwardly from the fuselage to allow for aircraft ingress and egress.

Detachable Projectile Module System For Operation With A Flying Vehicle

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US Patent:
20210107654, Apr 15, 2021
Filed:
Jun 29, 2020
Appl. No.:
16/914640
Inventors:
- Pleasant Grove UT, US
David Earl JAMES - Orem UT, US
Kendall James FOWKES - Provo UT, US
Jon Erik KNABENSCHUH - Orem UT, US
Eric James FOWKES - Lehi UT, US
Justin Craig HUNTINGTON - Provo UT, US
International Classification:
B64D 7/06
F41A 19/59
F41B 11/80
F41B 11/62
F41H 13/00
B64C 39/02
F41B 11/723
Abstract:
A projectile module is attached to a gun component which operates as a system to launch a projectile at a flying device. The gun component is configured to be removably and electro-mechanically attached to a flying vehicle. A cylindrical gas valve is part of the gun component and has a safety component configured on an exterior surface of the cylindrical gas valve to enable the gun component only to attach to the flying vehicle when the projectile module is locked into position. A splitter component configured on the gun component adjacent to the cylindrical gas valve and has an output opening for gas flow. The projectile module is removable and includes weights attached to a projectile, wherein the weights are positioned in channels on the projectile module. The projectile is fired when gas flow is initiated from a reservoir the cylindrical gas valve and splitter component to the channels containing the weights.

Detachable Projectile Module System For Operation With A Flying Vehicle

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US Patent:
20200346756, Nov 5, 2020
Filed:
Mar 9, 2020
Appl. No.:
16/812699
Inventors:
- Pleasant Grove UT, US
David Earl JAMES - Orem UT, US
Kendall James FOWKES - Provo UT, US
Jon Erik KNABENSCHUH - Orem UT, US
Eric James FOWKES - Lehi UT, US
Justin Craig HUNTINGTON - Provo UT, US
International Classification:
B64D 7/06
F41A 19/59
F41B 11/80
F41B 11/62
F41H 13/00
B64C 39/02
F41B 11/723
Abstract:
A projectile module is attached to a gun component which operates as a system to launch a projectile at a flying device. The gun component is configured to be removably and electro-mechanically attached to a flying vehicle. A cylindrical gas valve is part of the gun component and has a safety component configured on an exterior surface of the cylindrical gas valve to enable the gun component only to attach to the flying vehicle when the projectile module is locked into position. A splitter component configured on the gun component adjacent to the cylindrical gas valve and has an output opening for gas flow. The projectile module is removable and includes weights attached to a projectile, wherein the weights are positioned in channels on the projectile module. The projectile is fired when gas flow is initiated from a reservoir the cylindrical gas valve and splitter component to the channels containing the weights.
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Kendall J Fowkes from Provo, UT, age ~51 Get Report