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Gregory Joseph Vering

from Kirkland, WA
Age ~41
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Also known as:
Gregory J Vering, Joseph G Vering, Gregory J Verning
Phone and address:
11715 90Th Ave NE, Kirkland, WA 98034
Related to:
Isaiah VeringJobreen Vering, 72
Connected to:
Ilske F Veringa, 69Linda J Vering, 54Marie A Verini, 32Norma Verino, 42William W Verish, 41Augusto V Verissimo, 61Derek Verissimo, 44Laurel K Verissimo, 68Linda T Verissimo, 76Mario D Verissimo, 87

Gregory Vering Phones & Addresses

  • 11715 90Th Ave NE, Kirkland, WA 98034
  • 5828 14Th St, Everett, WA 98203 (425) 322-5021 (425) 374-7814
  • 505 74Th St SW, Everett, WA 98203
    • s
  • 7937 Densmore Ave N, Seattle, WA 98103
  • Shoreline, WA
  • Kent, WA
  • Carmel, CA
  • Snohomish, WA
  • 7054 Valley Greens Cir, Carmel, CA 93923 (831) 214-1067

Work

Company: Boeing commercial airplanes Oct 2012 Address: Everett, Wa Position: Structural design engineer

Education

Degree: Civil Engineering School / High School: Santa Clara University 2002 to 2006

Skills

Catia • Aircraft • Engineering • Aerospace • Composites • Aerospace Engineering • Aircraft Design • Structural Engineering • Fatigue Analysis • Stress Analysis • Aerodynamics • Finite Element Analysis • Pro Engineer • Aeronautics • Systems Engineering • Mechanical Engineering • Design Engineering • Metals • Kinematics • Damage Tolerance • Enovia Lca • Composite Structures • Engineering Management • Product Development • Computer Aided Design • Lms Virtual.lab • Landing Gear

Industries

Aviation & Aerospace

Resumes

Resumes

Gregory Vering Photo 1

Gregory Vering

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Location:
11715 90Th St, Kirkland, WA 98033
Industry:
Aviation & Aerospace
Work:
Boeing Commercial Airplanes - Everett, Wa since Oct 2012
Structural Design Engineer
Boeing Commercial Airplanes - Gifu, Japan Sep 2011 - Sep 2012
Structural Design Engineer
Boeing Commercial Airplanes - Everett, WA Aug 2006 - Aug 2011
Structural Design Engineer
Education:
Santa Clara University 2002 - 2006
Civil Engineering
Skills:
Catia
Aircraft
Engineering
Aerospace
Composites
Aerospace Engineering
Aircraft Design
Structural Engineering
Fatigue Analysis
Stress Analysis
Aerodynamics
Finite Element Analysis
Pro Engineer
Aeronautics
Systems Engineering
Mechanical Engineering
Design Engineering
Metals
Kinematics
Damage Tolerance
Enovia Lca
Composite Structures
Engineering Management
Product Development
Computer Aided Design
Lms Virtual.lab
Landing Gear

Publications

Us Patents

Landing Gear Shrink Link Mechanism

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US Patent:
20210276697, Sep 9, 2021
Filed:
Mar 1, 2021
Appl. No.:
17/188198
Inventors:
- Chicago IL, US
Leanne M. CAMPBELL - Snohomish WA, US
Gabriela K. DEFRANCISCI - Edmonds WA, US
Gregory J. VERING - Seattle WA, US
Aaron P. KNOCK - Seattle WA, US
Mitchell MELLOR - Bothell WA, US
Justin D. COTTET - Snohomish WA, US
International Classification:
B64C 25/20
B64C 25/60
B64C 25/12
Abstract:
A shrink mechanism for use with a landing gear of an aircraft. The landing gear includes an outer cylinder rotatably coupled to a frame of an aircraft about a trunnion axis of rotation and a shock strut assembly movably coupled to the outer cylinder so as to reciprocate along a longitudinal axis of the outer cylinder. The shrink mechanism incudes a first shrink link member pivotally coupled to the outer cylinder, a second shrink link member coupling the first shrink link member to the shock strut assembly, a crank member pivotally coupled to the outer cylinder, a drive member coupling the crank member to a walking beam of a landing gear retract mechanism, and a driven member coupling the crank member to the first shrink link member.

Landing Gear Shrink Link Mechanism

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US Patent:
20200031457, Jan 30, 2020
Filed:
Jul 30, 2018
Appl. No.:
16/049090
Inventors:
- Chicago IL, US
Leanne M. CAMPBELL - Snohomish WA, US
Gabriela K. DEFRANCISCI - Edmonds WA, US
Gregory J. VERING - Seattle WA, US
Aaron P. KNOCK - Seattle WA, US
Mitchell MELLOR - Bothell WA, US
Justin D. COTTET - Snohomish WA, US
International Classification:
B64C 25/10
B64C 25/60
Abstract:
A landing gear including an outer cylinder rotatably coupled to a frame of an aircraft about a trunnion axis of rotation, a shock strut assembly movably coupled to the outer cylinder so as to reciprocate along a longitudinal axis of the outer cylinder, and a shrink mechanism including a first shrink link member pivotally coupled to the outer cylinder, a second shrink link member coupling the first shrink link member to the shock strut assembly, a crank member pivotally coupled to the outer cylinder, a drive member coupling the crank member to a walking beam (a.k.a. retract actuator beam) of a landing gear retract mechanism, and a driven member coupling the crank member to the first shrink link member.
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Gregory Joseph Vering from Kirkland, WA, age ~41 Get Report