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Michael O Nebeker

from Washington, UT
Age ~62
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Also known as:
Michael E Nebeker, Michael O Nebecker, Mike Nebeker, Marlene B Nebeker, Megan Nebeker, Robert Nebeker, Lindsey Nebeker, Brandon Nebeker, Michael R, Nebeker Spenser
Related to:
Gayle H Nebeker, 87Carrie L Nebeker, 44Joseph B Roach, 37Sylvia A Nebeker, 86Brandon Nebeker, 39Trevor M NebekerStefanie W Nebeker, 52Lindsey N Nebeker, 40Whitney M Nebeker, 37Kathleen J MemmottNevelle O Nebeker, 90Marlene B Nebeker, 60
Connected to:
Adam M Nebeker, 47Amy K Nebeker, 37Clark R Nebeker, 75Cordell D Nebeker, 46Corey L Nebeker, 65David T Nebeker, 53Jeffrey Nebeker, 68Jessaca M Nebeker-Sprunt, 39Jonathan R Nebeker, 59Kim C Nebeker, 59

Michael Nebeker Phones & Addresses

  • Washington, UT
  • 2130 97Th St, Everett, WA 98205 (425) 334-6366
  • Lake Stevens, WA
  • Brooklyn, NY
  • Marysville, WA

Work

Position: President

Resumes

Resumes

Michael Nebeker Photo 1

President

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Work:

President

Publications

Us Patents

Eccentric Fastening Device

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US Patent:
7524154, Apr 28, 2009
Filed:
Nov 28, 2005
Appl. No.:
11/164509
Inventors:
Richard J. LaConte - Black Diamond WA, US
Michael O. Nebeker - Everett WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
F16B 21/02
US Classification:
411551, 411349, 4113726
Abstract:
An eccentric fastening device is provided. The eccentric fastening device includes a first threaded fastener, a base and a rotary lug providing a non-fastened pre-assembled position. The base includes a top, a bottom, a stem and a hole, where the stem axially extends from the bottom of the base, and the hole axially extends from the top through the stem of the base. The rotary lug is releasably retained in the hole of the base by the first threaded fastener. The rotary lug includes a cylindrical portion having a thread and a head, wherein the head is offset from the cylindrical portion. The cylindrical portion is substantially axially concentric with the hole of the base, allowing the head to be eccentrically rotated on or off of the stem, whereby a selective structure may be variably clamped and releasably retained between said head and said base. An aircraft having an eccentric fastening device is also provided. A method of installing the same is also provided.

Eccentric Fastening Device

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US Patent:
7761972, Jul 27, 2010
Filed:
Mar 5, 2009
Appl. No.:
12/398443
Inventors:
Richard J. LaConte - Black Diamond WA, US
Michael O. Nebeker - Everett WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B23P 11/00
US Classification:
2952502, 2952501, 2952511, 411347, 411349, 4113726
Abstract:
An eccentric fastening device is provided. The eccentric fastening device includes a first threaded fastener, a base and a rotary lug providing a non-fastened pre-assembled position. The base includes a top, a bottom, a stem and a hole, where the stem axially extends from the bottom of the base, and the hole axially extends from the top through the stem of the base. The rotary lug is releasably retained in the hole of the base by the first threaded fastener. The rotary lug includes a cylindrical portion having a thread and a head, wherein the head is offset from the cylindrical portion. The cylindrical portion is substantially axially concentric with the hole of the base, allowing the head to be eccentrically rotated on or off of the stem, whereby a selective structure may be variably clamped and releasably retained between said head and said base. An aircraft having an eccentric fastening device is also provided. A method of installing the same is also provided.

Retaining Member And Method For Use With A Seat Track

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US Patent:
20070215769, Sep 20, 2007
Filed:
Mar 15, 2006
Appl. No.:
11/376682
Inventors:
Michael Nebeker - Everett WA, US
Matthew Olson - Everett WA, US
Anthony Anderson - Mill Creek WA, US
James Ebner - Lake Stevens WA, US
International Classification:
A47B 96/06
US Classification:
248220310
Abstract:
A retaining component for securing an external structure or panel to a seat track within a mobile platform, such as an aircraft. The retaining component includes a pair of flexible flanges that are adapted to engage an external component or panel, in one example a seat track in a commercial aircraft cabin area. The retaining component also includes a base portion having a flexible portion with at least one locking tab protruding therefrom. One or more hook-shaped engaging tabs also protrude from the base portion. The engaging tabs and the locking tab enable the retaining component to be secured to a flange of a seat track having a plurality of spaced apart holes in a manner that does not require any external threaded or rivet style fastening elements, or the use of separate assembly tools. The retaining component, in one form, is a single piece, lightweight, integrally formed component that is ideally suited for use in mobile platforms such as commercial aircraft where assembly time and costs are important considerations in the manufacture of a commercial aircraft.
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Michael O Nebeker from Washington, UT, age ~62 Get Report