Michael G Drake

Address:

1819 Bellevue Ave APT 202, Seattle, WA 98122

Phone:

(206)3295061

VIN:

JTKDE177470203066

Make:

SCION

Model:

TC

Year:

2007

US Patent:

D515012, Feb 14, 2006

Filed:

Dec 28, 2004

Appl. No.:

29/220255

Inventors:

Mark E. Eatkins - Kirkland WA, US
Paul Mikulencak - Everett WA, US
R. Blake Emery - Enumclaw WA, US
Victor K. Stuhr - Seattle WA, US
Adam P. Malachowski - Lynnwood WA, US
Stephen T. Brown - Everett WA, US
Richard K. Wong - Auburn WA, US
Chester P. Nelson - Kirkland WA, US
Michael L. Drake - Bellevue WA, US
Christopher A. Vegter - Bothell WA, US
Bruce R. Detert - Seattle WA, US
Christopher A. Konings - Kirkland WA, US

Assignee:

The Boeing Company - Chicago IL

International Classification:

1212

US Classification:

D12319

US Patent:

D515013, Feb 14, 2006

Filed:

Dec 28, 2004

Appl. No.:

29/220256

Inventors:

Mark E. Eatkins - Kirkland WA, US
Paul Mikulencak - Everett WA, US
R. Blake Emery - Enumclaw WA, US
Victor K. Stuhr - Seattle WA, US
Adam P. Malachowski - Lynnwood WA, US
Stephen T. Brown - Everett WA, US
Richard K. Wong - Auburn WA, US
Chester P. Nelson - Kirkland WA, US
Michael L. Drake - Bellevue WA, US
Christopher A. Vegter - Bothell WA, US
Bruce R. Detert - Seattle WA, US
Christopher A. Konings - Kirkland WA, US

Assignee:

The Boeing Company - Chicago IL

International Classification:

1212

US Classification:

D12319

US Patent:

D516995, Mar 14, 2006

Filed:

Dec 28, 2004

Appl. No.:

29/220254

Inventors:

Mark E. Eatkins - Kirkland WA, US
Paul Mikulencak - Everett WA, US
R. Blake Emery - Enumclaw WA, US
Victor K. Stuhr - Seattle WA, US
Adam P. Malachowski - Lynnwood WA, US
Stephen T. Brown - Everett WA, US
Richard K. Wong - Auburn WA, US
Chester P. Nelson - Kirkland WA, US
Michael L. Drake - Bellevue WA, US
Christopher A. Vegter - Bothell WA, US
Bruce R. Detert - Seattle WA, US
Christopher A. Konings - Kirkland WA, US

Assignee:

The Boeing Company - Chicago IL

International Classification:

1212

US Classification:

D12319

US Patent:

D529857, Oct 10, 2006

Filed:

Aug 16, 2005

Appl. No.:

29/236425

Inventors:

Mark E. Eakins - Kirkland WA, US
Paul Mikulencak - Everett WA, US
R. Blake Emery - Renton WA, US
Victor K. Stuhr - Seattle WA, US
Adam P. Malachowski - Lynwood WA, US
Stephen T. Brown - Everett WA, US
Richard K. Wong - Auburn WA, US
Chester P. Nelson - Kirkland WA, US
Michael L. Drake - Bellevue WA, US
Christopher A. Vegter - Bothell WA, US
Bruce R. Detert - Seattle WA, US
Christopher A. Konings - Lynnwood WA, US

Assignee:

The Boeing Company - Chicago IL

International Classification:

1212

US Classification:

D12319

US Patent:

D531954, Nov 14, 2006

Filed:

Aug 16, 2005

Appl. No.:

29/236422

Inventors:

Mark E. Eakins - Kirkland WA, US
Paul Mikulencak - Everett WA, US
R. Blake Emery - Renton WA, US
Victor K. Stuhr - Seattle WA, US
Adam P. Malachowski - Lynwood WA, US
Stephen T. Brown - Everett WA, US
Richard K. Wong - Auburn WA, US
Chester P. Nelson - Kirkland WA, US
Michael L. Drake - Bellevue WA, US
Christopher A. Vegter - Bothell WA, US
Bruce R. Detert - Seattle WA, US
Christopher A. Konings - Lynwood WA, US

Assignee:

The Boeing Company - Chicago IL

International Classification:

1212

US Classification:

D12319

US Patent:

D537029, Feb 20, 2007

Filed:

Aug 16, 2005

Appl. No.:

29/236421

Inventors:

Mark E. Eakins - Kirkland WA, US
Paul Mikulencak - Snohomish WA, US
R. Blake Emery - Renton WA, US
Victor K. Stuhr - Seattle WA, US
Adam P. Malachowski - Lynwood WA, US
Stephen T. Brown - Everett WA, US
Richard K. Wong - Lynnwood WA, US
Chester P. Nelson - Kirkland WA, US
Michael L. Drake - Bellevue WA, US
Christopher A. Vegter - Bothell WA, US
Bruce R. Detert - Seattle WA, US
Christopher A. Konings - Lynnwood WA, US

Assignee:

The Boeing Company - Chicago IL

International Classification:

1212

US Classification:

D12319

US Patent:

7687927, Mar 30, 2010

Filed:

Nov 21, 2007

Appl. No.:

11/944199

Inventors:

Mark S. Shander - Mill Creek WA, US
Richard A. Cote - Mill Creek WA, US
Michael L. Drake - Bellevue WA, US
Howard Carter, III - Chesterfield MO, US
John T. Peters - Edmonds WA, US
Casey Y. K. Ng - Sammamish WA, US
Michael S. Hoag - Kent WA, US
John T. Paterson - Mukilteo WA, US

Assignee:

The Boeing Company - Chicago IL

International Classification:

H02K 7/00

US Classification:

290 7

Abstract:

An electrical architecture for an aircraft is provided. The electrical architecture is particularly suitable for relatively small, compact, and lightweight aircraft. In one embodiment, the electrical architecture includes an electrical generator component coupled to the aircraft engine, and an air compression system coupled to the electrical generator component. The electrical generator component is configured to receive mechanical power from the engine and to generate a constant frequency AC electrical power from the engine mechanical power, and the air compression system is configured to receive the constant frequency AC power as an input and, in response thereto, produce a pressurized air output having variable characteristics (for example, a variable flow rate or a variable air pressure).

US Patent:

20190270513, Sep 5, 2019

Filed:

May 21, 2019

Appl. No.:

16/418021

Inventors:

- Chicago IL, US
Mitchell Mellor - Bothell WA, US
Michael L. Drake - Bellevue WA, US
George Sonnenburg - Mukilteo WA, US

International Classification:

B64C 25/12
B64C 25/22
B64C 25/60
B64C 25/10
B64C 25/34
B64C 25/20

Abstract:

A landing gear including a shock strut assembly including an outer cylinder coupled to an airframe, a wheel movably coupled to the outer cylinder so as to reciprocate substantially along a longitudinal axis of the outer cylinder, and a shrink mechanism including a pivot arm pivotally coupled to the shock strut assembly, a drive member coupling the pivot arm to a landing gear retract mechanism, a driven member coupled to the pivot arm, a first shrink link member coupled to the pivot arm by the driven member, and a second shrink link member coupled to the first shrink link member and to the shock strut assembly. Rotation of the pivot arm by the drive member, effects a folding movement between the first shrink link member and the second shrink link member, and the folding movement effects at least a retraction of the wheel relative to the outer cylinder.