John W Standley, Age 64Rancho Cucamonga, CA

John Standley Phones & Addresses

Rancho Cucamonga, CA

Las Vegas, NV

386 Emma Ave, Ventura, CA 93003 (805) 658-7896

11155 Citrus Dr #75, Ventura, CA 93004 (805) 658-7896

Renton, WA

Camarillo, CA

7137 Sixshooter Dr, Las Vegas, NV 89119

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Work

Company: United states air force May 2009 Position: Accounting technician

Education

School / High School: Citrus College- Glendora, CA 2006 Specialities: Emergency Medical Technician

Mentions for John W Standley

Resumes

Resumes

John Standley Photo 1

John Standley - Glendale, AZ

Work:
United States Air Force May 2009 to 2000
Accounting Technician
Chipotle Mexican Grill - Glendora, CA Jul 2006 to Apr 2009
Crew Member
Education:
Citrus College - Glendora, CA 2006 to 2007
Emergency Medical Technician
Sierra High School Glendora - Glendora, CA 2002 to 2006

Business Records

Name / TitleCompany / ClassificationPhones & Addresses
John E. Standley J.E.S. EXPERT SERVICES LLC
John Standley HEARTLAND BAPTIST CHURCH, INC

Publications

Us Patents

Systems And Methods For Controlling Aircraft Flaps And Spoilers

US Patent:
7891611, Feb 22, 2011
Filed:
Dec 28, 2007
Appl. No.:
11/966361
Inventors:
Neal V. Huynh - Bellevue WA,
Robert J. Bleeg - Mercer Island WA,
Ralph Scott Pepper - Everett WA,
John A. Standley - Seattle WA,
Brian L. Bocksch - Seattle WA,
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64C 3/50
US Classification:
244215, 244217, 244213
Abstract:
Systems and methods for controlling aircraft flaps and spoilers are disclosed. Systems in accordance with some embodiments include a wing having a trailing edge, and a flap positioned at least partially aft of the wing trailing edge and being deployable relative to the wing between a first flap position and a second flap position by operation of a first actuator. A spoiler can be positioned at least proximate to the trailing edge and can be movable among at least three positions, including a first spoiler position in which the spoiler forms a generally continuous contour with an upper surface of the wing, a second spoiler position deflected downwardly from the first, and a third spoiler position deflected upwardly from the first. A second actuator can be operatively coupled to the spoiler to move the spoiler among the first, second and third spoiler positions in a manner that is mechanically independent of the motion of the flap.

Systems And Methods For Controlling Aircraft Flaps And Spoilers

US Patent:
2006017, Aug 10, 2006
Filed:
Feb 4, 2005
Appl. No.:
11/051738
Inventors:
Neal Huynh - Seattle WA,
Robert Bleeg - Seattle WA,
Ralph Pepper - Seattle WA,
John Standley - Seattle WA,
Brian Bocksch - Seattle WA,
International Classification:
B64C 9/22
US Classification:
244212000
Abstract:
Systems and methods for controlling aircraft flaps and spoilers are disclosed. Systems in accordance with some embodiments include a wing having a trailing edge, and a flap positioned proximate to the wing trailing edge and being deployable relative to the wing between a first flap position and a second flap position by operation of a first actuator. A spoiler can be positioned at least proximate to the trailing edge and can be movable among at least three positions, including a first spoiler position in which the spoiler forms a generally continuous contour with an upper surface of the wing, a second spoiler position deflected downwardly from the first, and a third spoiler position deflected upwardly from the first. A second actuator can be operatively coupled to the spoiler to move the spoiler among the first, second and third spoiler positions in a manner that is mechanically independent of the motion of the flap.

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