415 Squantum Road, PO Box 532, Jaffrey, NH 03452-6655 6035329400
Steven Walker Partner
Dyno Resource Corp. Individual and Family Social Services
P.o. Box 1585, Bellevue, WA 98027
Steven Walker Vice-president
ACCELERATION NATIONAL SERVICE CORPORATION
2390 E Camelback Rd, Phoenix, AZ 85016 14755 N Outer 40 Dr #400, Chesterfield, MO 63017 2801 Hwy 280 S, Birmingham, AL 35223
Steven G Walker Vice-President, Vice President
PROTECTIVE ADMINISTRATIVE SERVICES, INC
124 W Capitol Ave SUITE 1900, Little Rock, AR 72201 1 Chesterfield Pl 14755 North Outer 40 Dr STE 400, Wildwood, MO 63017 1 Chesterfield Mall, Wildwood, MO 63017
Steven C Walker Director
DEPOSIT GUARANTY CORP
Steven G Walker Vice-President
LYNDON FINANCIAL CORPORATION
PO Box 13008, Birmingham, AL 35202 124 W Capitol Ave STE 1900, Little Rock, AR 72201 2801 Hwy 280 S, Birmingham, AL 35223 Birmingham, AL 35223
Raymond Wilson - Athens AL, US Steven Paul Walker - Arlington WA, US Andrew Bourne - Bothell WA, US
Assignee:
B/E Aerospace, Inc. - Wellington FL
International Classification:
B64C 1/14 E05B 3/00
US Classification:
2441295, 2923363
Abstract:
An external door for use in accessing a cargo area of an aircraft fuselage. The door includes a locking system, a latching system, a lock monitoring system, an uplock used to secure the door in an open position, and an actuating system that assists in at least one of opening and closing the door. The locking system works by interfering with the movement of the latching system components. The locking system includes a monitoring device that prevents the aircraft from being pressurized in case of a malfunction in the locking system. The latching system includes a handle locking system that prevents operation of the latch handle by accident or by ground loading or flight forces. The systems of the door are preferably manually operated, and utilize rigid members.
THE BOEING COMPANY - Chicago IL, US Mark S. Good - Seattle WA, US Jan A. Kordel - Redmond WA, US Stephen J. Fox - Everett WA, US Matthew A. Lassen - Seattle WA, US Bruce Robert Fox - Everett WA, US Steven Paul Walker - Arlington WA, US Gregory M. Santini - Bothell WA, US
Assignee:
THE BOEING COMPANY - Chicago IL
International Classification:
B64C 3/56 B64C 3/58
US Classification:
2441994
Abstract:
A wing assembly comprises a raked wing tip having an outboard portion hinged to one of a main wing having at least one moveable control surface and an inboard raked wing tip portion. The outboard portion of the raked wing tip does not carry any moveable flight control surfaces.
Wing Fold System With Latch Pins Through Multiple Mating Lugs
Jan A. Kordel - Redmond WA, US Quentin Theodor Pietersen - Kirkland WA, US Steven Paul Walker - Arlington WA, US Kelly Thomas Jones - Snohomish WA, US Matthew August Lassen - Seattle WA, US Rickie Hansken - Tulalip WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64C 3/56
US Classification:
244 49
Abstract:
A wing fold system of a wing of an aircraft. The system may include a first lock of a latch to prevent movement of a latch pin of the latch to prevent movement of an unfixed portion of the wing with respect to a fixed portion of the wing, the first lock may include a first cam configured to prevent the second lock from transitioning to a second engaged position until the first lock may be in a first engaged position via contact with a second cam of the second lock. A second lock of the latch, the second lock may include the second cam configured to prevent the first lock from transitioning away from the first engaged position until the second lock transitions away from the second engaged position.
- Chicago IL, US Robert HOFFENBERG - Seattle WA, US Gregory M. SANTINI - Bothell WA, US Steven P. WALKER - Arlington WA, US
International Classification:
B64C 13/30 B64C 13/38 B64C 9/14 B64C 3/18
Abstract:
Certain aspects of the present disclosure provide techniques for an aerodynamic surface actuation system, including: a middle track connected to an aerodynamic surface and configured to move along a plurality of intermediate tracks, wherein one or more inner surfaces of the middle track are configured to interface with one or more outer surfaces of the plurality of intermediate tracks; a plurality of outer tracks, each including a flange and configured to interface with one or more inner surfaces of the plurality of intermediate tracks; and an actuator configured to control a position of the middle track and a position of the plurality of intermediate tracks via a plurality of linkages.
Example flap actuation systems and related methods are disclosed herein. An example flap actuation system includes a first actuator, a second actuator, a first drive arm coupled to the first actuator and to a flap, a second drive arm coupled to the second actuator and to the flap, a first cam, and a first output shaft. The first cam is to couple to the first drive to enable the first actuator to actuate the flap via the first drive arm. The example flap actuation system includes a second cam and a second output shaft. The first cam is to be uncoupled from the first drive arm in response to a failure of the first actuator. The second actuator is to actuate the flap via the first drive arm and the second drive arm in response to the failure of the first actuator.
- Chicago IL, US Steven Paul Walker - Arlington WA, US
Assignee:
THE BOEING COMPANY - Chicago IL
International Classification:
F16B 37/04
Abstract:
A nut plate assembly includes a base plate having base plate openings. The nut plate assembly includes channel fittings coupled to the bottom of the base plate each having a main body with a top facing the bottom of the base plate. Each channel fitting has a nut cap channel at the bottom of the main body aligned with the opening in the main body. The nut plate assembly includes nut caps received in the nut cap channels coupled to the channel fittings and positioned below the bottom of the main body. Each nut cap has a pocket holding a nut to receive a fastener used to secure the base plate to the mounting structure from an exterior surface of the mounting structure through the base plate and the main body of the channel fitting.
- Chicago IL, US Steven Paul Walker - Arlington WA, US
International Classification:
B64C 23/06 B64C 5/08
Abstract:
Aircrafts having foldable wings are disclosed. An example aircraft includes a fixed wing portion, a foldable wing tip, and a hinge interface to pivotally couple the foldable wing tip and the fixed wing portion. The hinge interface has a first hinge defining a hinge axis that is substantially parallel to a fuselage centerline. The first hinge has a first dimension in a spanwise direction and a second dimension in a chordwise direction. The first dimension is greater than the second dimension.
- Chicago IL, US Eric Gruner - Seattle WA, US Michael Addington - Seattle WA, US David Douglas Boes - Bellevue WA, US Eric Dwight Blohm - Bellevue WA, US Matthew Scott Elenbaas - Mukilteo WA, US Rickie Hansken - Marysville WA, US Mark John Herzberg - Seattle WA, US Eric Sean Kamila - Edmonds WA, US Jeffrey Michael Olds - Seattle WA, US Charuhas Soman - Bothell WA, US Keith Townsend - Everett WA, US Steven Paul Walker - Arlington WA, US
International Classification:
B64C 3/56
Abstract:
Foldable aircraft wings are disclosed. An example aircraft includes a foldable wing having a fixed wing portion, a foldable wing portion and a hinge to pivotally couple the foldable wing portion relative to the fixed wing portion. The hinge includes a wing transition portion including wing hinge ribs and wing stub ribs, respective ones of the wing hinge ribs coupled to corresponding respective ones of the wing stub ribs. The hinge also includes a tip transition portion including tip hinge ribs, where respective ends of the tip hinge ribs positioned between corresponding respective ones of the wing hinge ribs and the wing stub ribs.
Mount Carmel Medical GroupMount Carmel Columbus Cardiology Consultants West 745 W State St STE 750, Columbus, OH 43222 6142242281 (phone), 6142218869 (fax)
Mount Carmel Medical GroupMount Carmel Columbus Cardiology Consultants East 85 Mcnaughten Rd STE 300, Columbus, OH 43213 6148646644 (phone), 6142218869 (fax)
Mount Carmel Medical GroupMount Carmel Columbus Cardiology Consultants Dublin 6670 Perimeter Dr STE 100, Dublin, OH 43016 6142242281 (phone), 6142218869 (fax)
Education:
Medical School University of Cincinnati College of Medicine Graduated: 1978
Procedures:
Angioplasty Cardiac Catheterization Cardiac Stress Test Cardioversion Continuous EKG Echocardiogram Electrocardiogram (EKG or ECG) Pacemaker and Defibrillator Procedures
Dr. Walker graduated from the University of Cincinnati College of Medicine in 1978. He works in Columbus, OH and 2 other locations and specializes in Cardiovascular Disease. Dr. Walker is affiliated with Mount Carmel East Hospital, Mount Carmel St Anns Hospital and Mount Carmel West Hospital.
Medical School University of Texas Medical School at San Antonio Graduated: 1993
Languages:
English Spanish
Description:
Dr. Walker graduated from the University of Texas Medical School at San Antonio in 1993. He works in Dallas, TX and 1 other location and specializes in Anesthesiology. Dr. Walker is affiliated with Baylor Medical Center At Frisco, Baylor Scott & White Medical Center Irving and Texas Health Harris Methodist Hospital Fort Worth.
United Health Services Medical GroupUnited Health Services Walk-In Chenango Bridge 91 Chenango Brg Rd, Binghamton, NY 13901 6076484151 (phone), 6076487138 (fax)
Languages:
English
Description:
Mr. Walker works in Binghamton, NY and specializes in Family Medicine and Urgent Care Medicine. Mr. Walker is affiliated with Binghamton General Hospital, Delaware Valley Hospital, UHS Chenango Memorial Hospital and Wilson Medical Center.
Past: Sales/marketing Intern at Oldenburg Group Incorporated, Driver at Enterprise Rent-A-Car I am a 22-year-old automotive enthusiast seeking a job in the automotive, motorsports, or related industry upon graduation in June 2009