Jeff Evart Lamping, Age 59Snohomish, WA

Jeff Lamping Phones & Addresses

Snohomish, WA

Arlington, WA

Mount Vernon, WA

Mountlake Terrace, WA

Seattle, WA

Denver, CO

Kootenai, ID

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Mentions for Jeff Evart Lamping

Career records & work history

License Records

Jeff Lamping

Licenses:
License #: 54.31.2197 - Active
Issued Date: Dec 6, 1993
Expiration Date: Apr 1, 2017
Type: Fire Protection Individual
License #: 54.31.2197/1 - Active
Category: Fire Alarms/Detection
Issued Date: Jul 2, 1993

Jeff Lamping resumes & CV records

Resumes

Jeff Lamping Photo 18

Principal Engineer

Location:
15212 59Th St, Snohomish, WA 98290
Industry:
Aviation & Aerospace
Work:
Crane Aerospace & Electronics
Principal Engineer
Jeff Lamping Photo 19

Jeff Lamping

Location:
Snohomish, WA
Work:
Crane Aerospace & Electronics Companies
Principal Engineer
Crane Aerospace & Electronics
Principal Engineer
Education:
University of Washington

Publications & IP owners

Us Patents

Inductive Proximity Sensor For Detecting Ferromagnetic, Non-Permeable Or Magnet Targets

US Patent:
6507189, Jan 14, 2003
Filed:
Feb 28, 2001
Appl. No.:
09/796325
Inventors:
Kevin Woolsey - Snohomish WA
Jeff Lamping - Mountlake Terrace WA
John Marler - Woodinville WA
Bernie Burreson - Seattle WA
Steve Knudson - Seattle WA
Assignee:
Eldec Corporation - Lynnwood WA
International Classification:
G01B 714
US Classification:
32420726, 32420716
Abstract:
A core of a proximity sensor is made of a highly permeable metal and is shaped and sized to operate as a saturable core proximity sensor, a variable reluctance proximity sensor, and an eddy current proximity sensor. The core has a cross-sectional shape including a head portion, two legs extending from the head portion, and two foot portions (feet) extending from the two legs. The head portion forms a substantially planar section along the upper surface and is perpendicular to the sectional direction created by the two legs. The sectional direction of the two legs are perpendicular to the sectional direction of the two feet. The two feet are in a common plane along the bottom surface. Both foot portions are also parallel to the head portion. The cross-sectional shape of the core may further comprises two tail portions (tails), wherein each tail extends from one of the two foot portions in a direction toward the upper surface.

Position Indicating System

US Patent:
6690159, Feb 10, 2004
Filed:
Mar 16, 2001
Appl. No.:
09/810083
Inventors:
Bernard Burreson - Seattle WA
Patrick A. Knappert - Lynnwood WA
Kevin G. Woolsey - Snohomish WA
Jeff Lamping - Mountlake Terrace WA
Alan Orr - Woodinville WA
Assignee:
Eldec Corporation - Lynnwood WA
International Classification:
G01B 714
US Classification:
32420723, 32420724, 32420725, 32420712
Abstract:
A target device is carried by or mounted on a first part movable relative to a second part. The second part has a sensing device including an array of sensors providing outputs responsive to the magnet field of the target device. A processing device receives the outputs of the sensors and calculates relative positions of the two parts based on the outputs.

Aircraft Tire Pressure Loop Link

US Patent:
8059014, Nov 15, 2011
Filed:
Mar 23, 2009
Appl. No.:
12/409432
Inventors:
Jeff Lamping - Snohomish WA, US
Mark Finefrock - Lake Stevens WA, US
Assignee:
Eldec Corporation - Lynnwood WA
International Classification:
G08B 21/00
US Classification:
340945, 3405681, 340444
Abstract:
The aircraft tire pressure loop link is formed of first and second single metal loops connected by parallel spaced apart metal shafts, and provides for coupling a magnetic field between a wheel hub coil and a tire pressure sensor coil to provide electromagnetic communication between a control unit connect to the wheel hub coil and a tire pressure sensor connected to the tire pressure sensor coil; the current induced in the first single metal loop travels the distance from the edge of the wheel axle coil to the periphery of the of the wheel rim to the second single metal loop, which generates the flux in the tire pressure sensor receiver coil necessary to power the tire pressure sensor.

Aircraft Tire Pressure Loop Link

US Patent:
8305237, Nov 6, 2012
Filed:
Nov 4, 2011
Appl. No.:
13/289555
Inventors:
Jeff Lamping - Snohomish WA, US
Mark Finefrock - Lake Stevens WA, US
Assignee:
Eldec Corporation - Lynwood WA
International Classification:
G08B 21/00
US Classification:
340945, 3405681, 340444
Abstract:
The aircraft tire pressure loop link is formed of first and second single metal loops connected by parallel spaced apart metal shafts, and provides for coupling a magnetic field between a wheel hub coil and a tire pressure sensor coil to provide electromagnetic communication between a control unit connect to the wheel hub coil and a tire pressure sensor connected to the tire pressure sensor coil. The current induced in the first single metal loop travels the distance from the edge of the wheel axle coil to the periphery of the of the wheel rim to the second single metal loop, which generates the flux in the tire pressure sensor receiver coil necessary to power the tire pressure sensor.

Aircraft Tire Pressure Loop Link

US Patent:
8519869, Aug 27, 2013
Filed:
Mar 30, 2012
Appl. No.:
13/436616
Inventors:
Jeff Lamping - Snohomish WA, US
Igal Goniodsky - Kirkland WA, US
Assignee:
ELDEC Corporation - Lynwood WA
International Classification:
G08B 21/00
US Classification:
340945, 3404255, 3405681
Abstract:
The aircraft tire pressure loop link is formed of first and second single metal loops connected by parallel spaced apart metal shafts, and provides for coupling a magnetic field between a wheel hub coil and a tire pressure sensor coil to provide electromagnetic communication between a control unit connect to the wheel hub coil and a tire pressure sensor connected to the tire pressure sensor coil. The current induced in the first single metal loop travels the distance from the edge of the wheel axle coil to the periphery of the of the wheel rim to the second single metal loop, which generates the flux in the tire pressure sensor receiver coil necessary to power the tire pressure sensor.

Inductive Proximity Sensor For Detecting Ferromagnetic, Non-Permeable Or Magnet Targets

US Patent:
6424145, Jul 23, 2002
Filed:
Feb 29, 2000
Appl. No.:
09/515557
Inventors:
Kevin Woolsey - Snohomish WA
Jeff Lamping - Mountlake Terrace WA
John Marler - Woodinville WA
Bernie Burreson - Seattle WA
Steve Knudson - Seattle WA
Assignee:
Eldec Corporation - Lynnwood WA
International Classification:
G01R 3500
US Classification:
324202, 32420716, 32420726
Abstract:
An omega-shaped core is wrapped with two coils arranged to be responsive to magnetic permeable metal and conductive metal objects. The omega core allows the proximity sensor to operate as a saturated core sensor, a variable reluctance sensor or an eddy current loss sensor. The core is made from a thin, highly permeable metal that is preferably formed from a single piece of sheet metal, and comprises a substantially flat, rectangular member bent in four locations to form a head portion, two legs, and two feet. The bends form right angles so that the head portion is perpendicular to the two legs, and the two legs are perpendicular to the two feet. The two feet are parallel to each other and also parallel to the head portion. The core is positioned in a housing with two inductive coils, each coil being positioned around a leg portion of the core. A calibration bolt can be placed through the center of the core to change the level of inductance measured from the two inductive coils.

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