David L Carlile, Age 601158 Kensington Way, Richland, WA 99352

David Carlile Phones & Addresses

1158 Kensington Way, Richland, WA 99352 (509) 628-1956

Kennewick, WA

Pasco, WA

Simi Valley, CA

Mentions for David L Carlile

Career records & work history

Lawyers & Attorneys

David Carlile Photo 1

David Carlile - Lawyer

Specialties:
Commercial Law, Criminal Law/Intervention/Compensation, Defamation, Media & Entertainment, Family Law/De Facto, Probate/Wills/TFM, Property Law
ISLN:
922172205
Admitted:
1995

David Carlile resumes & CV records

Resumes

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Publications & IP owners

Us Patents

Systems And Methods For Recovering An Airship

US Patent:
8070096, Dec 6, 2011
Filed:
Aug 13, 2008
Appl. No.:
12/191152
Inventors:
Wilfred L. Wood - Canyon Country CA, US
Timothy W. Blunck - Rosamond CA, US
David E. Carlile - Quartz Hill CA, US
Assignee:
Lockheed Martin Corporation - Bethesda MD
International Classification:
B64C 1/12
US Classification:
244116, 244115, 244110 E
Abstract:
An airship recovery system is disclosed including a first cushion pad configured to create a suction force on an outer portion of the airship to capture the airship during landing. An arm is coupled to the first cushion pad and movable between at least two different vertical positions. In an embodiment the air is movable in multiple degrees of freedom. An actuator device is coupled to move the arm. A sensor device is incorporated to detect the location of the airship relative to the recovery system. A controller is utilized to receive signals from the sensor device regarding the location of the airship and output command signals to the actuator to move the arm and the first cushion pad toward a desired contact location on the airship.

Propulsion System For A Lighter-Than-Air Vehicle

US Patent:
5368256, Nov 29, 1994
Filed:
Aug 19, 1993
Appl. No.:
8/108280
Inventors:
John B. Kalisz - Newhall CA
David E. Carlile - Lancaster CA
Assignee:
Lockheed Corporation - Calabasas CA
International Classification:
B65B 130
B65B 134
US Classification:
244 26
Abstract:
The invention is a propulsion system for a lighter-than-air vehicle. In detail the propulsion system includes a pylon having a longitudinal axis and first and second ends, the first end of the pylon rotatably mounted to the vehicle and the second end extending outward from the vehicle. The pylon is rotatable about the first end in a plane perpendicular to the longitudinal axis of the vehicle. A thrust producing assembly is mounted on the second end of the pylon and is rotatable about an axis of rotation in a plane perpendicular to the longitudinal axis of the pylon. A powerplant assembly is coupled to the thrust producing assemblies to provide power thereto. An actuation system is provided for rotating the assembly about the axis of rotation. A second actuation system is provided for rotating the pylon about the first end.

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