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Patent Assignment Details
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Reel/Frame:004103/0513   Pages: 2
Recorded: 03/09/1983
Conveyance: ASSIGNMENT OF ASSIGNORS INTEREST.
Total properties: 6
1
Patent #:
Issue Dt:
08/21/1984
Application #:
06369300
Filing Dt:
04/16/1982
Title:
HELICOPTER ENGINE CONTROL WITH ROTOR SPEED DECAY ANTICIPATOR
2
Patent #:
Issue Dt:
01/03/1984
Application #:
06369301
Filing Dt:
04/16/1982
Title:
FUEL CONTROL FOR CONTROLLING HELICOPTER ROTOR/TURBINE ACCELERATION
3
Patent #:
Issue Dt:
12/11/1984
Application #:
06369302
Filing Dt:
04/16/1982
Title:
HELICOPTER CRUISE FUEL CONSERVING ENGINE CONTROL
4
Patent #:
Issue Dt:
01/15/1985
Application #:
06369481
Filing Dt:
04/16/1982
Title:
HELICOPTER ENGINE TORQUE COMPENSATOR
5
Patent #:
Issue Dt:
06/12/1984
Application #:
06369494
Filing Dt:
04/19/1982
Title:
TORSIONAL MODE SUPPRESSOR
6
Patent #:
Issue Dt:
02/19/1985
Application #:
06382258
Filing Dt:
05/26/1982
Title:
SUPER CONTINGENCY AIRCRAFT ENGINE CONTROL
Assignor
1
Exec Dt:
02/25/1983
Assignee
1
WEST HARTFORD,, CONNECTICUT
Correspondence name and address
M. P. WILLIAMS
UNITED TECHNOLOGIES CORP., PAT. SEC.
HARTFORD, CT 06101

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