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Dale W. R. Lawson
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Bonita, CA, US
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last 30 patents
Information
Patent Grant
Aircraft turbine engine thrust reverser
Patent number
5,230,213
Issue date
Jul 27, 1993
Rohr, Inc.
Dale W. R. Lawson
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Honeycomb noise attenuation structure
Patent number
4,539,244
Issue date
Sep 3, 1985
Rohr Industries, Inc.
Stanley L. Beggs
G10 - MUSICAL INSTRUMENTS ACOUSTICS
Information
Patent Grant
Thrust reverser geared linkage
Patent number
4,356,973
Issue date
Nov 2, 1982
Rohr Industries, Inc.
Dale W. R. Lawson
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Thrust reverser - cascade type
Patent number
4,340,178
Issue date
Jul 20, 1982
Rohr Industries, Inc.
Dale W. R. Lawson
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information
Patent Grant
Method of manufacture of honeycomb noise attenuation structure and...
Patent number
4,254,171
Issue date
Mar 3, 1981
Rohr Industries, Inc.
Stanley L. Beggs
G10 - MUSICAL INSTRUMENTS ACOUSTICS
Information
Patent Grant
Linkage system for a turbo fan engine thrust reverser
Patent number
4,216,926
Issue date
Aug 12, 1980
Rohr Industries, Inc.
Dale W. R. Lawson
F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS