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The ornamental design for a vibration reduction system, as shown and described. |
FIG. 1 is a perspective view of my vibration reduction system;
FIG. 2 is a side view, the opposite side view being a mirror image thereof;
FIG. 3 is a top view thereof;
FIG. 4 is a bottom view thereof; and,
FIG. 5 is a front view, the back view being a mirror image thereof.
Patent | Priority | Assignee | Title |
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Patent | Priority | Assignee | Title |
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Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
Mar 10 1993 | HALWES, DENNIS | AERONAUTICAL ACCESSORIES, INC | ASSIGNMENT OF ASSIGNORS INTEREST | 006517 | /0648 | |
Mar 10 1993 | GLOBAL HELICOPTER TECHNOLOGY, INC | AERONAUTICAL ACCESSORIES, INC | ASSIGNMENT OF ASSIGNORS INTEREST | 006517 | /0651 | |
Apr 15 1993 | Aeronautical Accessories, Inc. | (assignment on the face of the patent) | / | |||
Apr 01 2001 | EDWARDS & ASSOCIATES, INC | TEXTRON IPMP L P | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 015177 | /0226 | |
Apr 01 2001 | AERONAUTICAL ACCESSORIES, INC | TEXTRON IPMP L P | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 015177 | /0226 | |
Apr 01 2001 | BELL AIRCRAFT SERVICES MICHIGAN INC | TEXTRON IPMP L P | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 015177 | /0226 |
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