USD346146S - Vibration reduction system - Google Patents

Vibration reduction system Download PDF

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Publication number
USD346146S
USD346146S US29/007,223 US722393F USD346146S US D346146 S USD346146 S US D346146S US 722393 F US722393 F US 722393F US D346146 S USD346146 S US D346146S
Authority
US
United States
Prior art keywords
reduction system
vibration reduction
vibration
view
ornamental design
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US29/007,223
Inventor
Dennis Halwes
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Textron IPMP LP
Original Assignee
Aeronautical Accessories Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Aeronautical Accessories Inc filed Critical Aeronautical Accessories Inc
Priority to US29/007,223 priority Critical patent/USD346146S/en
Assigned to AERONAUTICAL ACCESSORIES, INC. reassignment AERONAUTICAL ACCESSORIES, INC. ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: GLOBAL HELICOPTER TECHNOLOGY, INC.
Assigned to AERONAUTICAL ACCESSORIES, INC. reassignment AERONAUTICAL ACCESSORIES, INC. ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: HALWES, DENNIS
Application granted granted Critical
Publication of USD346146S publication Critical patent/USD346146S/en
Assigned to TEXTRON IPMP L.P. reassignment TEXTRON IPMP L.P. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: AERONAUTICAL ACCESSORIES, INC., BELL AIRCRAFT SERVICES MICHIGAN INC., EDWARDS & ASSOCIATES, INC.
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Description

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.

Claims (1)

  1. The ornamental design for a vibration reduction system, as shown and described.
US29/007,223 1993-04-15 1993-04-15 Vibration reduction system Expired - Lifetime USD346146S (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US29/007,223 USD346146S (en) 1993-04-15 1993-04-15 Vibration reduction system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US29/007,223 USD346146S (en) 1993-04-15 1993-04-15 Vibration reduction system

Publications (1)

Publication Number Publication Date
USD346146S true USD346146S (en) 1994-04-19

Family

ID=70846488

Family Applications (1)

Application Number Title Priority Date Filing Date
US29/007,223 Expired - Lifetime USD346146S (en) 1993-04-15 1993-04-15 Vibration reduction system

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US (1) USD346146S (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD566032S1 (en) * 2007-02-27 2008-04-08 Thales Avionics Sa Pilot multipurpose cursor control unit for vibrations environment

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4420134A (en) 1980-10-27 1983-12-13 Kaman Aerospace Corporation Vibration isolator with crank driven inertia bar
US4664281A (en) 1985-10-15 1987-05-12 Killark Electric Manufacturing Co. Explosion proof enclosure
USD338186S (en) 1991-07-30 1993-08-10 Aeronautical Accessories, Inc. Enclosure for a helicopter vibration reduction system

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4420134A (en) 1980-10-27 1983-12-13 Kaman Aerospace Corporation Vibration isolator with crank driven inertia bar
US4664281A (en) 1985-10-15 1987-05-12 Killark Electric Manufacturing Co. Explosion proof enclosure
USD338186S (en) 1991-07-30 1993-08-10 Aeronautical Accessories, Inc. Enclosure for a helicopter vibration reduction system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD566032S1 (en) * 2007-02-27 2008-04-08 Thales Avionics Sa Pilot multipurpose cursor control unit for vibrations environment

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