USD338186S - Enclosure for a helicopter vibration reduction system - Google Patents

Enclosure for a helicopter vibration reduction system Download PDF

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Publication number
USD338186S
USD338186S US07/737,503 US73750391F USD338186S US D338186 S USD338186 S US D338186S US 73750391 F US73750391 F US 73750391F US D338186 S USD338186 S US D338186S
Authority
US
United States
Prior art keywords
enclosure
reduction system
vibration reduction
helicopter vibration
helicopter
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
US07/737,503
Inventor
Dennis R. 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 US07/737,503 priority Critical patent/USD338186S/en
Assigned to AERONAUTICAL ACCESSORIES, INC. reassignment AERONAUTICAL ACCESSORIES, INC. ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: HAWLES, DENNIS R.
Application granted granted Critical
Publication of USD338186S publication Critical patent/USD338186S/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 new enclosure for a helicopter vibration reduction system;
FIG. 2 is a top view thereof;
FIG. 3 is a right side view thereof;
FIG. 4 is a left side view thereof;
FIG. 5 is a bottom view thereof;
FIG. 6 is a front view thereof; and,
FIG. 7 is a rear view thereof.

Claims (1)

  1. The ornamental design for an enclosure for a helicopter vibration reduction system, as shown.
US07/737,503 1991-07-30 1991-07-30 Enclosure for a helicopter vibration reduction system Expired - Lifetime USD338186S (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US07/737,503 USD338186S (en) 1991-07-30 1991-07-30 Enclosure for a helicopter vibration reduction system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/737,503 USD338186S (en) 1991-07-30 1991-07-30 Enclosure for a helicopter vibration reduction system

Publications (1)

Publication Number Publication Date
USD338186S true USD338186S (en) 1993-08-10

Family

ID=70678476

Family Applications (1)

Application Number Title Priority Date Filing Date
US07/737,503 Expired - Lifetime USD338186S (en) 1991-07-30 1991-07-30 Enclosure for a helicopter vibration reduction system

Country Status (1)

Country Link
US (1) USD338186S (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD838864S1 (en) * 2016-09-07 2019-01-22 EMULATE, Inc. Opaque microfluidic chip without pressure features for use with a fluid perfusion module

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD838864S1 (en) * 2016-09-07 2019-01-22 EMULATE, Inc. Opaque microfluidic chip without pressure features for use with a fluid perfusion module

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