USD352299S - Inertial sensor support structure for accelerometers and gyros - Google Patents

Inertial sensor support structure for accelerometers and gyros Download PDF

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Publication number
USD352299S
USD352299S US29/005,969 US596993F USD352299S US D352299 S USD352299 S US D352299S US 596993 F US596993 F US 596993F US D352299 S USD352299 S US D352299S
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US
United States
Prior art keywords
gyros
accelerometers
support structure
inertial sensor
sensor support
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
US29/005,969
Inventor
Lucien E. Joly
Michael A. Knipfer
Michelle J. Miller
George O. Mitzschke
Mark T. Weinberger
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.)
Honeywell Inc
Original Assignee
Honeywell Inc
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Publication date
Application filed by Honeywell Inc filed Critical Honeywell Inc
Priority to US29/005,969 priority Critical patent/USD352299S/en
Application granted granted Critical
Publication of USD352299S publication Critical patent/USD352299S/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Description

FIG. 1 is a perspective view of the inertial sensor support showing mounting surfaces for gyros;
FIG. 2 is a left side perspective of FIG. 1;
FIG. 3 is a rear view of the perspective of FIG. 1;
FIG. 4 is a bottom view of the perspective of FIG. 1 rotated 180° showing mounting surfaces for accelerometers; and,
FIG. 5 is a bottom view of FIG. 1 rotated 90°.

Claims (1)

  1. The ornamental design for an inertial sensor support structure for accelerometers and gyros, as shown and described.
US29/005,969 1993-03-19 1993-03-19 Inertial sensor support structure for accelerometers and gyros Expired - Lifetime USD352299S (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US29/005,969 USD352299S (en) 1993-03-19 1993-03-19 Inertial sensor support structure for accelerometers and gyros

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US29/005,969 USD352299S (en) 1993-03-19 1993-03-19 Inertial sensor support structure for accelerometers and gyros

Publications (1)

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USD352299S true USD352299S (en) 1994-11-08

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Family Applications (1)

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US29/005,969 Expired - Lifetime USD352299S (en) 1993-03-19 1993-03-19 Inertial sensor support structure for accelerometers and gyros

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Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3269179A (en) 1959-05-29 1966-08-30 Honeywell Regulator Co Navigational instruments
US3489004A (en) 1966-07-21 1970-01-13 Honeywell Inc Navigational reference device
USD317132S (en) 1989-05-24 1991-05-28 Honeywell Inc. Ring laser gyroscope housing

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3269179A (en) 1959-05-29 1966-08-30 Honeywell Regulator Co Navigational instruments
US3489004A (en) 1966-07-21 1970-01-13 Honeywell Inc Navigational reference device
USD317132S (en) 1989-05-24 1991-05-28 Honeywell Inc. Ring laser gyroscope housing

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
ADIRS; Fault-Tolerant; no date provided.
Honeywell Air Transport Sys. Div.-Charles R. McClary, Position, Location, Navigation Symposium 1992.

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