FR2252629A1 - Vibration absorbing support for aircraft gyroscopes - has orthogonally sliding guides and shock absorbing - Google Patents

Vibration absorbing support for aircraft gyroscopes - has orthogonally sliding guides and shock absorbing

Info

Publication number
FR2252629A1
FR2252629A1 FR7341977A FR7341977A FR2252629A1 FR 2252629 A1 FR2252629 A1 FR 2252629A1 FR 7341977 A FR7341977 A FR 7341977A FR 7341977 A FR7341977 A FR 7341977A FR 2252629 A1 FR2252629 A1 FR 2252629A1
Authority
FR
France
Prior art keywords
gyroscopes
orthogonally
aircraft
sliding guides
instrument
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.)
Granted
Application number
FR7341977A
Other languages
French (fr)
Other versions
FR2252629B1 (en
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.)
Vibrachoc SAS
Original Assignee
Vibrachoc SAS
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 Vibrachoc SAS filed Critical Vibrachoc SAS
Priority to FR7341977A priority Critical patent/FR2252629A1/en
Publication of FR2252629A1 publication Critical patent/FR2252629A1/en
Application granted granted Critical
Publication of FR2252629B1 publication Critical patent/FR2252629B1/fr
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/02—Rotary gyroscopes
    • G01C19/04—Details
    • G01C19/16—Suspensions; Bearings
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/18—Stabilised platforms, e.g. by gyroscope
    • G—PHYSICS
    • G12—INSTRUMENT DETAILS
    • G12B—CONSTRUCTIONAL DETAILS OF INSTRUMENTS, OR COMPARABLE DETAILS OF OTHER APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G12B3/00—Details of movements not otherwise provided for
    • G12B3/08—Damping of movements, e.g. to promote rapid non-oscillatory movement to a final reading
    • G—PHYSICS
    • G12—INSTRUMENT DETAILS
    • G12B—CONSTRUCTIONAL DETAILS OF INSTRUMENTS, OR COMPARABLE DETAILS OF OTHER APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G12B9/00—Housing or supporting of instruments or other apparatus
    • G12B9/08—Supports; Devices for carrying

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Vibration Prevention Devices (AREA)

Abstract

The three guides are orientated along three respective axes, and can slide relative to one another along these axes such that the position of the instrument platform (2) can be varied relative to its support mounting without altering the angular direction of the instrument. The vibration damping means are interposed between the mounting and the instrument and have the same damping characteristics in each of the three axial directions. Four multi-directional vibration dampers (4) are used and each comprises an elastomer envelope containing a viscous silicone fluid.
FR7341977A 1973-11-26 1973-11-26 Vibration absorbing support for aircraft gyroscopes - has orthogonally sliding guides and shock absorbing Granted FR2252629A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7341977A FR2252629A1 (en) 1973-11-26 1973-11-26 Vibration absorbing support for aircraft gyroscopes - has orthogonally sliding guides and shock absorbing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7341977A FR2252629A1 (en) 1973-11-26 1973-11-26 Vibration absorbing support for aircraft gyroscopes - has orthogonally sliding guides and shock absorbing

Publications (2)

Publication Number Publication Date
FR2252629A1 true FR2252629A1 (en) 1975-06-20
FR2252629B1 FR2252629B1 (en) 1978-03-17

Family

ID=9128243

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7341977A Granted FR2252629A1 (en) 1973-11-26 1973-11-26 Vibration absorbing support for aircraft gyroscopes - has orthogonally sliding guides and shock absorbing

Country Status (1)

Country Link
FR (1) FR2252629A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0398483A2 (en) * 1989-04-28 1990-11-22 Leonard Studio Equipment Inc. Shock and vibration isolator
EP0424937A2 (en) * 1989-10-26 1991-05-02 Hughes Aircraft Company Apparatus for compensating for disturbing torques acting on a stabilized spacecraft or the like, with momentum wheel means
CN111005982A (en) * 2019-11-09 2020-04-14 武昌理工学院 Spring vibration reduction mechanism with quick locking function

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0398483A2 (en) * 1989-04-28 1990-11-22 Leonard Studio Equipment Inc. Shock and vibration isolator
EP0398483A3 (en) * 1989-04-28 1990-11-28 Leonard Studio Equipment Inc. Shock and vibration isolator
BE1002407A3 (en) * 1989-04-28 1991-01-29 Leonard Studio Equip SHOCK AND VIBRATION SHOCK ABSORBER.
EP0424937A2 (en) * 1989-10-26 1991-05-02 Hughes Aircraft Company Apparatus for compensating for disturbing torques acting on a stabilized spacecraft or the like, with momentum wheel means
EP0424937A3 (en) * 1989-10-26 1991-07-03 Hughes Aircraft Company Tilting momentum wheel for spacecraft
US5112012A (en) * 1989-10-26 1992-05-12 Yuan Mark S Tilting momentum wheel for spacecraft
CN111005982A (en) * 2019-11-09 2020-04-14 武昌理工学院 Spring vibration reduction mechanism with quick locking function

Also Published As

Publication number Publication date
FR2252629B1 (en) 1978-03-17

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Legal Events

Date Code Title Description
ST Notification of lapse