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 absorbingInfo
- 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
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)
- Automation & Control Theory (AREA)
- Acoustics & Sound (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (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.
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 (2)
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 |
-
1973
- 1973-11-26 FR FR7341977A patent/FR2252629A1/en active Granted
Cited By (6)
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 |
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 |