FR2383429A1 - Equipement gyroscopique avec un carter exterieur comportant une cavite interieure renfermant un boitier de gyroscope - Google Patents
Equipement gyroscopique avec un carter exterieur comportant une cavite interieure renfermant un boitier de gyroscopeInfo
- Publication number
- FR2383429A1 FR2383429A1 FR7806702A FR7806702A FR2383429A1 FR 2383429 A1 FR2383429 A1 FR 2383429A1 FR 7806702 A FR7806702 A FR 7806702A FR 7806702 A FR7806702 A FR 7806702A FR 2383429 A1 FR2383429 A1 FR 2383429A1
- Authority
- FR
- France
- Prior art keywords
- gyroscopic
- synchro
- internal cavity
- compasses
- external housing
- 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
-
- 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
- G01C19/34—Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes
- G01C19/38—Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes with north-seeking action by other than magnetic means, e.g. gyrocompasses using earth's rotation
-
- 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
- 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
- G01C19/28—Pick-offs, i.e. devices for taking-off an indication of the displacement of the rotor axis
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/12—Gyroscopes
- Y10T74/1261—Gyroscopes with pick off
- Y10T74/1275—Electrical
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Life Sciences & Earth Sciences (AREA)
- Environmental & Geological Engineering (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Geology (AREA)
- Gyroscopes (AREA)
- Control Of Combustion (AREA)
Abstract
La présente invention concerne des équipements gyroscopiques tels que des compas à équipage mobile flottant, utilisés pour la navigation marine. Ce compas comprend une gyrosphère pendulaire flottant dans une cavité sphérique contenant un fluide électriquement conducteur. Une électrode 14 faisant passer un courant à travers ce fluide pour faire tourner le rotor du gyroscope, forme une bande de largeur variant suivant une loi sinusoïdale; quatre électrodes associées 11, 38, 100 et 101 également espacées autour du carter de l'instrument fournissent des informations de position en azimut pour exciter un capteur synchro-transmetteur 121 dans lequel ces électrodes créent un vecteur champ qui produit des signaux de sortie représentant des relèvements reels en azimut avec les 3 fils de sortie du synchro-transmetteur. Application aux compas gyroscopiques.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/776,058 US4143466A (en) | 1977-03-09 | 1977-03-09 | Free floating gyroscopic compass azimuth pick-off and rotor drive system |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2383429A1 true FR2383429A1 (fr) | 1978-10-06 |
FR2383429B1 FR2383429B1 (fr) | 1983-03-11 |
Family
ID=25106334
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7806702A Granted FR2383429A1 (fr) | 1977-03-09 | 1978-03-08 | Equipement gyroscopique avec un carter exterieur comportant une cavite interieure renfermant un boitier de gyroscope |
Country Status (7)
Country | Link |
---|---|
US (1) | US4143466A (fr) |
JP (1) | JPS53110868A (fr) |
DE (1) | DE2810270A1 (fr) |
FR (1) | FR2383429A1 (fr) |
GB (1) | GB1564686A (fr) |
IT (1) | IT1155864B (fr) |
NO (1) | NO149155C (fr) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2070244B (en) * | 1980-01-23 | 1984-02-29 | Furuno Electric Co | Gyroscopic instrument |
US6145393A (en) * | 1998-11-27 | 2000-11-14 | Canton; Dino | Floated gimbal optical platform |
DE19921390B4 (de) * | 1999-05-10 | 2005-06-09 | Eads Astrium Gmbh | Positionierungssystem für eine Meßeinrichtung eines Satelliten |
US7458264B2 (en) * | 2004-09-10 | 2008-12-02 | Honeywell International Inc. | Generalized inertial measurement error reduction through multiple axis rotation during flight |
US7698064B2 (en) * | 2004-09-10 | 2010-04-13 | Honeywell International Inc. | Gas supported inertial sensor system and method |
US20060054660A1 (en) * | 2004-09-10 | 2006-03-16 | Honeywell International Inc. | Articulated gas bearing support pads |
US7366613B2 (en) * | 2004-09-10 | 2008-04-29 | Honeywell International Inc. | RF wireless communication for deeply embedded aerospace systems |
TWM266445U (en) * | 2004-11-24 | 2005-06-01 | Tian-Tsai Huang | Improved structure for pressure reading on pressure gauge |
WO2006060609A1 (fr) * | 2004-12-03 | 2006-06-08 | Honeywell International Inc. | Commande par jets de gaz d'une unite inertielle de mesure |
US7647176B2 (en) * | 2007-01-11 | 2010-01-12 | Honeywell International Inc. | Method and system for wireless power transfers through multiple ports |
US7762133B2 (en) * | 2007-07-17 | 2010-07-27 | Honeywell International Inc. | Inertial measurement unit with gas plenums |
US7425097B1 (en) | 2007-07-17 | 2008-09-16 | Honeywell International Inc. | Inertial measurement unit with wireless power transfer gap control |
US9303971B1 (en) * | 2010-12-15 | 2016-04-05 | The Boeing Company | High aspect ratio positioning system |
RU2594628C1 (ru) * | 2015-04-28 | 2016-08-20 | Акционерное общество "Концерн "Центральный научно-исследовательский институт "Электроприбор" | Двухстепенной поплавковый гироскоп |
US10836512B2 (en) | 2016-05-06 | 2020-11-17 | Honeywell International Inc. | Energy efficient spherical momentum control devices |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3373617A (en) * | 1965-03-25 | 1968-03-19 | Anschuetz & Co Gmbh | Gyroscopic instrument |
US3811328A (en) * | 1973-01-03 | 1974-05-21 | Us Army | Pulse duration modulation pickoff |
US3915019A (en) * | 1974-02-21 | 1975-10-28 | Singer Co | Optical gyro pick-off |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE394667C (de) * | 1922-02-18 | 1924-05-08 | Anschuetz & Co Gmbh | Kreiselapparat fuer Messzwecke |
US3226984A (en) * | 1962-04-02 | 1966-01-04 | Paul E Humphrey | Free gyroscope element |
US3670585A (en) * | 1970-04-17 | 1972-06-20 | Northrop Corp | Attitude readout for floated inertial platform |
-
1977
- 1977-03-09 US US05/776,058 patent/US4143466A/en not_active Expired - Lifetime
-
1978
- 1978-02-13 GB GB5635/78A patent/GB1564686A/en not_active Expired
- 1978-03-06 IT IT48310/78A patent/IT1155864B/it active
- 1978-03-08 FR FR7806702A patent/FR2383429A1/fr active Granted
- 1978-03-08 JP JP2645278A patent/JPS53110868A/ja active Pending
- 1978-03-08 NO NO780820A patent/NO149155C/no unknown
- 1978-03-09 DE DE19782810270 patent/DE2810270A1/de active Granted
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3373617A (en) * | 1965-03-25 | 1968-03-19 | Anschuetz & Co Gmbh | Gyroscopic instrument |
US3811328A (en) * | 1973-01-03 | 1974-05-21 | Us Army | Pulse duration modulation pickoff |
US3915019A (en) * | 1974-02-21 | 1975-10-28 | Singer Co | Optical gyro pick-off |
Also Published As
Publication number | Publication date |
---|---|
DE2810270A1 (de) | 1978-09-14 |
NO149155B (no) | 1983-11-14 |
IT7848310A0 (it) | 1978-03-06 |
FR2383429B1 (fr) | 1983-03-11 |
DE2810270C2 (fr) | 1987-05-21 |
US4143466A (en) | 1979-03-13 |
JPS53110868A (en) | 1978-09-27 |
NO780820L (no) | 1978-09-12 |
GB1564686A (en) | 1980-04-10 |
IT1155864B (it) | 1987-01-28 |
NO149155C (no) | 1984-02-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name | ||
ST | Notification of lapse |