GB513911A - Improvements relating to directional gyroscopes - Google Patents
Improvements relating to directional gyroscopesInfo
- Publication number
- GB513911A GB513911A GB9026/38A GB902638A GB513911A GB 513911 A GB513911 A GB 513911A GB 9026/38 A GB9026/38 A GB 9026/38A GB 902638 A GB902638 A GB 902638A GB 513911 A GB513911 A GB 513911A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gyroscope
- follow
- relay
- servomotor
- rod
- 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
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
Abstract
513,911. Fluid-pressure servomotor-control systems. ALKAN, R. March 24, 1938, No. 9026. Convention date, June 9, 1937. [Class 135] A directional gyroscope comprises a differential fluid-pressure relay coaxially arranged within a follow-up member and consisting of a fluid circuit divided into two parts by a deformable membrane and actuated in a manner known per se by means adapted to form a sort of pneumatic or hydraulic Wheatstone bridge, the deformable membrane being integral with the follow-up member controlled by the gyroscope and which is located coaxially with the axis of rotation of the gyroscope support. A gyroscope 1 has a differential fluid-pressure relay 25 arranged within a member 9 which follows up the movements of the gyroscope relative to its support and is actuated by a servomotor 10 the control or distributing valve 15 of which is actuated by the relay 25. The rotor 1 of the gyroscope is free to rotate about perpendicular axes 2, 3, 4 in a frame 5. The latter has a depending skirt or drum 6 with cut-away edges 7, adapted to obturate. differentially slits 8, 8<1> in the follow-up member 9 also formed as a drum. The slits 8, 8<1> communicate through cavities 27 and passages 26 with chambers 23, 24 on opposite sides of a flexible membrane 25 which constitutes the effective member of the relay. The membrane 25 is connected to a rod 28 passing through a gland in a trunnion on the follow-up member. A thrust bearing 29 on the rod 28 is engaged by a lever 31 connected to the piston valve 15 by a rod 16. The servomotor 10 operates a shaft 11 through reducing gear, the shaft 11 driving the follow-up member 9 through a pinion 12 and a crown wheel 13. The chambers 23, 24 also communicate through fixed orifices 21, 22 with a conduit 20 by which compressed air is supplied to the driving nozzle 34 of the rotor. The conduit 20 communicates by means of a cavity 19 and a rotatable union with a fixed supply pipe 17. To avoid " hunting," the transmission between the relay 25 and the valve 15 is provided with a spring 33. As shown this operates on the rod 16, so that a certain free movement of the drum 6 or dead space occurs before the member 9 follows this movement. By extending the shaft 11 of the servomotor 10, a drive may be obtained for various instruments which will follow the orientation of the gyroscope.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR513911X | 1937-06-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB513911A true GB513911A (en) | 1939-10-25 |
Family
ID=8913853
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9026/38A Expired GB513911A (en) | 1937-06-09 | 1938-03-24 | Improvements relating to directional gyroscopes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB513911A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106123882A (en) * | 2016-06-22 | 2016-11-16 | 陕西宝成航空仪表有限责任公司 | Monoblock type gyro thin walled framed structure for torpedo |
-
1938
- 1938-03-24 GB GB9026/38A patent/GB513911A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106123882A (en) * | 2016-06-22 | 2016-11-16 | 陕西宝成航空仪表有限责任公司 | Monoblock type gyro thin walled framed structure for torpedo |
CN106123882B (en) * | 2016-06-22 | 2019-01-22 | 陕西宝成航空仪表有限责任公司 | Monoblock type gyro thin walled framed structure for torpedo |
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