GB425957A - Improvements in or relating to gyroscopic apparatus for use on aircraft - Google Patents
Improvements in or relating to gyroscopic apparatus for use on aircraftInfo
- Publication number
- GB425957A GB425957A GB31560/34A GB3156034A GB425957A GB 425957 A GB425957 A GB 425957A GB 31560/34 A GB31560/34 A GB 31560/34A GB 3156034 A GB3156034 A GB 3156034A GB 425957 A GB425957 A GB 425957A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gyroscope
- nov
- nozzles
- threaded
- gyroscopic apparatus
- 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
- G01C19/02—Rotary gyroscopes
- G01C19/04—Details
- G01C19/06—Rotors
- G01C19/12—Rotors fluid driven
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Gyroscopes (AREA)
Abstract
425,957. Gyroscopic apparatus. SPERRY GYROSCOPE CO., Inc., Manhattan Bridge Plaza, Brooklyn, New York, U.S.A.- (Assignees of Carter, L. F., and Dundon, D. C.) Nov. 2, 1934, No. 31560. Convention date, Nov. 3, 1933. [Class 97 (iii)] The driving nozzle or pair of nozzles acting side by side of an air driven directional gyroscope are formed in a member having a fine lateral adjustment relative to the periphery of the rotor. In one form a gyroscope as described in Specification 394,412 is driven by air drawn through a passage in the lower bearing of the vertical gimbal ring 14. The latter carries a bracket 21 branching into two arms 22, 22<1> across which extends a threaded shaft 23. A member 25 carrying two nozzles 2, 2<1> is threaded on the shaft 23 and may be adjusted by means of the slotted end 24, lost motion being taken up by a spring 27. The hollow vertical bearing is connected to the member 25 by a tube 18 having a substantially horizontal swivel connection at the bottom so that it is not distorted by adjustment.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US425957XA | 1933-11-03 | 1933-11-03 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB425957A true GB425957A (en) | 1935-03-25 |
Family
ID=21922765
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB31560/34A Expired GB425957A (en) | 1933-11-03 | 1934-11-02 | Improvements in or relating to gyroscopic apparatus for use on aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB425957A (en) |
-
1934
- 1934-11-02 GB GB31560/34A patent/GB425957A/en not_active Expired
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