GB471093A - Improvements in and relating to navigational measuring instruments for vehicles, especially for aircraft - Google Patents
Improvements in and relating to navigational measuring instruments for vehicles, especially for aircraftInfo
- Publication number
- GB471093A GB471093A GB1750/37A GB175037A GB471093A GB 471093 A GB471093 A GB 471093A GB 1750/37 A GB1750/37 A GB 1750/37A GB 175037 A GB175037 A GB 175037A GB 471093 A GB471093 A GB 471093A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pointer
- clinometer
- aircraft
- behind
- jan
- 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
- G01C19/32—Indicating or recording means specially adapted for rotary gyroscopes
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Gyroscopes (AREA)
Abstract
471,093. Navigational instruments for aircraft. SIEMENS APPARATE UND MASCHINEN GES. Jan. 20, 1937, No. 1750. Convention date, Jan. 24, 1936. [Classes 97 (ii) and 97 (iii)] A turn indicator, longitudinal clinometer, and lateral clinometer are so combined into one instrument that their indicators are superposed in their zero positions. As shown the pointer 4 of the turn indicator is pivoted at 5 and actuated by the restrained gyroscope 2. The longitudinal clinometer comprises a closed rectangular tube 7 half filled with coloured alcohol. The indicating limb of the tube 7 lies behind the window 8 and immediately in front of the pointer 4. The transverse rolling ball level 10 is secured to a plate 6 immediately behind the pointer 4. In a modification the pointer 4 is provided with a double bend enabling it to pass behind the level 10, 11 is a switch for regulating the speed of the gyroscope.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE471093X | 1936-01-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB471093A true GB471093A (en) | 1937-08-27 |
Family
ID=6541229
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1750/37A Expired GB471093A (en) | 1936-01-24 | 1937-01-20 | Improvements in and relating to navigational measuring instruments for vehicles, especially for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB471093A (en) |
-
1937
- 1937-01-20 GB GB1750/37A patent/GB471093A/en not_active Expired
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