GB314786A - Improvements in electro-magnetic apparatus for the observation and correction of travel of aerial and marine craft - Google Patents
Improvements in electro-magnetic apparatus for the observation and correction of travel of aerial and marine craftInfo
- Publication number
- GB314786A GB314786A GB27154/28A GB2715428A GB314786A GB 314786 A GB314786 A GB 314786A GB 27154/28 A GB27154/28 A GB 27154/28A GB 2715428 A GB2715428 A GB 2715428A GB 314786 A GB314786 A GB 314786A
- Authority
- GB
- United Kingdom
- Prior art keywords
- winding
- contact
- inductor
- mercury
- revolution
- 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
- G01C17/00—Compasses; Devices for ascertaining true or magnetic north for navigation or surveying purposes
- G01C17/36—Repeaters for remote indication of readings of a master compass
Abstract
314,786. Vion, E. July 2, 1928, [Convention date]. Earth inductor machines; driving-arrangements; mercury collecting devices.-Apparatus for the observation and correction of the direction of travel in aerial and marine navigation comprises a member influenced by deviation from the correct course and operating an indicator proportionally to the time-integral of the deviation. As shown, an earth inductor is provided with a winding A, Fig. 1, and is rotated about an axis which is maintained vertical by gyroscopic action and by the action of gravity owing to the suspension of the inductor from a Cardan point B, C. The inductor is driven by a small air turbine A<1> which is actuated, when used on aircraft, by a Venturi device A<2> which creates a rarefaction in the casing D so that air from outside the casing impinges on the turbine A' through a nozzle d. The ends of the winding A are connected through mercury cups E, E' to the receiving device H. The mercury cup E rotates with the inductor armature and is shaped to prevent escape of mercury, which forms a peripheral ring e when rotating. Contact with this is made by a rod a<3>. The ends of the winding A are connected to a lever F and contact stud G, shown in Fig. 2, so that when the lever and contact engage, the winding A and the receiving device are short-circuited. The contact-breaker and stud are mounted on a plate J fixed to the spindle K and rotating with the winding A. One arm of the lever F engages a semicircular fixed cam L so that current is supplied to the receiving device H for half a revolution, the winding being then short-circuited for half a revolution. The cam L can be adjusted by the pilot in accordance with the desired course bv means of a handoperated disc M<2> through gearing M, M<1>. Two contact-makers F, G may be arranged so as to reverse the connections of the armature winding A at each half-revolution. The inductor may be provided with multiple windings and a corresponding number of contact-makers F, G for reversing the connections of these windings at the appropriate times.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR314786X | 1928-07-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB314786A true GB314786A (en) | 1929-12-23 |
Family
ID=8889550
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB27154/28A Expired GB314786A (en) | 1928-07-02 | 1928-09-21 | Improvements in electro-magnetic apparatus for the observation and correction of travel of aerial and marine craft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB314786A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2434324A (en) * | 1944-10-06 | 1948-01-13 | Control Instr Co Inc | Earth inductor compass |
-
1928
- 1928-09-21 GB GB27154/28A patent/GB314786A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2434324A (en) * | 1944-10-06 | 1948-01-13 | Control Instr Co Inc | Earth inductor compass |
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