GB601132A - Improvements in and relating to automatic pilots for aircraft - Google Patents
Improvements in and relating to automatic pilots for aircraftInfo
- Publication number
- GB601132A GB601132A GB1787845A GB1787845A GB601132A GB 601132 A GB601132 A GB 601132A GB 1787845 A GB1787845 A GB 1787845A GB 1787845 A GB1787845 A GB 1787845A GB 601132 A GB601132 A GB 601132A
- Authority
- GB
- United Kingdom
- Prior art keywords
- valve
- piston
- knob
- aircraft
- relating
- 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
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
601,132. Retarding valve actuation. DUNN, R. W., BROWN, G. W., ROWSE, L. E., SPENCER, W. A., SUDWORTH, J., HOPKIN, H. R., and MEYER, J. F. A. July 12, 1945, No. 17878. [Class 135] [Also in Groups XX and XXXV] Opening of a valve 25 controlling the precession of a gyroscope (see Group XX) takes place when the turn control knob 11 of an automatic pilot is moved but is delayed by the liquid dash-pot 16. The valve actuating rod 24 is connected to the piston 19 and the latter is urged downwards by the spring 18 when the plunger 14 is depressed by the cam surface 13 fixed to the knob 11. The piston 19 is provided with one-way flaps 22 so that the valve 25 is closed, immediately the knob 11 returns to the zero position, by the engagement of the flange 20 with the piston. Specifications 600,901 and 601,131 are referred to.
Publications (1)
Publication Number | Publication Date |
---|---|
GB601132A true GB601132A (en) | 1948-04-28 |
Family
ID=1733482
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1787845A Expired GB601132A (en) | 1945-07-12 | Improvements in and relating to automatic pilots for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB601132A (en) |
-
1945
- 1945-07-12 GB GB1787845A patent/GB601132A/en not_active Expired
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