GB583530A - Improvement in air relay assemblies for automatic pilots - Google Patents
Improvement in air relay assemblies for automatic pilotsInfo
- Publication number
- GB583530A GB583530A GB9118/44A GB911844A GB583530A GB 583530 A GB583530 A GB 583530A GB 9118/44 A GB9118/44 A GB 9118/44A GB 911844 A GB911844 A GB 911844A GB 583530 A GB583530 A GB 583530A
- Authority
- GB
- United Kingdom
- Prior art keywords
- improvement
- air relay
- relay assemblies
- automatic pilots
- operating
- 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
- 230000000712 assembly Effects 0.000 title 1
- 238000000429 assembly Methods 0.000 title 1
- 238000005266 casting Methods 0.000 abstract 1
- 230000000295 complement effect Effects 0.000 abstract 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Supply Devices, Intensifiers, Converters, And Telemotors (AREA)
Abstract
583,530. Fluid-pressure servomotors. JACK & HEINTZ, Inc. May 12, 1944, No. 9118. Convention date, Oct. 14, 1942. [Class 135] An air relay device for operating the oil valve of an automatic pilot for aircraft comprises two complementary castings 1, 2 securing an operating diaphragm 4 between them and each having a single channel 17 or 18 communicating with the respective diaphragm chamber 5 or 6 and with inlet and outlet passages 12, 13 and 14, 15 respectively.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US583530XA | 1942-10-14 | 1942-10-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB583530A true GB583530A (en) | 1946-12-20 |
Family
ID=22016298
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9118/44A Expired GB583530A (en) | 1942-10-14 | 1944-05-12 | Improvement in air relay assemblies for automatic pilots |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB583530A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3304880A (en) * | 1964-11-06 | 1967-02-21 | Gen Motors Corp | Pump and diaphragm plunger sub-assembly |
-
1944
- 1944-05-12 GB GB9118/44A patent/GB583530A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3304880A (en) * | 1964-11-06 | 1967-02-21 | Gen Motors Corp | Pump and diaphragm plunger sub-assembly |
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