GB824670A - Speed indicator for airplanes - Google Patents
Speed indicator for airplanesInfo
- Publication number
- GB824670A GB824670A GB2158856A GB2158856A GB824670A GB 824670 A GB824670 A GB 824670A GB 2158856 A GB2158856 A GB 2158856A GB 2158856 A GB2158856 A GB 2158856A GB 824670 A GB824670 A GB 824670A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- shaft
- speed
- pointer
- link
- 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
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
- G01P5/14—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
- G01P5/16—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid using Pitot tubes, e.g. Machmeter
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Measuring Fluid Pressure (AREA)
Abstract
824,670. Air-speed indicators. VYZKUMNY A ZKUSEBNI LETECKY USTAV. July 12, 1956, No. 21588/56. Class 69 (1). An aircraft air-speed indicator includes transmission mechanism for converting indicated air speed derived from a pitot tube to true air speed, by effectively multiplying it by the air density as obtained from measurements of air pressure and temperature. As shown, the differential pressure from the pitot tube acts on a pressure-sensitive bellows 1 coupled via a shaft 3 and toothed segment 17 and pinion 18 to a pointer 15 showing " indicated air speed." Shaft 3 is also coupled to a shaft 5, toothed sector 19, pinion 20 and pointer 16, via a link 4 pivoted to an arm 6 of fixed length on the shaft 3 and rotatable about this pivot against a spring 9 to vary the effective distance of pivot 9a (mounted on spring 9) from the axis of shaft 5, and hence the transmission ratio between shafts 3 and 5. The rotation of the link 4 is effected through members 8 and 7 by the action of an evacuated vessel 13 responsive to the air pressure and a capsule 14 connected to an air thermometer 14a constructed and coupled together so that the movement of link 11 is proportional to the change in logarithm of the air density; the result is stated to be that the effective arm at 9a is substantially proportional to air density within the desired density range so that pointer 16 indicates true air speed.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2158856A GB824670A (en) | 1956-07-12 | 1956-07-12 | Speed indicator for airplanes |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2158856A GB824670A (en) | 1956-07-12 | 1956-07-12 | Speed indicator for airplanes |
Publications (1)
Publication Number | Publication Date |
---|---|
GB824670A true GB824670A (en) | 1959-12-02 |
Family
ID=10165433
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2158856A Expired GB824670A (en) | 1956-07-12 | 1956-07-12 | Speed indicator for airplanes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB824670A (en) |
-
1956
- 1956-07-12 GB GB2158856A patent/GB824670A/en not_active Expired
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