GB131333A - - Google Patents
Info
- Publication number
- GB131333A GB131333A GB131333DA GB131333A GB 131333 A GB131333 A GB 131333A GB 131333D A GB131333D A GB 131333DA GB 131333 A GB131333 A GB 131333A
- Authority
- GB
- United Kingdom
- Prior art keywords
- tube
- flexible
- aircraft
- secured
- pressure
- 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.)
- Active
Links
Landscapes
- Measuring Fluid Pressure (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
Abstract
131,333. Aeronautical Instrument Co., and Brewer, G. May 2, 1918. Anemometers and air-current indicators.-Static and wind pressure tubes on aircraft are flexibly supported at their centre of gravity and provided with vanes so that they can adjust themselves within limit to the direction of the wind current. A flexible tube communicating with the pressure tube at its pivotal point conveys the pressure to a fixed tube on the aircraft. Fig. 1 shows a static pressure tube 4 flexibly suspended at its centre of gravity and provided with a conical rear end 8 or other vane. The tube 4 is divided at its point of suspension by an inclined partition 5, and the forward end communicates through a nozzle 6 and flexible tube 7 with a fixed tube 1 on the aircraft. A plate 14 secured to the partition 5 is secured to flexible connexions 9, 11 anchored respectively to a fixed frame 3 and to the tube 1. A spring 12 may be interposed in the connexion 11 which is enclosed by the tube 7. Fig. 4 shows a modification in which the tube is hinged about a transverse pin at the upper end of a spindle 16 capable of turning in a rigid arm 18 which is cruciform at its lower end and secured in the fixed tube 1. A flexible tube 7 surrounds the arm 18 and puts the tube 4 into communication with the tube 1.
Publications (1)
Publication Number | Publication Date |
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GB131333A true GB131333A (en) |
Family
ID=1724912
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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GB131333D Active GB131333A (en) |
Country Status (1)
Country | Link |
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GB (1) | GB131333A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2554634A (en) * | 1947-12-16 | 1951-05-29 | Glenn L Martin Co | Pitot-static tube with airstream aligning means |
US2623383A (en) * | 1945-04-07 | 1952-12-30 | Bendix Aviat Corp | Apparatus for calibrating the airspeed indicator of aircraft |
US3055215A (en) * | 1957-06-03 | 1962-09-25 | James O Ivie | Wind direction and turbulence indicator |
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0
- GB GB131333D patent/GB131333A/en active Active
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2623383A (en) * | 1945-04-07 | 1952-12-30 | Bendix Aviat Corp | Apparatus for calibrating the airspeed indicator of aircraft |
US2554634A (en) * | 1947-12-16 | 1951-05-29 | Glenn L Martin Co | Pitot-static tube with airstream aligning means |
US3055215A (en) * | 1957-06-03 | 1962-09-25 | James O Ivie | Wind direction and turbulence indicator |
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