GB124827A - A Combined Pressure and Static Head for Air Speed Indicators. - Google Patents
A Combined Pressure and Static Head for Air Speed Indicators.Info
- Publication number
- GB124827A GB124827A GB611616A GB611616A GB124827A GB 124827 A GB124827 A GB 124827A GB 611616 A GB611616 A GB 611616A GB 611616 A GB611616 A GB 611616A GB 124827 A GB124827 A GB 124827A
- Authority
- GB
- United Kingdom
- Prior art keywords
- tube
- carried
- cap
- head
- wind
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Measuring Fluid Pressure (AREA)
- Earth Drilling (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Abstract
124,827. Aeronautical Instrument Co., and Brewer, G. April 28, 1916. Pitot-tube apparatus.-A swivelling pressure-head for air-speed indicators of streamline form, constructed to convey both wind and static pressures to a differential pressure gauge on which the speed is indicated, is mounted upon a pivot carried by a tubular member and is provided with means for keeping the head of the device to the wind. The tubular member bearing the pivot is in communication with the wind-pressure chamber and is carried by a tubular mast, which may enclose a second tube communicating the static pressure of the secondary atmosphere, or may itself constitute the communicating means, the combined pressures being conveyed thereby to an indicating-device, such as that described in Specification 13796/13. A tube 4, Fig. 1, mounted in the nose of the device communicates with a casing constituted by a tube 5, an upper cap 6, and a lower cap 12, through which passes a tube 9, carried by the perforated upper end of which is a pivot 8, a bearing 7 therefor being carried by the cap 6. The casing 5 is rendered air-tight by a felt or like washer 11 secured so as to be capable of longitudinal movement between the cap 12 and a screwed end 13. Surrounding the lower end of the tube 9 and carried by the tubular mast is a second tube 10 closed at its upper end and perforated at 15 to communicate with tlie interier of the casing, which itself is connected with the exterior air by holes 16. Balance weights 18, provided with cavities 19 to receive shot, are mounted in the head. The tail 20 is made to diverge towards the rear as shown in Fig. 2, the preferred angle being 10 degrees.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB611616A GB124827A (en) | 1916-04-28 | 1916-04-28 | A Combined Pressure and Static Head for Air Speed Indicators. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB611616A GB124827A (en) | 1916-04-28 | 1916-04-28 | A Combined Pressure and Static Head for Air Speed Indicators. |
Publications (1)
Publication Number | Publication Date |
---|---|
GB124827A true GB124827A (en) | 1919-04-10 |
Family
ID=32342434
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB611616A Expired GB124827A (en) | 1916-04-28 | 1916-04-28 | A Combined Pressure and Static Head for Air Speed Indicators. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB124827A (en) |
Cited By (2)
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 |
US2662402A (en) * | 1948-11-22 | 1953-12-15 | North American Aviation Inc | Flight test head |
-
1916
- 1916-04-28 GB GB611616A patent/GB124827A/en not_active Expired
Cited By (2)
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 |
US2662402A (en) * | 1948-11-22 | 1953-12-15 | North American Aviation Inc | Flight test head |
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