GB1073051A - Improvements in or relating to pressure heads for aircraft - Google Patents
Improvements in or relating to pressure heads for aircraftInfo
- Publication number
- GB1073051A GB1073051A GB197765A GB197765A GB1073051A GB 1073051 A GB1073051 A GB 1073051A GB 197765 A GB197765 A GB 197765A GB 197765 A GB197765 A GB 197765A GB 1073051 A GB1073051 A GB 1073051A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- relating
- jan
- pressure heads
- pressure head
- 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
- G01P5/165—Arrangements or constructions of Pitot tubes
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Resistance Heating (AREA)
Abstract
1,073,051. Electrically heated pressure head for aircraft. AVIMO Ltd. Jan. 12 1966 [Jan. 15, 1985], No. 1977/65. Heading H5H. A pressure head comprises an .electrical heating element embedded in silicone rubber (4), Fig. 2 (not shown) between an outer housing (2) and an inner metal core (1). The element comprises two non-uniform helical windings (3a), (3b) between three layers of rubber (5), (6), (7), starting and finishing. at the same end of the head. The housing and core are of Cu and the wire may have a high temperature/ resistance coefficient to avoid overheating.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB197765A GB1073051A (en) | 1965-01-15 | 1965-01-15 | Improvements in or relating to pressure heads for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB197765A GB1073051A (en) | 1965-01-15 | 1965-01-15 | Improvements in or relating to pressure heads for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1073051A true GB1073051A (en) | 1967-06-21 |
Family
ID=9731404
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB197765A Expired GB1073051A (en) | 1965-01-15 | 1965-01-15 | Improvements in or relating to pressure heads for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1073051A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3535930A (en) * | 1966-07-26 | 1970-10-27 | Rosemount Eng Co Ltd | Aerodynamic components mounted externally on an aircraft |
-
1965
- 1965-01-15 GB GB197765A patent/GB1073051A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3535930A (en) * | 1966-07-26 | 1970-10-27 | Rosemount Eng Co Ltd | Aerodynamic components mounted externally on an aircraft |
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