GB1215923A - Temperature sensing apparatus - Google Patents
Temperature sensing apparatusInfo
- Publication number
- GB1215923A GB1215923A GB5264266A GB5264266A GB1215923A GB 1215923 A GB1215923 A GB 1215923A GB 5264266 A GB5264266 A GB 5264266A GB 5264266 A GB5264266 A GB 5264266A GB 1215923 A GB1215923 A GB 1215923A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas
- temperature
- nozzle
- flow
- gases
- 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
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K11/00—Measuring temperature based upon physical or chemical changes not covered by groups G01K3/00, G01K5/00, G01K7/00 or G01K9/00
- G01K11/22—Measuring temperature based upon physical or chemical changes not covered by groups G01K3/00, G01K5/00, G01K7/00 or G01K9/00 using measurement of acoustic effects
Landscapes
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- General Physics & Mathematics (AREA)
- Measuring Volume Flow (AREA)
Abstract
1,215,923. Measuring temperature electrically JOSEPH LUCAS (INDUSTRIES) Ltd. Feb. 13, 1968 [Nov. 24, 1966], No. 52642/66. Heading G1N. The temperature of a fluid, e.g. that of the gases flowing through the jet pipe of a gas turbine engine, is measured using apparatus in which the flow of gas from a nozzle 17 interferes with the flow of gas between nozzles 10, 14, the nozzle 10 being connected to an inlet 12 from the jet pipe and the nozzle 14 being connected via a device 18 with the nozzle 17. The device 18 is such that it produces a time dependent on the temperature of the gases in the gas flow between the nozzles 14, 17 so that the flow of gas between the nozzles 10, 14 is interrupted at a frequency dependent on the temperature of the gases. The pulses produced in the flow into nozzle 14 are transmitted via passage 15, diaphragm 21 to an electrical pressure sensitive transducer 23 from which a signal is derived which is indicative of changes in frequency of the pulses and therefore of the temperature of the gases. This signal may be used to control the fuel supply to the engine. The nozzles 10, 14, 17 are located in a chamber 13 connected to the inlet pipe 12, passages 11, 27 being connected across a restriction 28 in the pipe 12 across which a constant pressure difference, independent of temperature changes in the gas, is maintained by the provision of a further venturi restriction 29 through which the gases pass at sonic speeds.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5264266A GB1215923A (en) | 1966-11-24 | 1966-11-24 | Temperature sensing apparatus |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5264266A GB1215923A (en) | 1966-11-24 | 1966-11-24 | Temperature sensing apparatus |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1215923A true GB1215923A (en) | 1970-12-16 |
Family
ID=10464714
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5264266A Expired GB1215923A (en) | 1966-11-24 | 1966-11-24 | Temperature sensing apparatus |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1215923A (en) |
-
1966
- 1966-11-24 GB GB5264266A patent/GB1215923A/en not_active Expired
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