GB582260A - Improvements in or relating to temperature control for aircraft instruments - Google Patents
Improvements in or relating to temperature control for aircraft instrumentsInfo
- Publication number
- GB582260A GB582260A GB13022/44A GB1302244A GB582260A GB 582260 A GB582260 A GB 582260A GB 13022/44 A GB13022/44 A GB 13022/44A GB 1302244 A GB1302244 A GB 1302244A GB 582260 A GB582260 A GB 582260A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- oil
- relating
- temperature control
- instrument
- 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
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D23/00—Control of temperature
- G05D23/185—Control of temperature with auxiliary non-electric power
- G05D23/1854—Control of temperature with auxiliary non-electric power with bimetallic element
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Temperature-Responsive Valves (AREA)
- Measuring Fluid Pressure (AREA)
Abstract
582,260. Heating aircraft instruments. UNITED AIRCRAFT CORPORATION. July 7, 1944, No. 13022. Convention date, Jan. 29. [Class 64 (ii)] [Also in Group.XXIX] A thermostatic valve 20, comprising a bimetallic element 22 actuating a balanced piston valve member 21, is provided for regulating the flow of oil from two different discharge points 11, 12 at different temperatures from an aircraft engine 10 and supplying it at constant temperature to an instrument 24 such as an electric torque meter or strain gauge The two conduits 11, 12 discharge into tanks 13 from where the oil is pumped by pumps 17 to valve 20 under control of pressure relief valves 14 from where it passes to a conduit 23 and is circulated through or around the instrument casing 24.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US582260XA | 1944-01-29 | 1944-01-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB582260A true GB582260A (en) | 1946-11-11 |
Family
ID=22015469
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB13022/44A Expired GB582260A (en) | 1944-01-29 | 1944-07-07 | Improvements in or relating to temperature control for aircraft instruments |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB582260A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1403475B1 (en) * | 2002-09-26 | 2007-12-12 | Mann+Hummel Gmbh | Combined fluid filter and heat exchanger device |
CN107642622A (en) * | 2017-10-10 | 2018-01-30 | 河南工程学院 | Chemical experiment water-bath system |
-
1944
- 1944-07-07 GB GB13022/44A patent/GB582260A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1403475B1 (en) * | 2002-09-26 | 2007-12-12 | Mann+Hummel Gmbh | Combined fluid filter and heat exchanger device |
CN107642622A (en) * | 2017-10-10 | 2018-01-30 | 河南工程学院 | Chemical experiment water-bath system |
CN107642622B (en) * | 2017-10-10 | 2023-04-07 | 河南工程学院 | Water bath system for chemistry experiments |
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