SU1287698A1 - Cooling system for fuel equipment - Google Patents
Cooling system for fuel equipmentInfo
- Publication number
- SU1287698A1 SU1287698A1 SU3675723/06A SU3675723A SU1287698A1 SU 1287698 A1 SU1287698 A1 SU 1287698A1 SU 3675723/06 A SU3675723/06 A SU 3675723/06A SU 3675723 A SU3675723 A SU 3675723A SU 1287698 A1 SU1287698 A1 SU 1287698A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- circuit
- turbine
- nozzle
- cavity
- cooling system
- Prior art date
Links
Landscapes
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
Система охлаждения тепловыделяющего оборудования, содержащая разомкнутый воздушный циркуляционный контур и включенные в него одной полостью воздухо-воздушный теплообменник, установленный второй полостью в продувочной магистрали, регулятор расхода, турбину, замкнутую камеру с размещенным в ней охлаждаемым оборудованием, датчики давления, температуры и расхода, отличающаяся тем, что, с целью повышения экономичности при использовании системы для охлаждения генератора, работающего в импульсном режиме и снабженного схемой включения, генератор заключен в теплоинерционный кожух, подключенный на входе к контуру после турбины, а на выходе сообщенный с камерой контур имеет сопло с критическим сечением, расположенное внутри продувочной магистрали после теплообменника, при этом датчики расположены после камеры перед соплом и электрически связаны со схемой включения генератора.The cooling system of the heat-generating equipment, containing an open air circulation circuit and an air-air heat exchanger installed by one cavity, installed by a second cavity in the purge line, a flow regulator, a turbine, a closed chamber with cooled equipment placed in it, pressure, temperature and flow sensors, which differ the fact that, in order to increase efficiency when using a system for cooling a generator operating in a pulsed mode and equipped with a switching circuit, erator enclosed in teploinertsionny casing connected at the input to the circuit after the turbine and its output communicating with the cam contour has a nozzle with the throat disposed within the purge line after the heat exchanger, wherein the sensors are located after the chamber upstream of the nozzle and is electrically connected with the generator enable circuit.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU3675723/06A SU1287698A1 (en) | 1983-12-20 | 1983-12-20 | Cooling system for fuel equipment |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU3675723/06A SU1287698A1 (en) | 1983-12-20 | 1983-12-20 | Cooling system for fuel equipment |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1287698A1 true SU1287698A1 (en) | 2006-09-27 |
Family
ID=60542869
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU3675723/06A SU1287698A1 (en) | 1983-12-20 | 1983-12-20 | Cooling system for fuel equipment |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1287698A1 (en) |
-
1983
- 1983-12-20 SU SU3675723/06A patent/SU1287698A1/en active
Similar Documents
Publication | Publication Date | Title |
---|---|---|
ES473882A1 (en) | Apparatus for generating thermal energy and electrical energy | |
ES457664A1 (en) | Marine engine manifold | |
GB1415867A (en) | Device for cooling an electric generator | |
SE8102975L (en) | DEVICE FOR A FIREFUL STOVE | |
FR2384106A1 (en) | IC engine cooling system - has pump driven by electric motor with control circuit receiving constant voltage input and variable input from temp. transducer | |
GB1539166A (en) | Internal combustion engine | |
KR840001300A (en) | Fuel control device for internal combustion engine | |
KR870004457A (en) | Hydrogen recombination unit | |
SU1287698A1 (en) | Cooling system for fuel equipment | |
ES8606628A1 (en) | Water box and expansion chamber device for a heat exchanger, in particular a radiator for a motor vehicle | |
ATE126323T1 (en) | COMBINED GAS-STEAM TURBINE SYSTEM FOR GENERATING ELECTRICAL ENERGY. | |
SE8404617L (en) | SYSTEM FOR PREVENTING TURBINE ICE CREATION | |
FR2397532A1 (en) | Composite power generator unit - has engine and generator supported on foundation consisting of exhaust and coolant heat exchangers | |
SE7906218L (en) | VERMEPUMPDRIVNING | |
SU478497A2 (en) | Equipment cooling system | |
SU883528A1 (en) | Method of cooling flow-through portion of vapour-gas unit gas turbine | |
GB1242592A (en) | Improvements relating to gas-turbine installations | |
SU857646A1 (en) | Regenerative air preheater | |
SU809766A1 (en) | Air cooling system on the aircraft | |
SU604268A1 (en) | Installation of air cooling on aircraft | |
JPS57206709A (en) | Engine | |
SU1000560A1 (en) | Energy conversion apparatus | |
JPS56130531A (en) | Combustion device | |
JPS5631818A (en) | Method of cooling vehicle room with energy economization | |
SU572993A1 (en) | Aircraft cooling system |