SU78820A1 - Heating system of gas engine transport - Google Patents
Heating system of gas engine transportInfo
- Publication number
- SU78820A1 SU78820A1 SU4527A SU4527A SU78820A1 SU 78820 A1 SU78820 A1 SU 78820A1 SU 4527 A SU4527 A SU 4527A SU 4527 A SU4527 A SU 4527A SU 78820 A1 SU78820 A1 SU 78820A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- heating system
- gas
- gas engine
- engine
- engine transport
- Prior art date
Links
- 238000010438 heat treatment Methods 0.000 title description 5
- 239000007789 gas Substances 0.000 description 9
- 239000000203 mixture Substances 0.000 description 7
- 238000001816 cooling Methods 0.000 description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 239000000969 carrier Substances 0.000 description 1
- 239000002826 coolant Substances 0.000 description 1
Description
Изобрете ие касаетс сисгсмы прогрева транспортных двнгателсП путем пропускани через полости охлахсаени двигател пара и через трубу в картере двигател отход щих газов из вспомогательного котла , в топке которого сжигаетс газовоздушна смесь.The invention relates to the heating system for transporting diesel engines by passing steam through the engine cooling chambers and through a pipe in the engine crankcase of exhaust gases from an auxiliary boiler, in the furnace of which the gas-air mixture is burned.
Отл11Ч1гтелы1а особенность предлагаемой системы заключаемс п том, что дл приготоаленн н подэчи указанной смесн иснапьзустс служащий дл разжнганн газ генсраторз выт жной вентил тор, по;.с,1сыоаю1ЦнГ| необходимое количсстио «оздуха через открытый патрубок обычного газового смесител .The special feature of the proposed system lies in the fact that for the specified sub-mix of this mixture it is used for the gas that is used for the generation of exhaust gas, according to the; 1c, 1ccn | The amount of air required is through the open port of a conventional gas mixer.
Кроме того в системе применен незамкнутый контур прогрева полостей охлаждеин двигател с выпуском образуюи1еггх: конденсата наружу, что гарантирует от замерзани обратного трубопровода.In addition, the system uses an open loop for heating the cavities of the engine coolant with the release of condensate forming: condensate to the outside, which ensures that the return pipeline does not freeze.
11а чертеже схематично юображена предлагаема система прогрева транспортных газогенераторных двигателг-й .11a of the drawing shows schematically the proposed system for heating the gas-transport engine of engines.
Чррез открытый патрубок / воздух подсасываетс выт жным вентил тором 2 в обычный газовыйAn open pipe / air outlet is sucked by an exhaust fan 2 into a conventional gas
смес1гге ь 4, из которого газовоздушна смесь поступает в топку вспомогательного котла 3. В водопаровую руба1ику 5 котла вода поступает нз бачка 6.Mixture 4, from which the gas-air mixture enters the furnace of the auxiliary boiler 3. Water enters the water steam pipe 5 of the boiler from the tank 6.
Образопапшннс в котле пар по трубопроводу 7 подаетс в полости охлаждени двигател 8, а отход щие из топки газы подаютс по трубе Р в картер W двигател , откуда оии удал ютс через отверстие (на чертеже не показано) в атмосферу. Образующнйс конденсат нз полостен охлаждени двигател по трубке // выпускаетс наружу.The image of steam in the boiler through pipeline 7 is fed into the cooling cavities of the engine 8, and the gases coming from the furnace are fed through pipe P to the crankcase W of the engine, where they are removed through an opening (not shown) to the atmosphere. Formed condensate from the engine cooling cavity through the tube // is discharged to the outside.
Предмет нзобретенн Subject matter
1. Система прогрева транспортных газогенераторных двигателей пропускани через полости охлаждени двигател Tiapa и через трубу в картере двигател отход щих газов из вспомогательного котла, в топке которого сжигаетс газовоз, душна смесь, отличающа с тем , что дл приготовлени н подачи указанной смеси используетс служащий дл разжигани газогене127 ратора выт жной вентил тор, под асываюпшй необходимое колнчечггоо воздуха через открыл патрубшс обычного газо&ого смесн2 . В системе ло п. 1 рнме ен е незамкнутого контура прогрева по i лостеб охлажденн двнгател с пуском образующегос конденсата наружу.1. Heating system of transport gas-generating engines passing through the cooling cavities of the Tiapa engine and through the pipe in the engine crankcase of exhaust gases from the auxiliary boiler, in the furnace of which the gas carrier is burned, is a stuffy mixture, characterized in that it is used to ignite the mixture gas generator 127 exhaust fan, under the necessary air flow through the open air through the opening of a conventional gas & In the system of item 1 of pnme, the e of the unclosed warm-up contour by i hdder of the cooled cooling system with the start of the formed condensate to the outside.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4527A SU78820A1 (en) | 1947-03-25 | Heating system of gas engine transport |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4527A SU78820A1 (en) | 1947-03-25 | Heating system of gas engine transport |
Publications (3)
Publication Number | Publication Date |
---|---|
SU65766A1 SU65766A1 (en) | 1945-11-30 |
SU69726A1 SU69726A1 (en) | 1947-11-30 |
SU78820A1 true SU78820A1 (en) | 1950-02-28 |
Family
ID=
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1284335A (en) | Improvements in or relating to gas turbine engines | |
SU78820A1 (en) | Heating system of gas engine transport | |
GB1395418A (en) | Pollution rectifier | |
US1589391A (en) | Internal-combustion engine | |
SU83007A1 (en) | Gas turbine installation | |
SU80231A1 (en) | Method to facilitate the start of transport engines of internal combustion in winter conditions | |
GB1347421A (en) | Exhaust gas cleaning apparatus for an internal combustion engine | |
SU1659A1 (en) | The method of operation of the heat engine | |
FR2401319A1 (en) | Aircraft jet engine heat exchanger - includes water injection system to reduce temp. of inlet gases to safe level during take=off | |
SU40096A1 (en) | Engine-generator gas mixture | |
SU375398A1 (en) | INLET CARBURETTING ENGINE INTERNAL COMBUSTION SYSTEM | |
SU1721273A1 (en) | Combustion engine | |
SU3859A1 (en) | Steam injection device | |
GB460794A (en) | Internal combustion turbine | |
SU74137A1 (en) | Internal Combustion Turbine | |
SU79293A1 (en) | Air heater for locomotive boiler | |
SU86813A2 (en) | Suction pipe for carburetor internal combustion engines | |
GB298624A (en) | Improvements in or relating to two-stroke internal combustion engines | |
SU1112138A1 (en) | Device for supplying steam to internal combustion engine | |
SU39485A1 (en) | Method of using exhaust heat of internal combustion engines | |
RU1820020C (en) | Internal combustion engine | |
GB209874A (en) | Improvements in or relating to exhaust expansion chambers for internal combustion engines | |
SU459377A1 (en) | Oil Waste Disposal Device | |
SU91095A1 (en) | Gas turbine engine with heat regenerator | |
GB191837A (en) | Improvements relating to means for effecting a saving in fuel in internal combustion engines |