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SU119039A1 - Installation for cooling internal combustion engines, such as aircraft - Google Patents

Installation for cooling internal combustion engines, such as aircraft

Info

Publication number
SU119039A1
SU119039A1 SU132659A SU132659A SU119039A1 SU 119039 A1 SU119039 A1 SU 119039A1 SU 132659 A SU132659 A SU 132659A SU 132659 A SU132659 A SU 132659A SU 119039 A1 SU119039 A1 SU 119039A1
Authority
SU
USSR - Soviet Union
Prior art keywords
installation
internal combustion
aircraft
combustion engines
steam
Prior art date
Application number
SU132659A
Other languages
Russian (ru)
Inventor
И.В. Варшавский
Original Assignee
И.В. Варшавский
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by И.В. Варшавский filed Critical И.В. Варшавский
Priority to SU132659A priority Critical patent/SU119039A1/en
Application granted granted Critical
Publication of SU119039A1 publication Critical patent/SU119039A1/en

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Landscapes

  • Supercharger (AREA)

Description

Установки системы охлаждени  двигателей внутреннего сгорани  с использованием пара, образующего в рубашках цилиндров дл  вращени  паровой турбины и с использованием тепла выхлопных газов дл  дополнительного подогрева воды, известны.The installation of a cooling system for internal combustion engines using steam, which forms cylinder jackets for rotating a steam turbine and using exhaust heat for additional heating of water, is known.

Однако, такие установки имеют р д существенных недостатков.However, such installations have a number of significant drawbacks.

Мощность двигател  при наддуве не увеличиваетс  в случае вращени  компрессора газовой турбиной, так как создаваемое последней противодавление почти настолько же уменьшает мощность двигател , насколько она увеличиваетс  от наддува.Engine power during supercharging does not increase in the case of compressor rotation by the gas turbine, since the back pressure created by the latter almost reduces engine power as much as it increases from supercharging.

При вращении же компрессора от вала двигател , расход мощности на компрессор может превзойти прибавочную мощность двигател  от наддува. При работе двигател  на сто нке самолета, пар не может быть достаточно конденсирован воздухом, вследствие чего необходимо на сто нке часть пара выпускать в атмосферу, что уменьшает необходимый запас воды в системе при полете.When the compressor rotates from the engine shaft, the power consumption per compressor can surpass the engine's additional power from the boost. When the engine is working on the aircraft's station, the steam cannot be sufficiently condensed with air, as a result of which it is necessary to release some of the steam into the atmosphere on the station, which reduces the required water supply in the system during flight.

В описываемой установке указанные недостатки устранены тем, что парова  турбина соединена с компрессором, служащим дл  наддува охлаждаемого двигател . Дл  обеспечени  переключени  воздуха, подаваемого компрессором по мере надобности и в конденсатор, на воздушной магистрали установлены переключающие вентили.In the installation described, these disadvantages are eliminated by the fact that the steam turbine is connected to a compressor that serves to pressurize a cooled engine. In order to ensure the switching of the air supplied by the compressor as needed to the condenser, switching valves are installed on the air line.

На чертеже изображена схема установки парового охлаждени  двигател  внутреннего сгорани . В установке на одном валу с паровой турбиной 1 установлен компрессор 2, подающий сжатый водух по трубопроводу 3 через вентиль 4 в цилиндры 5 двигател  внутреннего сгорани .The drawing shows a diagram of the installation of steam cooling of the internal combustion engine. In the installation on the same shaft with the steam turbine 1, a compressor 2 is installed, which supplies compressed water through pipeline 3 through valve 4 to the cylinders 5 of the internal combustion engine.

Образующийс  в рубашках и головках цилиндров 5 двигател  из воды пар определенного давлени  по трубопроводу 6 через сборник 7 и регул тор 8 давлени  поступает на лопатки паровой турбины /, где пар развивает добавочную мощность. Из турбины пар направл етс  по трубопроводу 9 в вод ной или воздушный конденсатор 10, где он охлаждаетс . Образовавша с  из пара вода в конденсаторе 10 откачиваетс  насосом 7/ и далее по трубопроводу 12 прогон етс  через экономайзер 13, где подогреваетс  теплотой отход ших газов и направл етс  по трубопроводу 14 в рубашки и головки цилиндров 5 двигател .The steam formed in shirts and cylinder heads 5 of the water from a water of a certain pressure through the pipeline 6 through the collector 7 and the pressure regulator 8 enters the blades of the steam turbine /, where the steam develops additional power. From the turbine, steam is directed through conduit 9 to a water or air condenser 10, where it is cooled. The water formed from the steam in the condenser 10 is pumped out by the pump 7 / and then through the pipeline 12 is run through the economizer 13, where it is heated by the heat of exhaust gases and sent through the pipeline 14 to the jackets and the cylinder heads 5 of the engine.

SU132659A 1933-07-29 1933-07-29 Installation for cooling internal combustion engines, such as aircraft SU119039A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU132659A SU119039A1 (en) 1933-07-29 1933-07-29 Installation for cooling internal combustion engines, such as aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU132659A SU119039A1 (en) 1933-07-29 1933-07-29 Installation for cooling internal combustion engines, such as aircraft

Publications (1)

Publication Number Publication Date
SU119039A1 true SU119039A1 (en) 1958-11-30

Family

ID=48391021

Family Applications (1)

Application Number Title Priority Date Filing Date
SU132659A SU119039A1 (en) 1933-07-29 1933-07-29 Installation for cooling internal combustion engines, such as aircraft

Country Status (1)

Country Link
SU (1) SU119039A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5609029A (en) * 1993-07-08 1997-03-11 Wartsila Diesel International Ltd Oy Thermal power engine and its operating method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5609029A (en) * 1993-07-08 1997-03-11 Wartsila Diesel International Ltd Oy Thermal power engine and its operating method

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