SU31190A1 - Internal combustion turbine - Google Patents
Internal combustion turbineInfo
- Publication number
- SU31190A1 SU31190A1 SU110390A SU110390A SU31190A1 SU 31190 A1 SU31190 A1 SU 31190A1 SU 110390 A SU110390 A SU 110390A SU 110390 A SU110390 A SU 110390A SU 31190 A1 SU31190 A1 SU 31190A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- internal combustion
- combustion turbine
- nozzle
- turbine
- compressed air
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title description 7
- 239000007789 gas Substances 0.000 description 9
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- 238000001816 cooling Methods 0.000 description 2
- 238000001704 evaporation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 230000009931 harmful effect Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000011819 refractory material Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 239000008400 supply water Substances 0.000 description 1
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Description
В авторском свидетельстве № 2337 описана трубима внутреннего горени , в которойдл уменьшени вредного вли ни высокой температуры рабочих газов, привод щей лопатки турбины быстров негодность, камера горени состоит из наружного цилиндра , внутреннего из огнеупорного материала с наружными ребрами и промежуточного цилиндра из листового материала , при чем сжатый воздух вводитс в пространство .между наружным и промежуточным цилиндрами дл охлаждени , их и добавочно через окна вб внутренний цилиндр, где смешиваетс с продуктами горени и понижает их емпературу. Продукты горени по выходе из рабочих лопаток турбины направл ютс в трубчатый холодильник и, охлаждаемые, удал ютс из него центробежным компрессором.The author's certificate No. 2337 describes the internal combustion tube, in which to reduce the harmful effects of the high temperature of the working gases, which causes the turbine blade to become unusable, the combustion chamber consists of an outer cylinder, an inner refractory material with outer ribs and an intermediate cylinder made of sheet material, with than compressed air is introduced into the space between the outer and intermediate cylinders for cooling them and, additionally, through the holes in the inner cylinder, where the mountain is mixed with products and Temperature and lowers them. Combustion products at the exit of the turbine rotor blades are sent to a tubular cooler and, cooled, are removed from it by a centrifugal compressor.
В предлагаемой турбине дл большего охлаждени газов, поступающих на рабочие лопатки, близ выходного конца газового сопла помещена форсунка, подаюи а распыленную сжатым воздухом воду. Истекающие газы перемешиваютс с распы ленной водой, котора , хот и отнимает теплоту от газов на свое испарение или подогревание, но не уменьшает кинетйче266 In the proposed turbine for greater cooling of the gases entering the working blades, a nozzle is placed near the exit end of the gas nozzle, supplying sprayed water with compressed air. The effluent gases are mixed with sprayed water, which, although it takes heat from the gases to its evaporation or heating, does not reduce the kinetics
ской энергии газов, поступающих на лопатки турбины.energy of gases entering the turbine blades.
На чертеже изображен продольный разрез камеры горени турбины внутреннего горени .The drawing shows a longitudinal section of the combustion chamber of the internal combustion turbine.
Близ выходного конца газового сопла 12 расположен под углом к оси сопла канал 57, в который ввинчена обычна форсунка 38, снабженна подвижной трубкой 39, служащей дл подачи сжатого воздуха. Сбоку к форсунке 38 присоединена труба 40, через которую подаетс вода. Выход щий из трубки 39 сжатый воздух распыливает захватываемую им воду и со значительной скоростью подает ее в общую струю истекающего из сопла газа, где смешиваетс с последним, и распыленна вода охлаждает как его, так и, частично, лопатки 13-77 турбины.Near the output end of the gas nozzle 12 is located at an angle to the axis of the nozzle channel 57, into which a conventional nozzle 38 is screwed, equipped with a movable tube 39, which serves to supply compressed air. At the side of the nozzle 38, a pipe 40 is connected through which water is supplied. The compressed air coming out of the tube 39 sprays the water it captures and at a considerable speed delivers it into the general stream of gas flowing out of the nozzle, where it mixes with the latter, and the sprayed water cools both it and, partially, the turbine blades 13-77.
Предмет изобретени .The subject matter of the invention.
В турбине внутреннего горени , описанной в авторском свидетельстве № 2337, применение форсунки 38, предназначенной дл подачи распыленной сжатым воздухом воды и помещенной близ выходного конца газового сопла 12.In the internal combustion turbine described in the author's certificate No. 2337, the use of a nozzle 38 is used to supply water sprayed with compressed air and placed near the outlet end of the gas nozzle 12.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU110390A SU31190A1 (en) | 1932-06-03 | 1932-06-03 | Internal combustion turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU110390A SU31190A1 (en) | 1932-06-03 | 1932-06-03 | Internal combustion turbine |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU2337A Addition SU62861A1 (en) | 1940-01-15 | 1940-01-15 | Blowing pipe for Genze steamer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU31190A1 true SU31190A1 (en) | 1933-07-31 |
Family
ID=48348537
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU110390A SU31190A1 (en) | 1932-06-03 | 1932-06-03 | Internal combustion turbine |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU31190A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1995023920A1 (en) * | 1994-03-02 | 1995-09-08 | Smeshannoe Tovarischestvo 'germes' | Process for the conversion of thermal energy into mechanical energy in a gas-turbine engine, and a gas-turbine engine |
-
1932
- 1932-06-03 SU SU110390A patent/SU31190A1/en active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1995023920A1 (en) * | 1994-03-02 | 1995-09-08 | Smeshannoe Tovarischestvo 'germes' | Process for the conversion of thermal energy into mechanical energy in a gas-turbine engine, and a gas-turbine engine |
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