SU137730A1 - Combined turbo-rotary piston power installation - Google Patents
Combined turbo-rotary piston power installationInfo
- Publication number
- SU137730A1 SU137730A1 SU681093A SU681093A SU137730A1 SU 137730 A1 SU137730 A1 SU 137730A1 SU 681093 A SU681093 A SU 681093A SU 681093 A SU681093 A SU 681093A SU 137730 A1 SU137730 A1 SU 137730A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- rotary piston
- power installation
- piston power
- combined turbo
- turbo
- Prior art date
Links
Landscapes
- Supercharger (AREA)
Description
Известны комбинированные турбо-роторно-поршневые силовые установки , состо щие из двухтактного роторно-поршневого агрегата, например двигател или генератора газа, и расположенных по обе стороны от него газовой турбины и турбокомпрессора. Однако габариты таких установок велики.Combined turbo-rotary-piston power units are known, consisting of a push-pull rotary-piston unit, such as an engine or a gas generator, and located on either side of it of a gas turbine and a turbo-compressor. However, the dimensions of such installations are large.
В описываемой комбинированной турбо-роторно-поршневой силовой установке указанный недостаток устранен тем, что дл уменьшени общих габаритов установки и сокращени длины газовых каналов вал роторно-поршневого агрегата, «апример двигател или генератора газа, выполнен пустотелым, а внутри его полости соосно с ним располончен общий вал турбины и компрессора, на концах которого установлены их рабочие колеса.In the described combined turbo-rotor-piston power plant, this disadvantage is eliminated by the fact that in order to reduce the overall dimensions of the installation and reduce the length of the gas channels, the shaft of the rotor-piston unit, such as an engine or gas generator, is hollow a common shaft of the turbine and compressor, at the ends of which their impellers are installed.
На чертеже изображена установка.The drawing shows the installation.
Комбинированна турбо-роторно-норщнева силова установка состоит из газовой турбины 1, компрессора 2 и двухтактного роторнопоршневого генератора 3 газа.The combined turbo-rotary-norschnev power plant consists of a gas turbine 1, a compressor 2 and a two-stroke rotary piston generator 3 of gas.
При вращении рабочего колеса 4 компрессора 2 воздух подаетс через впускные окна 5 в цилиндр б, где, смещива сь с впрыснутым топливом, он образует горючую смесь, котора затем сжимаетс поршн ми 7 и воспламен етс . Расширившиес продукты сгорани через выпускные окиа 8 поступают на рабочее колесо 9 газовой турбины 1 и привод т его во вращательное движение.When the impeller 4 of compressor 2 is rotated, air is supplied through inlet ports 5 into cylinder b, where, displaced with the injected fuel, it forms a combustible mixture, which is then compressed by pistons 7 and ignited. The expanded combustion products through the exhaust ports 8 are fed to the impeller 9 of the gas turbine 1 and cause it to rotate.
Часть мощности, развиваемой турбиной 1, расходуетс на вращение рабочего колеса 4, сид щего с колесом 9 на одном валу 10, проход щем внутри полости 11 пустотелого эксцентрикового вала 12 роторно-поршневого генератора 3, а часть может сниматьс с установки как со стороны газовой турбины 1, так и со стораны компрессора 2.Part of the power developed by the turbine 1 is consumed to rotate the impeller 4 sitting with the wheel 9 on one shaft 10 passing inside the cavity 11 of the hollow eccentric shaft 12 of the rotary-piston generator 3, and a part can be removed from the installation as from the gas turbine 1, and from the compressor side 2.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU681093A SU137730A1 (en) | 1960-10-05 | 1960-10-05 | Combined turbo-rotary piston power installation |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU681093A SU137730A1 (en) | 1960-10-05 | 1960-10-05 | Combined turbo-rotary piston power installation |
Publications (1)
Publication Number | Publication Date |
---|---|
SU137730A1 true SU137730A1 (en) | 1960-11-30 |
Family
ID=48293926
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU681093A SU137730A1 (en) | 1960-10-05 | 1960-10-05 | Combined turbo-rotary piston power installation |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU137730A1 (en) |
-
1960
- 1960-10-05 SU SU681093A patent/SU137730A1/en active
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