SU128235A1 - Multidisc friction turbine with a tangential gas supply on the periphery and a gas outlet in the center of the turbine - Google Patents
Multidisc friction turbine with a tangential gas supply on the periphery and a gas outlet in the center of the turbineInfo
- Publication number
- SU128235A1 SU128235A1 SU643678A SU643678A SU128235A1 SU 128235 A1 SU128235 A1 SU 128235A1 SU 643678 A SU643678 A SU 643678A SU 643678 A SU643678 A SU 643678A SU 128235 A1 SU128235 A1 SU 128235A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- turbine
- center
- periphery
- gas outlet
- gas supply
- Prior art date
Links
- 238000005192 partition Methods 0.000 description 3
- 239000011324 bead Substances 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Description
Известна многодискова турбина трени Тесла и Ieeт низкий к.п.д., а также больший вес и габариты при одинаковой полезной мощности по сравнению с другими типами турбии.Known multidisc friction turbine Tesla and low efficiency, as well as more weight and size at the same net power compared with other types of touring.
Предлагаема многодискова турбина трени с тангенциальным кодЕодом газа иа периферии и отводом газа в центре турбины отличаетс тем, что в ее проточной части установлены изогнутые перегородки, выполненные в виде буртиков на торцовых поверхност х дисков- Така кснструкци турбины, вследствие возможности достижени наивыгоднейших скоростей на входе в турбину и на Еыходе из нее, а также в с возможностью придани траектории газа оптимальной длины, позвол ет получить большие к.п,д. при меньшем весе и габаритах по сравнению с многодисковой турбиной трени Тесла.The proposed multi-disk friction turbine with a tangential gas code and periphery and a gas outlet in the center of the turbine is characterized in that curved partitions are installed in its flow part, made in the form of collars on the end surfaces of the discs. the turbine and on the exit from it, as well as with the possibility of imparting the gas path to an optimal length, allows to obtain large kp, e. with less weight and dimensions compared to Tesla's multi-disk friction turbine.
На чертеже показана описываема многодискова турбина трени в лвух П|юекц11 х.The drawing shows the described multi-disk friction turbine in two of them.
Диски / турбины .расположены на небольшом рассто нии друг от друга. В проточной части турбины установлены изогнутые перегородки, выполненные виде буртиков 2 на торцовых поверхност х дисков. Подвод газа к турбине осуш,б,:твл етс через расположенные на периферии каналы 3, а отвод газа - в центре турбины.The discs / turbines are located a short distance from each other. In the flow part of the turbine, curved partitions are installed, made in the form of beads 2 on the end surfaces of the disks. The gas supply to the turbine is dried, b,: it passes through the peripheral channels 3, and the gas outlet is in the center of the turbine.
При движении газа в каналах, образованных буртиками 2 и дисками /, вследствие трени о стенки канала часть кинетической .энергии газа преобразуетс в механическую работу на валу 4.When gas moves in the channels formed by the flanges 2 and the disks /, due to friction against the channel walls, a part of the kinetic energy of the gas is converted into mechanical work on the shaft 4.
Предхмет изобретени Pre invention
Многодискова турбина трени с тангенциальным подводом газа па периферии и отводом газа HI центре турбины, отличаюш,а с тем, что, с целью увеличени к.п.д. и уменьшени веса и габаритов турбины , в ее проточной части у(Стаиовлены изогнутые перегородки, выполненные в виде буртиков на торцовых поверхност х дисков.A multidisk friction turbine with a tangential gas supply to the periphery and a gas outlet HI at the center of the turbine is different, and in order to increase the efficiency and reduce the weight and dimensions of the turbine, in its flow part, y (Curved partitions made in the form of shoulders on the end surfaces of the disks are staked.
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Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU643678A SU128235A1 (en) | 1959-11-10 | 1959-11-10 | Multidisc friction turbine with a tangential gas supply on the periphery and a gas outlet in the center of the turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU643678A SU128235A1 (en) | 1959-11-10 | 1959-11-10 | Multidisc friction turbine with a tangential gas supply on the periphery and a gas outlet in the center of the turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU128235A1 true SU128235A1 (en) | 1959-11-30 |
Family
ID=48399455
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU643678A SU128235A1 (en) | 1959-11-10 | 1959-11-10 | Multidisc friction turbine with a tangential gas supply on the periphery and a gas outlet in the center of the turbine |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU128235A1 (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4036584A (en) * | 1975-12-18 | 1977-07-19 | Glass Benjamin G | Turbine |
| US4255081A (en) * | 1979-06-07 | 1981-03-10 | Oklejas Robert A | Centrifugal pump |
| US4529354A (en) * | 1983-06-06 | 1985-07-16 | Klepesch Philip H | Total flow turbine |
| US5082428A (en) * | 1990-08-16 | 1992-01-21 | Oklejas Robert A | Centrifugal pump |
-
1959
- 1959-11-10 SU SU643678A patent/SU128235A1/en active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4036584A (en) * | 1975-12-18 | 1977-07-19 | Glass Benjamin G | Turbine |
| US4255081A (en) * | 1979-06-07 | 1981-03-10 | Oklejas Robert A | Centrifugal pump |
| US4529354A (en) * | 1983-06-06 | 1985-07-16 | Klepesch Philip H | Total flow turbine |
| US5082428A (en) * | 1990-08-16 | 1992-01-21 | Oklejas Robert A | Centrifugal pump |
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