EA200401249A1 - TURBINE - Google Patents
TURBINEInfo
- Publication number
- EA200401249A1 EA200401249A1 EA200401249A EA200401249A EA200401249A1 EA 200401249 A1 EA200401249 A1 EA 200401249A1 EA 200401249 A EA200401249 A EA 200401249A EA 200401249 A EA200401249 A EA 200401249A EA 200401249 A1 EA200401249 A1 EA 200401249A1
- Authority
- EA
- Eurasian Patent Office
- Prior art keywords
- cylindrical drum
- open ends
- gears
- pair
- working fluid
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/32—Non-positive-displacement machines or engines, e.g. steam turbines with pressure velocity transformation exclusively in rotor, e.g. the rotor rotating under the influence of jets issuing from the rotor, e.g. Heron turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/24—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like
- F01D1/28—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like traversed by the working-fluid substantially radially
Abstract
Турбина содержит сегнерово колесо, выполненное в виде трубы 1, установленной с возможностью вращения, на трубе 1 радиально закреплена с противоположных сторон по крайней мере одна пара патрубков 3 с отогнутыми в противоположные стороны открытыми концами 4. Цилиндрический барабан 5 скреплен соосно с трубчатым валом 6, установленным с возможностью вращения, и охватывает сегнерово колесо. Цилиндрический поясок цилиндрического барабана 5 примыкает к отогнутым открытым концам 4 с зазором и на нем радиально закреплена с противоположных сторон по крайней мере одна пара патрубков 8 с открытыми концами 9, отогнутыми в разные стороны. Корпус 11 охватывает сегнерово колесо и цилиндрический барабан 5 и имеет штуцер 12 для выхода рабочего тела. Во втором корпусе 15 расположены валы 2 и 6, на которых размещены шестерни 16 и 17. Вал 18 отбора мощности расположен во втором корпусе 15 с возможностью вращения и на нем закреплены шестерни 19 и 20 кинематически связанные с шестернями 16 и 17. Рабочее тело подают в трубу 1 сегнерова колеса и далее в каналы каждой пары патрубков 3. Рабочее тело истекает с высокой скоростью из противоположных открытых концов 4, разгоняясь с обеспечением вращения сегнерова колеса. Поток рабочего тела попадает в полость цилиндрического барабана 5, приводя его во вращение, и далее, попадая в пару патрубков 8 цилиндрического барабана 5, истекает через открытые концы 9 с высокой скоростью, приводя во вращение барабан за счет создания момента реактивных сил. От вращающихся сегнерова колеса и цилиндрического барабана 5 вращения передаются соответственно валам 2 и 6 и далее через шестерни 16, 17 и 19, 20, 21 на вал 18 отбора мощности к потребителю.Международная заявка была опубликованаThe turbine contains a Segner wheel, made in the form of a pipe 1 mounted for rotation, on pipe 1 at least one pair of branch pipes 3 radially fixed on opposite sides with open ends bent away in opposite directions 4. The cylindrical drum 5 is fastened coaxially with the tubular shaft 6, rotatably mounted, and covers the Segner wheel. The cylindrical corbel of the cylindrical drum 5 adjoins the bent open ends 4 with a gap and at least one pair of branch pipes 8 with open ends 9 bent in different directions on it is radially fixed on opposite sides. The housing 11 covers the Segner wheel and the cylindrical drum 5 and has a fitting 12 for the exit of the working fluid. In the second case 15, shafts 2 and 6 are located, on which gears 16 and 17 are placed. The power takeoff shaft 18 is located in the second case 15 rotatably and gears 19 and 20 are attached kinematically connected with gears 16 and 17. The working fluid is fed pipe 1 Segner wheels and then into the channels of each pair of nozzles 3. The working fluid expires at high speed from opposite open ends 4, accelerating to ensure rotation of the Segner wheel. The flow of the working fluid enters the cavity of the cylindrical drum 5, causing it to rotate, and then, falling into a pair of nozzles 8 of the cylindrical drum 5, expires through the open ends 9 at high speed, causing the drum to rotate by creating a moment of reactive forces. From the rotating Segner wheel and the cylindrical drum 5, the rotations are transmitted respectively to the shafts 2 and 6 and further through the gears 16, 17 and 19, 20, 21 to the power take-off shaft 18 to the consumer. The international application was published
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2002110753/06A RU2217596C1 (en) | 2002-04-24 | 2002-04-24 | Turbine |
PCT/RU2003/000184 WO2003091547A1 (en) | 2002-04-24 | 2003-04-21 | Turbine |
Publications (2)
Publication Number | Publication Date |
---|---|
EA200401249A1 true EA200401249A1 (en) | 2005-02-24 |
EA005939B1 EA005939B1 (en) | 2005-08-25 |
Family
ID=29268131
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EA200401249A EA005939B1 (en) | 2002-04-24 | 2003-04-21 | Turbine |
Country Status (5)
Country | Link |
---|---|
AU (1) | AU2003231434A1 (en) |
EA (1) | EA005939B1 (en) |
RU (1) | RU2217596C1 (en) |
UA (1) | UA74514C2 (en) |
WO (1) | WO2003091547A1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2597351C2 (en) * | 2012-04-24 | 2016-09-10 | Николай Фомич Архипов | Internal combustion engine |
CN103758582A (en) * | 2013-01-03 | 2014-04-30 | 摩尔动力(北京)技术股份有限公司 | Low-entropy turbine |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SU26306A1 (en) * | 1930-10-13 | 1932-05-31 | П.И. Бакулин | Reactive turbine |
US3032988A (en) * | 1959-06-10 | 1962-05-08 | Loyal W Kleckner | Jet reaction turbine |
US3930744A (en) * | 1973-10-10 | 1976-01-06 | Hollymatic Corporation | Pressure gas engine |
YU46140B (en) * | 1984-03-07 | 1993-05-28 | Stojčić, Tode | TURBINE WITH OPPOSITE ROTARY ROTORS |
-
2002
- 2002-04-24 RU RU2002110753/06A patent/RU2217596C1/en not_active IP Right Cessation
-
2003
- 2003-04-21 AU AU2003231434A patent/AU2003231434A1/en not_active Abandoned
- 2003-04-21 EA EA200401249A patent/EA005939B1/en not_active IP Right Cessation
- 2003-04-21 WO PCT/RU2003/000184 patent/WO2003091547A1/en not_active Application Discontinuation
- 2003-04-21 UA UA20041109682A patent/UA74514C2/en unknown
Also Published As
Publication number | Publication date |
---|---|
RU2217596C1 (en) | 2003-11-27 |
AU2003231434A1 (en) | 2003-11-10 |
EA005939B1 (en) | 2005-08-25 |
WO2003091547A1 (en) | 2003-11-06 |
UA74514C2 (en) | 2005-12-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MM4A | Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s) |
Designated state(s): KG MD TJ TM |
|
MM4A | Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s) |
Designated state(s): AM AZ BY KZ RU |