EA200401249A1 - TURBINE - Google Patents

TURBINE

Info

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
Application number
EA200401249A
Other languages
Russian (ru)
Other versions
EA005939B1 (en
Inventor
Радислав Николаевич Воробьев
Анатолий Михайлович Зелинский
Original Assignee
Общество С Ограниченной Ответственностью "Мидера-К"
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 Общество С Ограниченной Ответственностью "Мидера-К" filed Critical Общество С Ограниченной Ответственностью "Мидера-К"
Publication of EA200401249A1 publication Critical patent/EA200401249A1/en
Publication of EA005939B1 publication Critical patent/EA005939B1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/32Non-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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/24Non-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
    • F01D1/28Non-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

EA200401249A 2002-04-24 2003-04-21 Turbine EA005939B1 (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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