SU31718A1 - Reactive internal combustion turbine - Google Patents
Reactive internal combustion turbineInfo
- Publication number
- SU31718A1 SU31718A1 SU89252A SU89252A SU31718A1 SU 31718 A1 SU31718 A1 SU 31718A1 SU 89252 A SU89252 A SU 89252A SU 89252 A SU89252 A SU 89252A SU 31718 A1 SU31718 A1 SU 31718A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- internal combustion
- combustion turbine
- turbine
- reactive internal
- combustion
- Prior art date
Links
Landscapes
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
Description
В предлагаемой реактивной fyp6HHe внутреннего горени с камерами горени , расположенными во вращающемс колесе, с целью создани реакции взрыва в камере, продукты горени выпускаютс через отверсти , помещенные в стенках камер с автоматическими клапанами, открывающимис в последующую по направлению вращени турбины камеру, сообщаемую с выпускной трубой.In the proposed reactive fyp6HHe internal combustion with combustion chambers located in a rotating wheel, in order to create an explosion reaction in the chamber, the combustion products are discharged through openings placed in the walls of the chambers with automatic valves opening in the subsequent turbine direction of the chamber communicating with the exhaust pipe .
На чертеже фиг. 1 изображает схематический поперечный разрез реактивной турбины внутреннего горени с одной свечей; фиг. 2-то же, сдвум свечами.In FIG. 1 shows a schematic cross-section of a jet turbine for internal combustion with one candle; FIG. 2 the same, with two candles.
В кожухе С турбины помещено колесо с расположенными в нем камерами горени , стенки а которых снабжены отверсти ми с автоматическими клапанами k. Горючее поступает в камеры по трубе d, и при взрыве его, посредством зажигани электрической запальной свечи е, образовавшиес газы открывают клапан k, через который газы вырываютс в соседнюю, последующую по направлению вращени камеру.In the casing C of the turbine there is a wheel with combustion chambers located in it, the walls of which are provided with openings with automatic valves k. The fuel enters the chambers through pipe d, and when it explodes, by igniting an electric glow plug e, the resulting gases open valve k, through which the gases are pulled into the next chamber, which follows in the direction of rotation.
в этот момент сообщающуюс с выхлопной трубой В, а созданна реакци взрыва приводит во вращение колесо. При подходе к трубе d следующей камеры , в нее поступает соответствующа порци горючего, воспламен етс и т. д. Турбина, изображенна на фиг. 2, снабжена двум подвод щими горючее трубами d и двум запальными свечами е дл возможности производства взрыва одновременно в двух камерах горени с целью повыщени скорости вращени турбины.at that moment, communicating with the exhaust pipe B, and the created explosion reaction causes the wheel to rotate. When approaching the tube d of the next chamber, the corresponding portion of fuel enters it, ignites, etc. The turbine shown in FIG. 2, is provided with two fuel feed pipes d and two glow plugs e for enabling the explosion to occur simultaneously in two combustion chambers in order to increase the rotational speed of the turbine.
Предмет изобретени .The subject matter of the invention.
Реактивна турбина внутреннего горени с камерами горени , расположенными во вращающемс колесе, отличающа с тем, что стенки а камер горени снабжены отверсти ми Ь с автоматическими клапанами k, открывающимис в соседнюю камеру горени , последующую по направлению вращени , котора сообщаетс с выпускной трубой В,An internal combustion turbine with combustion chambers located in a rotating wheel, characterized in that the walls of the combustion chambers are provided with openings b with automatic valves k opening into the adjacent combustion chamber, which follows in the direction of rotation, which communicates with the exhaust pipe B,
фиг.FIG.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU89252A SU31718A1 (en) | 1931-05-30 | 1931-05-30 | Reactive internal combustion turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU89252A SU31718A1 (en) | 1931-05-30 | 1931-05-30 | Reactive internal combustion turbine |
Publications (1)
Publication Number | Publication Date |
---|---|
SU31718A1 true SU31718A1 (en) | 1933-08-31 |
Family
ID=48349014
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU89252A SU31718A1 (en) | 1931-05-30 | 1931-05-30 | Reactive internal combustion turbine |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU31718A1 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6298653B1 (en) | 1996-12-16 | 2001-10-09 | Ramgen Power Systems, Inc. | Ramjet engine for power generation |
US6446425B1 (en) | 1998-06-17 | 2002-09-10 | Ramgen Power Systems, Inc. | Ramjet engine for power generation |
US6510683B1 (en) | 1992-09-14 | 2003-01-28 | Ramgen Power Systems, Inc. | Apparatus for power generation with low drag rotor and ramjet assembly |
WO2004097178A2 (en) * | 2003-04-28 | 2004-11-11 | Kostioukov Vladimir Nikolaevic | Intermittent gas-turbine engine |
RU2717473C2 (en) * | 2015-02-17 | 2020-03-23 | Сафран Хеликоптер Энджинз | Constant-volume combustion system for gas turbine engine of aircraft engine |
-
1931
- 1931-05-30 SU SU89252A patent/SU31718A1/en active
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6510683B1 (en) | 1992-09-14 | 2003-01-28 | Ramgen Power Systems, Inc. | Apparatus for power generation with low drag rotor and ramjet assembly |
US6298653B1 (en) | 1996-12-16 | 2001-10-09 | Ramgen Power Systems, Inc. | Ramjet engine for power generation |
US6334299B1 (en) | 1996-12-16 | 2002-01-01 | Ramgen Power Systems, Inc. | Ramjet engine for power generation |
US6434924B1 (en) | 1996-12-16 | 2002-08-20 | Ramgen Power Systems, Inc. | Ramjet engine for power generation |
US6446425B1 (en) | 1998-06-17 | 2002-09-10 | Ramgen Power Systems, Inc. | Ramjet engine for power generation |
WO2004097178A2 (en) * | 2003-04-28 | 2004-11-11 | Kostioukov Vladimir Nikolaevic | Intermittent gas-turbine engine |
WO2004097178A3 (en) * | 2003-04-28 | 2004-12-23 | Vladimir Nikolaevic Kostioukov | Intermittent gas-turbine engine |
RU2717473C2 (en) * | 2015-02-17 | 2020-03-23 | Сафран Хеликоптер Энджинз | Constant-volume combustion system for gas turbine engine of aircraft engine |
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