SU31718A1 - Reactive internal combustion turbine - Google Patents

Reactive internal combustion turbine

Info

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
Application number
SU89252A
Other languages
Russian (ru)
Inventor
Б.К. Штавеман
Original Assignee
Б.К. Штавеман
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 Б.К. Штавеман filed Critical Б.К. Штавеман
Priority to SU89252A priority Critical patent/SU31718A1/en
Application granted granted Critical
Publication of SU31718A1 publication Critical patent/SU31718A1/en

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  • 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.

SU89252A 1931-05-30 1931-05-30 Reactive internal combustion turbine SU31718A1 (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (8)

* Cited by examiner, † Cited by third party
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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