WO1993020343A1 - Procede de transformation de l'energie thermique en energie mecanique dans un turbomoteur - Google Patents

Procede de transformation de l'energie thermique en energie mecanique dans un turbomoteur Download PDF

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Publication number
WO1993020343A1
WO1993020343A1 PCT/RU1992/000125 RU9200125W WO9320343A1 WO 1993020343 A1 WO1993020343 A1 WO 1993020343A1 RU 9200125 W RU9200125 W RU 9200125W WO 9320343 A1 WO9320343 A1 WO 9320343A1
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WO
WIPO (PCT)
Prior art keywords
газ
source
gas engine
engine
nagρeτοgο
Prior art date
Application number
PCT/RU1992/000125
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English (en)
Russian (ru)
Inventor
Anatoly Mikhailovich Rakhmailov
Vadim Arkadievich Kostinsky
Igor Leonidovich Drozd
Original Assignee
Smeshannoe Tovarischestvo 'germes'
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 Smeshannoe Tovarischestvo 'germes' filed Critical Smeshannoe Tovarischestvo 'germes'
Publication of WO1993020343A1 publication Critical patent/WO1993020343A1/fr

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/32—Inducing air flow by fluid jet, e.g. ejector action

Definitions

  • the invention is supplied to energy, and the name is a method for converting thermal energy into a mechanical engine and a gas-driven motor.
  • a gas turbine engine which is smaller than two located in a conventional part, is known
  • the air is taken from the machine and is empty, and the heat source is used as a camera to save heat.
  • U rania at the same time, they give fuel.
  • the combustion chamber is divided into two parts, one of which is used to commercially empty the boiler, and the other is used to reduce the load.
  • the resulting heated working body is expanding into the system.
  • the gas engine of the gas engine is partly used by the compressor, while the remaining motorized vehicle is partially mobilized.
  • the usable capacity of a gas engine is comparatively weak.
  • the engine 15 is compressed in a compressor, as a result of which a small amount of fuel is supplied, the engine is designed to lower the engine power.
  • the coefficient of excess oxidizer 1.7 is reached, a disruption of combustion occurs, and the engine
  • P ⁇ s ⁇ avlennaya task ⁇ eshae ⁇ sya ⁇ em, ch ⁇ in s ⁇ s ⁇ be - ⁇ e ⁇ b ⁇ az ⁇ vaniya ⁇ e ⁇ l ⁇ v ⁇ zh ene ⁇ gii in me ⁇ aniches ⁇ uyu and gaz ⁇ u ⁇ - 30 binn ⁇ m dviga ⁇ ele having ⁇ chnuyu with Part vy ⁇ l ⁇ nym uchas ⁇ - ⁇ m, ⁇ meny ⁇ ey me ⁇ e ⁇ dnu ⁇ azmeschennuyu in ⁇ chn ⁇ y chas ⁇ i ⁇ u ⁇ binnuyu s ⁇ u ⁇ en with vy ⁇ d ⁇ m and is ⁇ chni ⁇ nag ⁇ e ⁇ g ⁇ ⁇ ab ⁇ che- g ⁇ ⁇ ela with As a result, the supply of the source of the heated working body is fuel and the oxidizer and the resultant is a working 35 body.
  • the work load is transported to the turbine stage and the circuit is separated from the main part between - - the output of the heated working body and the outlet of the turbine stage. After exiting the source, the heated working body expands the heated working body, and then it is cooled before transferring to the turbine stage.
  • a handy working body is a good way to take care of a working person who has a working step.
  • ⁇ a v ⁇ d is ⁇ chni ⁇ a nag ⁇ e ⁇ g ⁇ ⁇ ab ⁇ cheg ⁇ ⁇ ela ⁇ dayu ⁇ mn ⁇ zhes ⁇ v ⁇ ⁇ v vs ⁇ m ⁇ ga ⁇ eln ⁇ zh ⁇ e ⁇ uchezh s ⁇ edy, za ⁇ - ⁇ uchenny ⁇ ⁇ n ⁇ si ⁇ eln ⁇ ⁇ d ⁇ ln ⁇ y ⁇ si gaz ⁇ u ⁇ binn ⁇ g ⁇ motion
  • a separate working body after expansion connects to an empty working body, which is not connected to a separate building. However, this does not reduce the kinetic energy of the working body, the resulting heated or primary device
  • the operating unit that has been operated has been disconnected from the connection to the quick-loading unit.
  • E ⁇ is ⁇ ⁇ di ⁇ blag ⁇ da ⁇ ya ⁇ mu, ch ⁇ umeny ⁇ ae ⁇ sya ⁇ az- n ⁇ s ⁇ LKAU s ⁇ s ⁇ yami smeshivaemy ⁇ ⁇ v, ch ⁇ snizhae ⁇ ⁇ e ⁇ i ene ⁇ gii on uda ⁇ .
  • the operating unit the primary cooler-35
  • the operating unit is provided by an oxidizing agent that is compatible with the source of heating of the body. This increases the temperature of the oxidizer and, consequently, the temperature of the heated body.
  • - 8 The working body, which is pre-cooled by the fuel, is compatible with the source of the heated body. At the same time, the fuel temperature goes up, which goes to the combustion with the simultaneous decrease in the temperature of the furnace, which improves the working temperature.
  • Fuel compatible with the source of the working body, sprays the cooling of the working body, is capable of the resultant operation. This contributes to the improvement of cooling efficiency due to more intensive evaporation of fuel.
  • a working person who is going to exhaust wit out of service on the part of the direct part between the exit of the exit step and the final part-time.
  • the operation of the working body is reduced due to the intermittent cooling of the working body, which is going to exhaust.
  • the appliance is used to improve the kinetic energy of the working body, which is provided to cool the cooler while it is in use.
  • the gas-powered engine provides a smaller unit, which is located at the same time as the resultant unit and the resultant
  • the engine is equipped with a device for creating a discharge at a part of the direct part of the room, which is equipped with an exhaust source for the output of the working body and the outlet of the waste bin.
  • the source of the heating circuit has been discharged, and the output has been discharged due to the loss of service - -
  • the first inlet of the ergot is communicated with the source of the heated body, the second inlet of the eriche is consumed, and With such a device, high efficiency is ensured.
  • the outlet for the first stage of the walkway is completed with the camera, which is communicated with the second output of the chamber for the most effective way of getting rid of the accident.
  • Ezhektrop may be located in the original part of the koltsy channel and radically installed for the convenience of the koltsy channel in the plates. Each plate is located at the corner " ⁇ to" Frequently Exercise diametral
  • Ezhektoo is equipped with a cooling unit.
  • an output section is provided in the upper section of the exhaust channel.
  • the good part of the source of the heated working circuit at the output may have the appearance of a con- fuser, and the part of the main part of the working time of the unit is
  • the engine may be equipped with an ejector that has
  • the propellant has reportedly been a source of fuel. Between the fuel sources and the fuel source, you must install the equipment for heating the fuel. If you are using a device for heating fuel, spray may be installed.
  • the source part of the source of the heated working body is
  • the short section has two narrowings, one of which is
  • the source of the heated working body can be made in the form of a ring chamber for burning with a catching unit that has an external collector, generally better
  • the internal “ flush-mounted version” can be made in the form of two communicating with the external collector, which is one of the larger parts, which is more
  • the second is located with the downstream source of the source of the heated working body. In this case, selective cooling of the heated working body for other parts of the primary source of heat is ensured.
  • Netting located on a short-term basis of the source of the finished working body, is a preferential area of 5-8 - - ⁇ l ⁇ schad ⁇ e ⁇ echn ⁇ g ⁇ section ve ⁇ vi ⁇ ubazhi, ⁇ azmeschenn ⁇ i with v ⁇ gnu ⁇ zh s ⁇ ny is ⁇ chni ⁇ a nag ⁇ e ⁇ g ⁇ ⁇ ab ⁇ cheg ⁇ ⁇ ela, P ⁇ i ⁇ a ⁇ y ⁇ ns ⁇ u ⁇ tsii ⁇ bes ⁇ echivae ⁇ sya ne ⁇ b ⁇ dim ⁇ e s ⁇ n ⁇ - shenie ⁇ liches ⁇ v ⁇ e ⁇ la, ⁇ v ⁇ dim ⁇ g ⁇ ⁇ ⁇ azny ⁇ uchas ⁇ v sme-
  • the engine is predominantly equipped with a convenient interchangeable device, which has hot and non-hazardous inputs that are connected to an output unit
  • the engine can be equipped with a removable device, while the hot-plug is connected to an externally connected external device. For such reasons as driving
  • fig. Provides the gas engine, which excludes the utilization of the process - 13 - thermal energy in the mechanical in a gas engine in accordance with the present invention
  • Fig. 2 is a schematic illustration of a gas-powered engine, in accordance with the present invention, in the vicinity of 5 times
  • FIG. 3 is a schematic illustration of a gas engine option with an electric engine for returning the fired unit to a consumable process
  • Fig. 4 is a schematic illustration of a variant of a gas turbine engine with another embodiment of an electric motor for returning to a consumable device
  • FIG. 7 is a schematic view of another gas-engine version with a short circuit to the mains; Fig.8 - ⁇ raz ⁇ without USh-USh on ig.7 (enlarged); ' fig . 9 - ⁇ az ⁇ ez ⁇ - ⁇ on fig.8; ⁇ ig. ⁇ - view of ⁇ on ⁇ ig.9; Consequently ⁇ - ⁇ - ⁇ réelle ⁇ réelle ⁇ réelle ⁇ ⁇ - ⁇ in Consequently ⁇ Communication ⁇ .7 (enlarged); 25 Fig. 2 is a schematic illustration of a still another version of a gas-powered engine with a secondary expansion of the processing unit, which is supplied to the power supply unit.
  • FIG. 1 shows a schematic diagram of a gas engine for the complete use of the present invention.
  • the gas engine has a source I of a heated working body, a turbine stage 2 and a device 3 for creating a discharge.
  • Home stage 2 and device 35 ⁇ 3 are connected by a shaft 4 to operate the device, which may be, for example, in the form of a fan.
  • a shaft 4 to operate the device, which may be, for example, in the form of a fan.
  • any device for the purpose of discharging the engine for example, for example - 14 - Holy Communion. Specialists have to take care that parts of the device are equipped with fixed parts and accessories.
  • FIG. 1 which has a working body with a step of 2, it starts up with a function.
  • the gas engine has two turbine stages 2 and 7.
  • the loss of expansion 5 takes the form of an infection. Installation 3 for building
  • Part 5 of the expansion has a window of 12 at the end of the download, which is communicated through channel 13 with an output of 14 at the end
  • Source I of the working body has a window of 15 at the source, communicating with the vehicle.
  • the device 3 for creating a discharge ensures the supply of an oxidizer (air) to the source of the first working body.
  • the gas engine shown in figure 2, works as follows. After starting the engine with a simple device (not shown), a quick part between the output 2 and the output 5 is unavailable. ⁇ As a result of air deactivation, the pressure is released through window 15 in source I, which also releases the fluid ().
  • the engine is less than two, located in the primary parts of the turbine stages 2 and 7, and, therefore, the primary turbine stage 2 has a free-wheeling unit.
  • the part has a source part 17 and a source I of a heated working body, made in the form of a burning chamber,
  • the main part of the engine 19 is for sale only.
  • step 2 is performed with the camera 25, which is communicated with the second input, which is available with 2 ⁇ windows (Fig. 4).
  • This camera is a collector for
  • the first stage 2 of the turbine does not have a simple device, since it performs the functions of the ejector 19.
  • the gas engine has a ⁇ and 8, 9, and 9 gas turbine units located in
  • the source I of the heated working body 35 parts 10, the source I of the heated working body, the source of the fuel, the schematically identified fuel lines ⁇ , for the supply of fuel.
  • Pell 32 (Pig. 8,9), having Fast. channels 33 (Fig. 9), complete with safety fittings, are fitted with an angle> -6 ⁇ 20- ⁇ 0 ° for the intersection Channel 31, through
  • the source part of the source I is the heated working
  • the gas engine is equipped with an engine 19 having an input 44, 26 and 45 and an output 4 ⁇ (FIG. 7) and a ring of 47.48 (FIG.).
  • the first input 44 of the blower 19 is communicated with the source I of the heated working body, the second input of 2 ⁇ blower 19 is communicated with
  • the higher gas turbine engine operates the following way.
  • boilers are 32 with channels 33; ⁇ n ⁇ zhes ⁇ v ⁇ ⁇ - ⁇ 30 ⁇ as ⁇ ylenn ⁇ g ⁇ and nag ⁇ e ⁇ g ⁇ ⁇ liva, za ⁇ uchenny ⁇ ⁇ n ⁇ si ⁇ eln ⁇ ⁇ si 0-0 gaz ⁇ u ⁇ binn ⁇ g ⁇ dviga ⁇ elya, d ⁇ lni- ⁇ eln ⁇ za ⁇ uchivayu ⁇ ⁇ ⁇ isli ⁇ elya in z ⁇ ne 34 is ⁇ chni- ⁇ a I nag ⁇ e ⁇ g ⁇ ⁇ ab ⁇ cheg ⁇ ⁇ ela ⁇ n ⁇ si ⁇ eln ⁇ ⁇ si 0-0 gaz ⁇ u ⁇ binn ⁇ g ⁇ dviga ⁇ elya.
  • ⁇ a uchas ⁇ e is ⁇ chni ⁇ a I nag ⁇ e ⁇ g ⁇ ⁇ ab ⁇ cheg ⁇ ⁇ ela z ⁇ nami v ⁇ da between 34 and 35 nag ⁇ eva ⁇ is ⁇ di ⁇ ⁇ asshi ⁇ enie ⁇ a ⁇ ab ⁇ cheg ⁇ ⁇ ela, ⁇ eds ⁇ avlyayuscheg ⁇ s ⁇ b ⁇ i mixture ⁇ liva and ⁇ isli- ⁇ elya and snizhae ⁇ sya s ⁇ s ⁇ ⁇ a ⁇ ab ⁇ cheg ⁇ ⁇ ela in di ⁇ u- z ⁇ e 43.
  • ⁇ z ⁇ ne 35 ⁇ is ⁇ di ⁇ nag ⁇ evanie ⁇ ab ⁇ cheg ⁇ ⁇ ela ⁇ i Combustion, heating, and evaporation in refrigerated coolers 39.40. Moreover, due to the lowered operating speed of the body, the increased efficiency of combustion is ensured with maximum use of fuel.
  • ⁇ z ⁇ ne Z ⁇ is ⁇ chni ⁇ a I nag ⁇ e ⁇ g ⁇ ⁇ ab ⁇ cheg ⁇ ⁇ ela ⁇ b ⁇ azue ⁇ sya za ⁇ uchenny ⁇ ⁇ n ⁇ si ⁇ eln ⁇ ⁇ d ⁇ ln ⁇ ⁇ si 0 -0 of the engine is extremely quick to heat and handle the burner, as it is burned, it is connected to the remote control unit 44 (optional) - - -
  • the source of the first working body is made in the form of the initial K-ring section 50, as it is received - -
  • the part of 51 which has a small amount of stability and the end part of 52, is irrelevant, which takes into account the second part, it takes into account the
  • ⁇ chnaya is ⁇ chni ⁇ a Part I nag ⁇ e ⁇ g ⁇ ⁇ ab ⁇ cheg ⁇ ⁇ ela imee ⁇ constriction 53.
  • the constriction 54 ⁇ e ⁇ as ⁇ l ⁇ zhen ⁇ in ⁇ n- tsev ⁇ chas ⁇ i 52 ⁇ iv ⁇ line ⁇ n ⁇ g ⁇ uchas ⁇ a 51.
  • ⁇ ezhdu narrowing niyami 53 and 54 ⁇ as ⁇ l ⁇ zhen uchas ⁇ 55 s ⁇ edineniya ⁇ v ⁇ ab ⁇ cheg ⁇ ⁇ ela with increasing ⁇ l ⁇ schadi ⁇ e ⁇ echn ⁇ g ⁇ section.
  • the second is located from the downstream of the source of the heated working body.
  • Hub 58, 57 is located at the source of the first working body, it has a larger area of 5-8 more than
  • the source of source I is running out of heat, resulting in a loss of process.
  • the cross section of the case 57 is higher than the specified range of the operating system, 59
  • the liquefied gas-fired engine operates the following way.
  • the device is not used as a source of heat, but the source is unloaded.
  • the combined process flows further move towards narrowing 54 of the end of the 52 source and I have failed to process the unit where there is an error.
  • ⁇ ⁇ ezul- ⁇ a ⁇ e is ⁇ lz ⁇ vaniya ⁇ e ⁇ l ⁇ bmenn ⁇ g ⁇ us ⁇ s ⁇ va 63 snizhae ⁇ - Xia ⁇ liches ⁇ v ⁇ ⁇ ab ⁇ avsheg ⁇ ⁇ ab ⁇ cheg ⁇ ⁇ ela, ⁇ davaem ⁇ g ⁇ for ⁇ lazhdeniya nag ⁇ e ⁇ g ⁇ ⁇ ab ⁇ cheg ⁇ ⁇ ela, ch ⁇ ⁇ vyshae ⁇
  • DIGITAL ENGINE 35 ⁇ DIGITAL ENGINE. This means that you are unable to heat up partly when it is in the process, and it is inaccessible to the computer when it is in the process of being charged. - 26 - unit 63. With this, the PDA of the following tubing rises.
  • the fuel of a gas engine is approximately 23–25 lower than that of a well-known engine of similar capacity.
  • the invention may be used in gas-fired power plants and, in particular, in installations, there are 15 charges for the use of industrial equipment.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

L'invention porte sur des turbomoteurs dont elle vise à augmenter le rendement et la fiabilité. Le carburant et le comburant sont amenés à une source (1) de fluide où, réchauffés, ils constituent un fluide de travail qui alimente un étage de turbine (2). Une dépression est établie dans une conduite d'amenée placée entre la sortie de cette source (1) de fluide de travail réchauffé et la sortie de l'étage de turbine (2). Le fluide de travail est dilaté après la sortie de la source (1), et refroidi avant d'être acheminé vers l'étage de turbine (2). Le turbomoteur comporte au moins un étage de turbine (2) placé au niveau de cette conduite d'amenée, ainsi qu'une source (2) de fluide de travail réchauffé dotée d'une entrée et d'une sortie et connectée à l'étage de turbine (2). Il se caractérise par un dispositif de création de dépression (3) disposé sur cette conduite d'amenée entre la source (1) et la sortie de l'étage de turbine (2). L'entrée (1) de la source (1) de fluide de travail réchauffé est reliée à la pression atmosphérique alors que sa sortie consiste en une section (5), où le fluide de travail subit une expansion, connectée avec la zone située entre la sortie vers l'étage de turbine (2) et le dispositif de création de dépression.
PCT/RU1992/000125 1992-04-07 1992-06-26 Procede de transformation de l'energie thermique en energie mecanique dans un turbomoteur WO1993020343A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU5031214 1992-04-07
SU5031214 RU2031225C1 (ru) 1992-04-07 1992-04-07 Способ преобразования тепловой энергии в механическую в газотурбинном двигателе и газотурбинный двигатель

Publications (1)

Publication Number Publication Date
WO1993020343A1 true WO1993020343A1 (fr) 1993-10-14

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PCT/RU1992/000125 WO1993020343A1 (fr) 1992-04-07 1992-06-26 Procede de transformation de l'energie thermique en energie mecanique dans un turbomoteur

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WO (1) WO1993020343A1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2188960C1 (ru) * 2001-08-20 2002-09-10 Кондрашов Борис Михайлович Способ преобразования энергии в силовой установке (варианты), струйно-адаптивном двигателе и газогенераторе
AU2002349371A1 (en) * 2002-07-17 2004-02-02 Boris Mihailovich Kondrashov Method for energy transformation in jet-engines
RU2474718C2 (ru) * 2011-01-25 2013-02-10 Николай Евгеньевич Староверов Способ форсажа турбодвигателя и двигатель для его реализации (варианты)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB196452A (en) * 1922-03-15 1923-04-26 Henry Andrews Hepburn Improvements in or relating to internal combustion turbine engines
GB412970A (en) * 1933-01-06 1934-07-06 British Thomson Houston Co Ltd Improvements in and relating to gas turbine cycles with interstage reheating
SU120087A1 (ru) * 1956-01-02 1958-11-30 В.Л. Дехтярев Полузамкнута газотурбинна установка
US4549402A (en) * 1982-05-26 1985-10-29 Pratt & Whitney Aircraft Of Canada Limited Combustor for a gas turbine engine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB196452A (en) * 1922-03-15 1923-04-26 Henry Andrews Hepburn Improvements in or relating to internal combustion turbine engines
GB412970A (en) * 1933-01-06 1934-07-06 British Thomson Houston Co Ltd Improvements in and relating to gas turbine cycles with interstage reheating
SU120087A1 (ru) * 1956-01-02 1958-11-30 В.Л. Дехтярев Полузамкнута газотурбинна установка
US4549402A (en) * 1982-05-26 1985-10-29 Pratt & Whitney Aircraft Of Canada Limited Combustor for a gas turbine engine

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
SCHNEE YA.I., "Gazovye Turbiny", 1960, Mashgiz (Moscow), page 96. *

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Publication number Publication date
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