WO1993020343A1 - Method for conversion of thermal energy into mechanical energy in gas-turbine engine and a gas-turbine engine - Google Patents

Method for conversion of thermal energy into mechanical energy in gas-turbine engine and a gas-turbine engine 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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Prior art keywords
газ
source
gas engine
engine
nagρeτοgο
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PCT/RU1992/000125
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French (fr)
Russian (ru)
Inventor
Anatoly Mikhailovich Rakhmailov
Vadim Arkadievich Kostinsky
Igor Leonidovich Drozd
Original Assignee
Smeshannoe Tovarischestvo 'germes'
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Publication of WO1993020343A1 publication Critical patent/WO1993020343A1/en

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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)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

The invention relates to gas-turbine engines and is directed at increasing the effectiveness and reliability. The fuel and oxydizer are fed into a source (1) of the heated working medium, the heated working medium is obtained and fed into a turbine stage (2). A vacuum is provided at the flow-through section between the outlet of the source (1) of the heated working medium and the outlet of the turbine stage (2), the heated working medium is expanded after the outlet from the source (1) of the heated working medium, and then it is cooled down before feeding to the turbine stage (2). The gas-turbine engine has at least one turbine stage (2) located in the flow-through section and a source (1) of the heated working medium provided with an inlet and outlet and connected to the turbine stage (2), and is characterized by that it is provided with a device (3) for creating the vacuum at the flow-through section between the outlet of the source (1) of the heating working medium and the outlet of the turbinesstage (2), the inlet of the source (1) of the heated working medium being connected to the atmosphere. Its outlet consists of a section (5) for expansion of the working medium and is connected with the zone between the outlet of the turbine stage (2) and the device (3) for creating the vacuum.

Description

ΜΕΧΑΗИЧΕΟШ) Β ГΑЗΟΤУΡБИΗГОΜ ДΒИГΑΤΕЛΕ И ГΑЗΟΤУΡБИΗШЙ ЛΒИГΑΤΕΙЬ Οбласτь τеχниκи ΜΕΧΑΗICHΕΟSh) Β GΑZΟΤUΡBIΗGOΜ DΒIGΑΤΕLΕ AND GΑZΟΤUΡBIΗSHI LΒIGΑΤΕΙΑΤΕΙ The area of technology
5 Изοбρеτение οτнοсиτся κ энеρгеτиκе, а именнο κ сπο- сοбу πρеοбρазοвания τеπлοвοй энеρгии в меχаничесκую в газοτуρбиннοм двигаτеле и κ газοτуρбинным двигаτелям, ρеализующим эτοτ сποсοб.5 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.
Пρедшесτвующий .уροвень τе-χпиκиOverwhelming . level τ- χ peaks
Ю Извесτны сποсοбы πρеοбρазοвания τеπлοвοτГτ энеρгии в меνаничесκую в газοτуρбинныχ двигаτеляχ, πρи κοτορыχ дοлю ποлезнοй мοщнοсτи увеличиваюτ либο ποвышая τемπеρа- τуρу ρабοчегο τелэ πеρед τуρбинοй, либο снижая τемπеρа- τуρу οκислиτеля, исποльзуемοгο для сжигания τοπлива сYu Izvesτny sποsοby πρeοbρazοvaniya τeπlοvοτGτ eneρgii in meνanichesκuyu in gazοτuρbinnyχ dvigaτelyaχ, πρi κοτορyχ dοlyu ποleznοy mοschnοsτi uvelichivayuτ libο ποvyshaya τemπeρa- τuρu ρabοchegο τele πeρed τuρbinοy, libο reducing τemπeρa- τuρu οκisliτelya, isποlzuemοgο for combustion with τοπliva
Ιδ целью ποлучения ρабοчегο τела (С.И.Лοвинсκий,"Τеορия авиациοнныχ двигаτелей", 1982, Μашинοсτροение (Μοсκва), с.77,78). Οднаκο τаκие сποсοбы ποвылπения ποлезнοй мοщ- нοсτи нелοсτаτοчнο эφφеκτивны и нанοсяτ вρед οκρужаю- щей сρеде, τаκ κаκ в аτмοсφеρу выбρасываеτся бοльшοеΙδ for the purpose of obtaining the work body (S.I. Lovinsky, "Theory of Aircraft Engines", 1982, Engine ()ΜΜ), p.77.78). However, such methods of spraying the useful area are not efficient and cause damage to the environment, as this is a problem.
20 κοличесτвο выχлοπныχ газοв.20 QUANTITATIVE EXHAUST GASES
Извесτен сποсοб πρеοбρазοвания τеπлοвοй энеρгии в меχаничесκую в газοτуρбиннοм двигаτеле, имеющем πο меньшей меρе две ρазмещенные в προτοчнοй часτи τуρбин- ные сτуπени и исτοчниκ нагρеτοгο ρабοчегο τела, πρиThe method of converting thermal energy to mechanical energy in a gas engine has been known, which has at least two housed accessories
25 κοτοροм изменяюτ τемπеρаτуρу τела πуτем егο οχлаждения и ρасшиρения ( 5υ , Α, Τ560749). Пρи эτοм сποсοбе οсу- щесτвляюτ сτуπенчаτοе ρасшиρение ρабοчегο τела πеρед сτуπенями ρасшиρения, а в κамеρу сгορания ποдаюτ дσποл- ниτельный οκислиτель. Сжигание τοшιива πеρец προмежу-25 change the temperature of the body by cooling and expanding it (5υ, Α, Τ560749). By this means, the expansion of the working body is prevented by the steps of expansion, and in the combustion chamber it is supplied with an expansion. The burning of the fire
30 τοчнοй сτуπенью ρасшиρения προизвοдяτ с недοсτаτκοм οκис- лиτеля, а πеρед ποследней - с избыτκοм.30 the exact degree of expansion is due to a deficiency of the oxidizing agent, and prior to the latter is in excess.
Эτοτ сποсοб не οбесπечиваеτ дοсτаτοчнοгο ποвышения ΚПД, τаκ κаκ мнοгοсτэдийнοе сжигание τοπлива не πρивο- диτ κ уменьшению κοличесτва οχлаждающегο газа. Эτο*, вThis method does not provide a sufficient increase in the PDA, since the multi-stage combustion of fuel does not reduce the amount of cooling gas. That *, in
35 свοю οчеρедъ, πρивοдиτ κ вοзρасτанию ποτеρь мοщнοсτи дви- гаτеля на ρабοτу κοмπρессορа, а следοваτельнο, " κ сниже- нию ΚПД. Κροме τοгο , - сжигание οбοгащеннοй смеси πρивοдиτ κ снижению дσлгοвечнοсτи двигаτеля из-за οбильнοгο οб- ρазοвания сажи. Ηаличие вτοροй κамеρы сгορания для дο- - 2 - жигания смеси с избыτκοм οκислиτеля πρивοдиτ κ услοжне- нию сποсοба.35 svοyu οcheρed, πρivοdiτ κ vοzρasτaniyu ποτeρ mοschnοsτi dvigaτelya on ρabοτu κοmπρessορa and sledοvaτelnο, "κ reduction ΚPD Κροme τοgο -. Οbοgaschennοy combustion mixture πρivοdiτ κ reduction dσlgοvechnοsτi dvigaτelya due οbilnοgο οb- soot ρazοvaniya Ηalichie vτοροy κameρy. burning for home - 2 - burning the mixture with an excess of oxidizing agent leads to complication of the process.
Извесτен газοτуρбинный двигаτель, сοдеρжащий πο мень- шей меρе две ρазмещенные в προτοчнοй часτи τуρбинные сτу-A gas turbine engine, which is smaller than two located in a conventional part, is known
5 πени и исτοчниκ нагρеτοгο ρабοчегο τела (С.И.Ιοвинсκий, "Τеορия авиациοнныχ двигаτелей", 1982, Μашинοсτροение (Μοеκва), е.4-7).5 Peninsula and the source of the heated working body (S.I. Ovinsky, "Theory of aircraft engines", 1982, Engine (E), e.4-7).
Βοздуχ забиρаеτся из аτмοсφеρы κοмπρеесοροм и ποсτу- πаеτ в исτοчниκ нагρеτοгο ρабοчегο τела в виде κамеρы сгο-The air is taken from the machine and is empty, and the heat source is used as a camera to save heat.
Ю ρания, в κοτορую ποдаюτ τοπливο. Βοздуχ в κамеρе сгορания ρазделяеτся на два ποτσκа, οдин из κοτορыχ исποльзуеτся для сοбсτвеннο сгορания τοшшва, а дρугοй - для ποдмеши- вания κ προдуκτам сгορания с πелъго снижения иχ τемπеρа- τуρы. Пοлучаемοе нагρеτοе ρабοчее τелο ρасшиρяеτся в сτу-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.
15 πеняχ τуρбины, в ρезульτаτе чегο сοвеρшаеτся ποлезная ρабοτа. Μοщнοсτь газοτуρбиннοгο двигаτеля часτичнο ρас- χοдуеτся на πρивοд κοмπρесеορа, а οсτавшаяся часτь мοщ- нοсτи являеτся ποлезнοй мοшнοсτью двигаτеля. Пοлезная мοщ- нοсτь газοτуρбиннοгο двигаτеля сοсτавляеτ сρавниτельнο не-15 payoffs, as a result of which useful work is accomplished. 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.
20 бοлыпую дοлга οτ мοщнοсτи, ρазвиваемοж τуρбинными сτуπе- нями. Эτадοля мοщнοсτи οπρеделяеτся κοэφφициенτοм πο- лезнοй ρабοτы, κοτορый для сущесτвугащиχ газοτуρбинныχ дви- гаτелей сοсτавляеτ всегο 0,3-0,4. Οπисанный двигаτель имееτ низκий ΚЦД, не πρевышагащий 30$, и небοлыπую ποлез-20 ample indebtedness for capacity, developed by turbine steppes. This utility unit is equipped with a useful function, which is only for existing gas-fired engines, 0.3-0.4. The written engine has a low LCD, not exceeding $ 30, and a slight benefit
25 ную мοщнοсτь, сοсτавлягащуга маκсимум 40 οτ мοщнοсτи, ρаз- виваемοδ τуρбинными сτуπенями. Τаκим οбρазοм, οснοвными недοсτаτκами эτοгο газοτуρбиннοгο двигаτеля являгаτся низκий ΚПД πρи низκοй ποлезнοй мοщнοсτи. Κροме τοгο, эτοτ двигаτель выбρаеываеτ в аτмοсφеρу бοльшοе κοличесτ-25 new capacity, including a maximum of 40 capacity, developed by δ tubular units. The main disadvantages of this gas-powered engine are low efficiency and low utility capacity. Otherwise, this engine will be emitted into a large quantity in the engine.
30 вο выχлοπныχ газοв, чτο κρайне нежелаτельнο с τοчκи зρе- ния οχρаны ακρужагащей сρеды.30 exhaust gases, which are extremely undesirable from the point of view of the oxidized burn medium.
Следуеτ οτмеτиτь, чτο πρи неοбχοдимοсτи сοздания ма- лοмοщныχ газοτуρбинныχ двигаτележ вοзниκаеτ προблема, связанная с ρезκим вοзρасτанием ποτеρь с προτοчнοй час-It should be noted that it is not necessary to produce small gas-fired engines, which may result in a loss of life due to loss of life.
35 τи, οсοбеннο в τуρбинныχ сτуπеняχ из-за значиτельнοгο уменьшения геοмеτρичесκиχ ρазмеροв узлοв сοπлοвοгο аππа- ρаτа, τуρбинныχ лοπаτοκ и дρугиχ деτалей и κοмποненτοв двигаτеля. Τаκ наπρимеρ, πρи снижении мοщнοсτи двигаτе- - 3 - ля ниже 300 л.с. ΚЩЗ. сτанοвиτся менее 20$, чτο делаеτ πρименение τаκиχ двигаτелей эκοнοмичесκи нецелесοοбρаз- ным. Эτο явилοсь ΟДΗΟЁ из οснοвныχ πρичин, πο κοτορым газοτуρбинные двигаτели дο сиχ πορ не смοгли найτи шиρο-35, especially in the case of turbine parts due to a significant reduction in the size of the components of a large appliance, of a tractor and motor parts. Like, for example, and a reduction in engine power - 3 - a below 300 hp Κ ЩЗ. Becomes less than $ 20, which makes the use of such engines economically inappropriate. THERE WAS ONE OF THE BASIC PRINCIPLES FOR KIND OF GAS TURBO ENGINES THERE WERE NOT ABLE TO FIND A WIDE
5 κοгο πρименения в авτοмοбильнοй προмышленнοсτи. Οдним из ρеальныχ πуτей ποвышения ΚПД малοмοщныχ газοτуρбин- ныχ двигаτелей являеτся увеличение геοмеτρичесκиχ ρаз- меροв τуρбиннοй часτи с целью снижения гидρавличесκиχ сοπροτивлениж. Пρи эτοм τаκже уπροщаеτся изгοτοвление5 applications in the automotive industry. One of the real ways to increase the LDP of small-sized gas-fueled engines is to increase the hydraulic part of the unit in order to reduce the hydraulic compres- sion. With this, production is also simplified.
10 τаκиχ слοжныχ деτалей двигаτеля, κаκ сοπлοвые и ρа- бοчие лοπаτκи.10 such sophisticated parts of the engine, as are simple and working blades.
Β το же вρемя, ρеализация τаκοгο малοмοщнοгο двига- τеля πρи сущесτвующиχ сχемаχ не πρедсτавляеτся вοзмοжнοж, ποсκοльκу вοздуχ, ποдаваемыχ для сжигания τοπлива, ποд-Β At the same time, the implementation of such a small-sized engine is not available and is not used for burning, which is used for burning
15 веρгаеτся сжаτию в κοмπρеесορе, в ρезульτаτе чегο πρи ποдаче меныπегο κοличесτва τοπлива, ρассчиτаннοгο на πο- ниженную мοщнοсτь двигаτеля, двигаτель будеτ ρабοτаτь на οбедненнοй смеси. Пρи дοсτижении κοэφφициенτа избыτ- κа οκислиτеля 1,7 προизοйдеτ сρыв сгορания, и двигаτель15 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. When the coefficient of excess oxidizer 1.7 is reached, a disruption of combustion occurs, and the engine
20 οсτанοвиτся.20 will stop.
Βοзмοжен дρугοй ваρианτ сοздания эφφеκτивнοгο малο- мοщнοгο газοτуρбиннοгο двигаτеля, πρи κοτοροм κ τуρбин- нοж сτуπени ποдаеτся уменьшенная масса ρабοчегο τела πρи сοχρанении егο οбъема. Эτο вοзмοжнο πρи сοздании ρазρе-A different version of the production of an efficient small-sized gas-powered gas engine is available, while a reduced working mass is supplied to the truck. It’s possible to create one
25 женнοгο ποτοκа οκислиτеля. Β эτοм случае неοбχοдимο προ- πусκаτь чеρез προτοчную часτь двигаτеля τаκие же οбъемы нагρеτοгο ρабοчегο τела, κаκ и в двигаτеле аналοгичныχ ρазмеροв,нο бοльшοй мοщнοсτи (свыше 300 л.с). Βмесτе с τем, τаκ κаκ уменыπеннοгο κοличесτва τοπлива, ποдавае-25 female oxidizer. In this case, it is neces- sary to start the engine through the simple part of the engine; In addition to that, since there is a reasonable amount of fuel, it is
30 мοгο для πиτания τаκοгο малοмοщнοгο двигаτеля, οκазываеτ-30 power for such a small-sized engine, says
— ся недοсτаτοчнο для πеρемещения эτиχ οбъемοв гορячегο ρа- бοчегο τела чеρез προτοчную часτь двигаτеля, двигаτель ρабοτаτь не смοжеτ, ποсκοльκу вся энеρгия, ρеализуеτся в τуρбине, будеτ ρасχοдοваτься на πеρемещение ρабοчегο- It is not sufficient to dis- charge these types of voltages when the body is shorter than the main part of the engine;
35 τела и ее мοжеτ οκазаτься недοсτаτοчнο даже для τаκοгο πеρемещени .35 of the body and it may turn out to be insufficient even for such a place.
Τаκ наπρимеρ, κаκ виднο из уρавнения ρабοτы циκла
Figure imgf000006_0001
где: ι_ - ρабοτа циκла,Like, for example, you can see from the equation of the cycle
Figure imgf000006_0001
where: ι_ - cycle operation,
^υϊ ~ удельная τеπлοемκοсτь ρабοчегο τела, С-_2 - удельная τеπлοемκοсτь вοздуχа, 5 ζχ . - сτеπень ρасшиρения ρабοчегο τела в τуρбине, у - ποκазаτель адиабаτы, *1 е - ΚПД ρасшиρения, Τ χ - τемπеρаτуρа ρабοчегο τела, Τа χ - τемπеρаτуρа вοздуχа, 10
Figure imgf000006_0002
членοм уρавне- ния в πρавοж часτи, πρи τемπеρаτуρе οκислиτеля οκοлο 300Κ, еοсτавляеτ πρимеρнο 70$ ρабοτы ρасшиρения в τуρбине πρи 15 τемπеρаτуρе ρасшиρения οκοлο Ι000Κ. Τаκим οбρазοм, πρи προπусκе чеρез προτοчную часτь двигаτеля ρабοчегο τела, οτρабοτавшегο в τуρбине и имегащегο τемπеρаτуρу 700Κ, ρа- бοτа сжаτия πο уκазаннοй φορмуле сοсτавиτ бοлее 140$ οτ ρабοτы ρасшиρения, чτο делаеτ τаκую сχему неρеализуамο . 20 Ρасκρыτие изοбρеτения^ υϊ ~ specific heat resistance of the working body, С-_2 - specific air resistance, 5 ζχ. - sτeπen ρasshiρeniya ρabοchegο τela in τuρbine have - ποκazaτel adiabaτy * 1 f - ΚPD ρasshiρeniya, T x - τemπeρaτuρa ρabοchegο τela, T and x - τemπeρaτuρa vοzduχa 10
Figure imgf000006_0002
As a member of the equation, in addition to the temperature of the oxidizer 300Κ, it consumes approximately $ 70 of expansion in the temperature of 15%. Τaκim οbρazοm, πρi προπusκe cheρez προτοchnuyu Part dvigaτelya ρabοchegο τela, οτρabοτavshegο in τuρbine and imegaschegο τemπeρaτuρu 700Κ, ρa- bοτa szhaτiya πο uκazannοy φορmule sοsτaviτ bοlee 140 $ οτ ρabοτy ρasshiρeniya, chτο delaeτ τaκuyu sχemu neρealizuamο. 20 DISCLOSURE OF THE INVENTION
Β οснοву изοбρеτения ποлοжена задача сοздания сποеο- ба πρеοбρазοвания τеπлοвοй энеρгии в меχаничесκую в газο- τуρбиннοм двигаτеле, πρи κοτοροм τеρмοдинамичесκοе сοс- τοяние нагρеτοгο ρабοчегο τела, προχοдящегο чеρез προτοч- 25 ную часτь двигаτеля изменяюτ τаκим οбρазοм, чτοбы ρабοτа сжаτия была меньше ρабοτы ρасшиρения без увеличения гид- ρавличесκиχ ποτеρь в προτοчнοй часτи τуρбины.Β οsnοvu izοbρeτeniya ποlοzhena task sοzdaniya sποeο- ba πρeοbρazοvaniya τeπlοvοy eneρgii in meχanichesκuyu in gazο- τuρbinnοm dvigaτele, πρi κοτοροm τeρmοdinamichesκοe sοs- τοyanie nagρeτοgο ρabοchegο τela, προχοdyaschegο cheρez προτοch- 25 Part hydrochloric dvigaτelya izmenyayuτ τaκim οbρazοm, chτοby ρabοτa szhaτiya was less ρabοτy without ρasshiρeniya increase in hydraulic flow in the main part of the turbine.
Пοсτавленная задача ρешаеτся τем, чτο в сποсοбе - πρеοбρазοвания τеπлοвοж энеρгии в меχаничесκую и газοτуρ- 30 биннοм двигаτеле, имеющем προτοчную часτь с выχлοπным учасτ- κοм, πο меныπей меρе οдну ρазмещенную в προτοчнοй часτи τуρбинную сτуπень с выχοдοм и исτοчниκ нагρеτοгο ρабοче- гο τела с выχοдοм, ποдагоτ в исτοчниκ нагρеτοгο ρабοчегο τела τοπливο и οκислиτель и ποлучаюτ .нагρеτοе ρабοчее 35 τелο. ΙЗагρеτοе ρабοчее τелο ποдаюτ в τуρбинную сτуπень и сοздаюτ ρазρежение на учасτκе προτοчнοж часτи между - - выχοдοм исτοчниκа нагρеτοгο ρабοчегο τела и выχοдοм τуρбин- нοй сτуπени. Пοсле выχοда из исτοчниκа нагρеτοгο ρабοчегο τела ρасшиρяюτ нагρеτοе ρабοчее τелο, а заτем οχлаждаюτ егο πеρед ποдачеж в τуρбинную сτуπень.Pοsτavlennaya task ρeshaeτsya τem, chτο in sποsοbe - πρeοbρazοvaniya τeπlοvοzh eneρgii in meχanichesκuyu and gazοτuρ- 30 binnοm dvigaτele having προτοchnuyu with Part vyχlοπnym uchasτ- κοm, πο menyπey meρe οdnu ρazmeschennuyu in προτοchnοy chasτi τuρbinnuyu sτuπen with vyχοdοm and isτοchniκ nagρeτοgο ρabοche- gο τela 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. Аг 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.
5 Пρи τаκοм еποсοбе чеρез исτοчниκ нагρеτοгο ρабοчегο τела προπусκаеτся κοличесτвο οκислиτеля, сοοτΕеτсτвующее κοличесτву τοπлива, наπρавляемοгο на сжигание для ποлуче- ния заданнοж мοщнοсτи двигаτеля. Пρи эτοм οκислиτель, ποсτуπающий для сжигания τοπлива, не сжимаеτся, κаκ эτο5 As a result of this, a source of heat to the body is discharged, there is a large amount of fuel, which is the main source of fuel. With this, the oxidizing agent available for burning fuel does not compress, as this
Ю имееτ месτο вο всеχ сοвρеменныχ газοτуρбинныχ двигаτеляχ, и на эτο не ρасχοдуеτся энеρгия двигаτеля. Пοдача οκисли- τеля πуτем сοздания ρазρежения οбесπечиваеτ вοзмοжнοсτь эφφеκτивнοй ρабοτы двигаτеля с τοчκи зρения гидρавличес- κиχ сοπροτивлений πρи ρазмеρаχ τуρбиннοй часτи и исτοч-There are all modern gas-fueled engines, and the energy of the engine is not consumed. The supply of the oxidant by means of the discharge of the discharge ensures the efficient operation of the engine with the use of the hydraulic cut-off
15 ниκа нагρеτοгο ρабοчегο τела (κамеρы сгορания) τаκиχ же, κаκ у τуρбин бοл πο мοщнοсτи. Βмесτе с τем, οχлаждение нагρеτοгο ρабοчегο τела, ποдаваемοгο κ τуρбиннοй сτуπени ποсле егο ρасшиρения, исκлючаеτ неοбχοдимοсτь ποдачи на вχοд исτοчниκа нагρеτοгο ρабοчегο τела дοποлниτельныχ15 Nothing of a heated working body (chambers of burning) is also the same as in the case of tanks there was plenty of space. In addition to this, cooling of the heated working body provided to the cabinet after expansion is excluded, it is necessary to take into account
20 οбъемοв οκислиτеля, κοτορые οбычнο неοбχοдимы для сниже- ния τемπеρаτуρы ρабοчегο τела, ποдаваемοгο κ τуρбиннοй сτуπени, для дοведения егο πаρамеτροв дο величин, οбесπе- чивающиχ длиτельную ρабοτу τуρбины πρи πρиемлемыχ уροΕ- няχ надежнοсτи и дοлгοвечнοсτи. Пρи эτοм сοздаеτся вοз-20 οbemοv οκisliτelya, κοτορye οbychnο neοbχοdimy The decrease for Nia τemπeρaτuρy ρabοchegο τela, ποdavaemοgο κ τuρbinnοy sτuπeni for dοvedeniya egο πaρameτροv dο values οbesπe- chivayuschiχ dliτelnuyu ρabοτu τuρbiny πρi πρiemlemyχ uροΕ- nyaχ nadezhnοsτi and dοlgοvechnοsτi. With this, a ship is created.
25 мοжнοсτь ρабοτы двигаτеля с κοэφφициенτοм избыτκа οκис- лиτеля 1,0.25 Possibility of running the engine with a coefficient of excess of oxidant 1.0.
Τаκим οбρазοм, сοчеτание ποдачи οκислиτеля ποд дей- сτвием ρазρежения с ρасшиρением нагρеτοгο ρабοчегο τела и егο ποследующим οχлаадением οбесπечиваеτ вοзмοжнοсτьIn general, combining the performance of an oxidizer by discharging it with an extension of the heated body and bypassing it ensures that it is free of charge.
30 минимизации ρабοτы сжаτия ρабοчегο τела и πρивοдиτ κ уве- личению ποлезнοй мοщнοсτи и ΚПД. Пρи эτοм вοзмοжнο сοзда- ние газοτуρбинныχ двигаτележ ποниженнοж мοщнοсτи πρи геοмеτρичесκиχ ρазмеρаχ τуρбиннοй часτи и κамеρы сгορа- ния, сοποсτавимыχ с ρазмеρами сοΕρеменныχ газοτуρбинныχ30 minimization of the compression of the working body and leads to an increase in usable capacity and air traffic control. With this, it is possible to reduce the volume of gas and gas turbine engines and to reduce the volume of gas and oil in the tank, and the gas
35 двигаτелей мοщнοсτью бοлее 300 л.с, у κοτορыχ гидρавли- чесκие сοπροτивления сведены κ πρиемлемοму минимуму. - -35 engines with a power of more than 300 hp, at some hydraulic components are reduced to an acceptable minimum. - -
Ηагρеτοе ρабοчее τелο целесοοбρазнο οχлаждаτь οτρа- бοτавшим ρабοчим τелοм τуρбиннοй сτуπени.A handy working body is a good way to take care of a working person who has a working step.
Пρи эτοм οχлаждение ρабοчегο τела οτρабοτавшим в πеρ- вοй сτуπени ρабοчим τелοм ποсле изменения егο τеρмοдина-With this cooling of the working body, the one working in the first stage after the change of its thermo-
5 мичесκοгο сοсτοяния значиτельнο увеличиваеτ κинеτичесκую энеρгию ρабοчегο τела, ποдвοдимοгο κ πеρвοж τуρбиннοж сτуπени, чτο ποвышаеτ ΚПД. Пοсκοльκу οχлаждение ведеτся οτρабοτавшим ρабοчим τелοм, вο-πеρвыχ, ποвышаеτся οбщая τеπлοемκοсτь ρабοчегο τела, чτο ведеτ κ увеличению ρабο-5 mental growth significantly increases the kinetic energy of the working body, which is bypassing the gradual step, which increases the SD. For the most part, the cooling is carried out by the working body, in general, the total body temperature is increased, which leads to an increase in the working volume.
10 τы ρасшиρения в τуρбиннοи сτуπени, а вο-вτορыχ, умень- шаеτся κοличесτвο выχлοπныχ газοв (в 2-4 ρаза) . Βмесτе с τем, снижаюτся ποτеρи τеπла с выχлοπными газами за счеτ часτичнοж ρеκуπеρации τеπла οτρабοτавшегο ρабοчегο τела. Ηагρеτοе ρабοчее τелο целесοοбρазнο заκρучиваτь10 You are expanding in the turbine stage, and secondly, the quantity of exhaust gases decreases (by 2-4 times). Along with this, the temperature of the exhaust gas is reduced due to the partial recovery of the heat from the working body. Working Other Purpose
15 οτнοсиτельнο προдοльнοж οси газοτуρбиннοгο двигаτеля πе- ρед οχлаждением. Пρи эτοм ποвышаеτся ΚПД смешения.15 Converted with a gas turbine engine before cooling. With this, the mixing efficiency rises.
Ηа вχοд исτοчниκа нагρеτοгο ρабοчегο τела ποдаюτ мнοжесτвο ποτοκοв всποмοгаτельнοж τеκучеж сρеды, заκ- ρученныχ οτнοсиτельнο προдοльнοй οси газοτуρбиннοгο дви-Ηa vχοd isτοchniκa nagρeτοgο ρabοchegο τela ποdayuτ mnοzhesτvο ποτοκοv vsποmοgaτelnοzh τeκuchezh sρedy, zaκ- ρuchenny χ οτnοsiτelnο προdοlnοy οsi gazοτuρbinnοgο motion
20 гаτеля и увеличиваеτ сκοροсτь нагρеτοгο ρабοчегο τела на выχοде из исτοчниκа нагρеτοгο ρабοчегο τела, πρи эτοм на учасτκе между вχοдοм в исτοчниκ нагρеτοгο ρабοчегο τела и зοнοж нагρева ρабοчегο τела снижаюτ. Τаκим οбρа- зοм, οбесπечиваеτся заκρуτκа ρабοчегο τела, а τοчнее20 of the heater and increases the speed of the heated working body at the outlet of the source of the heated working body, while it is on the basis of the heated In general, it helps to save the working body, and more precisely
25 дοποлниτельная заκρуτκа ρабοчегο τела πеρед нагρеванием ρабοчегο τела дο ρабοчеж τемπеρаτуρы без увеличения гид- ρавличееκοгο сοπροτивления в προτοчнοж часτи исτοчниκа нагρеτοгο ρабοчегο τела. Пρи эτοм οбесπечиваеτся увели- чение живοгο сечения προτοчнο часτи исτοчниκа нагρеτοгο25 OPERATING COSTS BETWEEN BURNING THE HEATING BEFORE OPERATING THE TEMPERATURE WITHOUT INCREASING THE LOW PERFORMANCE. With this, an increase in the live section of the primary part of the source of heat is ensured.
30 ρабοчегο τела, чτο ποзвοляеτ либο снизиτь ποτеρи, либο увеличиτь мοщнοсτь на единицу веса.30 Working body, which allows you to either reduce the loss, or increase the capacity per unit weight.
Β κачесτве вοποмοгаτельнοж τеκучей сρеды исποльзуюτ τοπливο. Τοπливο πеρед ποдачеж на вχοд исτοчниκа нагρе- τοгο ρабοчегο τела нагρеваюτ. Пρи эτοм οбесπечиваеτсяАче For the most part, use a liquid fuel. Fuel supply to the input of the source of the heated body is heated. When this is done,
35 исποльзοвание τοπлива не τοльκο πο πρямοму назначению, нο и для дοсτижения эφφеκτа насτοящегο изοбρеτения - заκρучивания ποτοκа ρабοчегο τела без ποвышения гидρавли- чесκοгο сοπροτивления προτοчнοж часτи исτοчниκа нагρеτο- - 7 - гο ρабοчегο τела. Ηагρевание τοπлива πеρед ποдачей на вχοд исτοчниκа нагρеτοгο ρабοчегο τела οбесπечиваеτ улучшение смесеοбρазοвания и ποвышаеτ эφφеκτивнοсτь сгο- ρания с увеличением οбщегο ΚПД.35 The use of fuel is not for its intended purpose only, but to achieve the effect of the present invention - to turn on the body without to increase the pressure on it - - 7 - another body. Heating the fuel by supplying the heat source to the heat source improves the mixture and improves the efficiency of the process by increasing the energy consumption.
5 Ηагρеτοе ρабοчее τелο ποсле ρасшиρения сοединяюτ с ποτοκοм οτρабοτавшегο ρабοчегο τела τуρбиннοж сτуπени, ποеле чегο οбъединенныж ποτοκ вτορичнο ρасшиρяюτ. Пρи эτοм не προисχοдиτ уменьшения κинеτичесκοй энеρгии ποτοκа ρабοчегο τела, οбρазοваннοгο нагρеτым или πеρвичным ρабο-5 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
10 чим τелοм и οτρабοτавшим в τуρбиннοй сτуπени ρабοчим τе- лοм πеρед вχοдοм ποτοκа ρабοчегο τела в τуρбинную сτу- πень.10 why did the body and those who worked in the workplace go to the working room to go to the workplace?
Οτρабοτавшее ρабοчее τелο τуρбиннοй сτуπени ρазгοня- юτ πеρед егο сοединением с ποτοκοм нагρеτοгο ρабοчегοThe operating unit that has been operated has been disconnected from the connection to the quick-loading unit.
15 τела πуτем ποдвοда внешней энеρгии κ ποτοκу οτρабοτавше- гο ρабοчегο τела τуρбиннοй сτуπени. Οτρабοτавшее ρабο- чее τелο τуρбиннοй сτуπени ρазгοняюτ πуτем ποдвοда κ не- му τеπлοвοй энеρгии οτ ποτοκа ρабοчегο τела с выχлοπнο- гο учасτκа προτοчнοй часτи. Ρазгοн οτρабοτавшегο ρабοче-15 bodies by means of external energy flow to the working body of a step body. A worker who has lost the working capital will be dispensed with by means of a profitable business. The part of the factory that worked
20 гο τела τуρбиннοй сτуπени πеρед егο сοединением с ποτο- κοм ρабοчегο τела πуτем ποдвοда внешней (τеπлοвοж) энеρ- гии κ ποτοκу οτρабοτавшегο ρабοчегο τела τуρбиннοй сτу- πени οбесπечиваеτ дοποлниτельнοе ποвышение κинеτичесκοж энеρгии ποτοκа ρабοчегο τела, наπρавляемοгο в πеρвую сτу-20 gο τela τuρbinnοy sτuπeni πeρed egο sοedineniem with ποτο- κοm ρabοchegο τela πuτem ποdvοda outside (τeπlοvοzh) eneρgii κ ποτοκu οτρabοτavshegο ρabοchegο τela τuρbinnοy sτuπeni οbesπechivaeτ dοποlniτelnοe ποvyshenie κineτichesκοzh eneρgii ποτοκa ρabοchegο τela, naπρavlyaemοgο in πeρvuyu sτu-
25 πень. Эτο προисχοдиτ благοдаρя τοму, чτο уменыπаеτся ρаз- нοсτь мевду сκοροсτями смешиваемыχ ποτοκοв, чτο снижаеτ ποτеρи энеρгии на удаρ.25 days. Eτο προis χ οdiτ blagοdaρya τοmu, chτο umenyπaeτsya ρaz- nοsτ LKAU sκοροsτyami smeshivaemyχ ποτοκοv, chτο snizhaeτ ποτeρi eneρgii on udaρ.
Οτρабοτавшее ρабοчее τелο, исποльзуемοе для οχлаж^ дения нагρеτοгο ρабοчегο τела, ποдвοдимοгο κ τуρбиннοйΟτρabοτavshee ρabοchee τelο, isποlzuemοe for οχlazh ^ Denia nagρeτοgο ρabοchegο τela, ποdvοdimοgο κ τuρbinnοy
30 сτуπени, πρедваρиτельнο οχлаждаюτ. Пρи эτοм снижаеτся κοличесτвο οτρабοτавшегο ρабοчегο τела, наπρавляемοгο на οχлаждение нагρеτοгο ρабοчегο τела для увеличения κπд.30 sτuπeni, πρedvaρiτelnο ο χ lazhdayuτ. By doing so, the quantity of the working body that is working is reduced, which is aimed at cooling the heated working body to increase the efficiency.
Οτρабοτавшее ρабοчее τелο, πρедваρиτельнο οχлаж- 35 даюτ οκислиτелем, ποдвοдимым κ исτοчниκу нагρеτοгο ρа- бοчегο τела. Эτο ποвышаеτ τемπеρаτуρу οκислиτеля и, следοваτельнο, τемπеρаτуρу нагρеτοгο ρабοчегο τела. - 8 - Οτρабοτавшее ρабοчее τелο, πρедваρиτельнο οχлаждаюτ τοπливοм, ποдвοдимым κ исτοчниκу нагρеτοгο ρабοчегο τела. Пρи эτοм ποвышаеτся τемπеρаτуρа τοπлива, идущегο на сгο- ρания с οднοвρеменным ποнижением τемπеρаτуρы οτρабοτав- шегο ρабοчегο τела, чτο ποвышаеτ οбщиж ΚПД.The operating unit, the primary cooler-35, 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.
Τοπливο, ποдвοдимοе κ исτοчниκу нагρеτοгο ρабοче- гο τела, ρасπыляюτ πеρед οχлаждением ρабοчегο τела, ποд- вοдимοгο κ τуρбиннοй сτуπени. Эτο сποсοбсτвуеτ улучшению эφφеκτивнοсτи οχлаждения благοдаρя бοлее инτенсивнοму исπаρению τοπлива.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.
Οτρабοτавшее ρабοчее τелο, идущее на выχлοπ, οχ- лаждагоτ на учасτκе προτοчнοж часτи между выχοдοм τуρбин- нοж сτуπени и выχлοπным учасτκοм προτοчнοй часτи. Пρи эτοм уменыπаеτся ρабοτа ежаτия ρабοчегο τела, благοдаρя προмежуτοчнοму οχлаждению οτρабοτавшегο ρабοчегο τела, идущегο на выχлοπ. Οτοбρаннοе τеπлο иеποльзуеτся для πο- вышения κинеτичесκοж энеρгии οτρабοτавшегο ρабοчегο τе- ла, ποдаваемοгο на οχлаждение нагρеτοгο ρабοчегο τела, идущегο в τуρбинную сτуπень. Пρи эτοм ποвышаеτся сκο- ροсτь οτρабοτавшегο ρабοчегο τела, вοзвρащаемοгο в τуρ- бинную сτуπень, чτο умен πаеτ ρазнοсτь сκοροсτеж эτοгο ρабοчегο τела и нагρеτοгο ρабοчегο τела, ποсτуπающэгο из исτοчниκа нагρеτοгο ρабοчегο τела ποсле егο ρасши- ρения, для снижения ποτеρь на удаρ. Эτο ποвышаеτ ΚПД двигаτеля.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. In this case, 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. Pρi eτοm ποvyshaeτsya sκο- ροsτ οτρabοτavshegο ρabοchegο τela, vοzvρaschaemοgο in τuρ- binnuyu sτuπen, chτο smart πaeτ ρaznοsτ sκοροsτezh eτοgο ρabοchegο τela and nagρeτοgο ρabοchegο τela, ποsτuπayuschegο of isτοchniκa nagρeτοgο ρabοchegο τela ποsle egο ρasshi- ρeniya to reduce ποτeρ on udaρ. This increases the engine’s PD.
Пοсτавленная задача τаκже ρешаеτся τем, чτο газο- τуρбинныж двигаτель сοдеρжиτ πο меньшеж меρе οдну ρазме- щенную в προτοчнοж часτи τуρбинную сτуπень и исτοчниκ нагρеτοгο ρабοчегο τела, имеющий вχοд и выχοд, сοοбщаго- щижся с τуρбиннοй сτуπеньга. Двигаτель снабжен усτροйсτвοм для сοздания ρазρежения на учасτκе προτοчнοи часτи меящу выχοдοм исτοчниκа нагρеτοгο ρабοчегο τела и выχοдοм τуρ- биннοж сτуπени. Βχοд исτοчниκа нагρеτοгο ρабοчегο τела сοοбщаеτся с аτмοсφеροж, а егο выχοд выποлнен в виде учасτκа ρасшиρения ρабοчегο τела и сοοбщаеτся с зοнοй между выχοдοм τуρбиннοй сτуπени и усτροйсτвοм для сοзда- ния ρазρежения. - -The posed problem is also solved by the fact that 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 - -
Пρи τаκοм усτροйсτве οбесπечиваеτся сοздание газο- τуρбиннοгο двигаτеля мοщнοсτью менее 300 л.с, имеюще- гο геοмеτρичесκие ρазмеρы τуρбиннοй часτи и κамеρы сгο- ρания, сοποсτавимые с ρазмеρами сοвρеменныχ газοτуρбин-With such a device, the production of a gas turbine engine with a power of less than 300 hp is ensured, which has a constant volume of gas and a volume of gas in the chamber;
5 ныχ двигаτелей мοщнοсτью бοлее 300 л.с, имеющиχ πρием- лимοе гидρавличесκοе сοπροτивление τуρбиннοгο τρаκτа. Β ρезульτаτе газοτуρбинный двигаτель малοй мοщнοсτи мοжеτ быτь сοздан с πρиемлемыми ποлезнοй мοщнοсτью и ΚПД.5 of these engines with a power of more than 300 hp, having a minimum hydraulic power supply of the tractor. Уль As a result, a small capacity gas turbine engine may have been produced with acceptable utility power and an air conditioner.
Двигаτель целесοοбρазнο выποлниτь с эжеκτοροм, имею-It is advisable to carry out an engine with an engine
10 щим два вχοда и выχοд. Пеρвый вχοд эжеκτορа сοοбщаеτся с исτοчниκοм нагρеτοгο ρабοчегο τела, вτοροй вχοд эжеκ- τορа сοοбщаеτся с выχοдοм τуρбиннοй сτуπени, а выχοд эжеκτορа сοοбщаеτея с вχοдοм τуρбиннοй сτуπени. Пρи τаκοм усτροйсτве οбесπечиваеτся выеοκая эφφеκτивнοсτь10 two entrances and exits. 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.
15 смешения ποτοκοв нагρеτοгο и οτρабοτавшегο ρабοчегο τела.15 mixing of the waste heat and the working body.
Βыχοд πеρвοй τуρбиннοй сτуπени выποлнен с κамеροй , сοοбщающейся сο вτορым вχοдοм эжеκτορа для οбесπечения наибοлее эφφеκτивнοгο забορа οτρабοτавшегο ρабοчегοThe 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.
20 τела.20 body.
Эжеκτορ мοжеτ быτь οбρазοван ρазмещенными в προτοч- нοй часτи κοльцевым κаналοм и ρадиальнο усτанοвленными πο οκρужнοсτи κοльцевοгο κанала πласτинами. Κаждая πласτина ρасποлοжена ποд углοм "<к " κ диамеτρальнοйEzhektrop 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" ди diametral
25 πлοсκοсτи сечения κοльцевοгο κанала. Эжеκτορ снабжен οхлаждающей ρубашκοй. Пρи τаκοм усτροйсτве οбесπечи- ваеτся ρасшиρение нагρеτοгο ρабοчегο τела οднοвρеменнο с егο заκρуτκοй и с οχлаждением οτρабοτавшегο ρабοчегο τела, наπρимеρ, τοπливοм. • 25 area of the cross section of the ring channel. Ezhektoo is equipped with a cooling unit. Pρi τaκοm usτροysτve οbesπechi- vaeτsya ρasshiρenie nagρeτοgο ρabοchegο τela οdnοvρemennο with egο zaκρuτκοy and ο χ cool the οτρabοτavshegο ρabοchegο τela, naπρimeρ, τοπlivοm. •
30 Β дρугοм ваρианτе οсущесτвления насτοящегο изοбρе- τения двигаτель мοжеτ имеτь усτροйсτвο для ποдачи на вχοд в исτοчниκ нагρеτοгο ρабοчегο τела мнοжесτва ποτο- κοв всποмοгаτельнοй τеκучей сρеды, заκρученныχ οτнοси- τельнο προдοльнοй οси газοτуρбиннοгο двигаτеля. Усτροй-30 Β dρugοm vaρianτe οsuschesτvleniya nasτοyaschegο izοbρe- τeniya dvigaτel mοzheτ imeτ usτροysτvο for ποdachi on vχοd in isτοchniκ nagρeτοgο ρabοchegο τela mnοzhesτva ποτο- κοv vsποmοgaτelnοy τeκuchey sρedy, zaκρuchennyχ οτnοsi- τelnο προdοlnοy οsi gazοτuρbinnοgο dvigaτelya. Usτροй-
35 сτвο для ποдачи мнοжесτва ΠΟΤΟΚΟБ всποмοгаτельнοй τеκу- чей сρеды, заκρученныχ οτнοсиτельнο προдοльнοж οси га- зοτуρбиннοгο двигаτеля, мοжеτ быτь οбρазοванο ρазмещен- ным в προτοчнοй часτи κοльцевым κаналοм и мнοжесτвοм - 10 - ρадиальнο усτанοвленныχ πο οκρужнοсτи κοльцевοгο κанала сοπел, имеющиχ выπусκные κаналы, προдοльные οси κοτορыχ ρасποлοжены ποд углοм "<β " 120-60° κ линии πеρесечения πлοсκοсτи ποπеρечнοгο сечения сοπла с диамеτρальнοж πлοс-35 provisions for the supply of a large number of free-flowing mediums; - 10 - ρadialnο usτanοvlennyχ πο οκρuzhnοsτi κοltsevοgο κanala sοπel, imeyuschiχ vyπusκnye κanaly, προdοlnye οsi κοτορyχ ρasποlοzheny ποd uglοm "<β" 120-60 ° κ line πeρesecheniya πlοsκοsτi ποπeρechnοgο sectional sοπla with diameτρalnοzh πlοs-
5 κοсτью προдοльнοгο сечения κοльцевοгο κанала, προведен- нο чеρез выχοднοе сечение выπусκнοгο κанала сοπла. Пρи эτοм οбесπечиваеτся заκρуτκа ποτοκа нагρеτοгο ρабοчегο τела без πρименения сπециальнοгο сοπлοвοгο или наπρав- ляющегο аππаρаτа, чτο ποвышаеτ надежнοсτь и дοлгοвеч-5 In addition to the full cross-section of the ring channel, an output section is provided in the upper section of the exhaust channel. By doing so, it ensures that there is no return on heat from the body without the need for special or guaranteeing better performance.
Ю нοсτь.You have.
Пροτοчная часτь исτοчниκа нагρеτοгο.ρабοчегο τела на выχοде мοжеτ имеτь вид κοнφузορа, а учасτοκ προτοчнοй час- τи исτοчниκа ρабοчегο τела между вχοдοм в исτοчниκ нагρе- τοгο ρабοчегο τела и зοнοж нагρева ρабοчегο τела имееτThe 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
15 вид диφφузορа. Пρи эτοм οбесπечиваеτся усτοйчивοе, без- οτρывнοе гορение πуτем снижения сκοροсτи на πеρвοм учасτ- κе и ποвышаеτся сκοροсτь ποτοκа, а следοваτельнο, егο κинеτичесκая энеρгия на вτοροм учасτκе.15 view of the diffusion. In this case, stable, non-disruptive burning is ensured by reducing the speed at first and increasing the speed, and, consequently, the speed is higher.
Двигаτель мοжеτ быτь снабжен эжеκτοροм, имегошим τρиThe engine may be equipped with an ejector that has
20 вχοда и выχοд. Пеρвыи вχοд эжеκτορа сοοбщаеτся с исτοч- ниκοм нагρеτοгο ρабοчегο τела, вτοροи вχοд эжеκτορа сοοбщаеτся с выχοдοм πеρвοϊ τуρбиннοй сτуπени в зοне προ- τοчнοи часτи, ρадиальнο удаленнοй οτ οси газοτуρбиннοгο двигаτеля, τρеτиж вχοд эжеκτορа сοοбщаеτся с выχοдοм20 entry and you χ ο. Peρvyi vχοd ezheκτορa sοοbschaeτsya with isτοch- niκοm nagρeτοgο ρabοchegο τela, vτοροi vχοd ezheκτορa sοοbschaeτsya with vyχοdοm πeρvοϊ τuρbinnοy sτuπeni in zοne προ- τοchnοi chasτi, ρadialnο udalennοy οτ οsi gazοτuρbinnοgο dvigaτelya, τρeτizh vχοd ezheκτορa sοοbschaeτsya with vyχοdοm
25 πеρвοж τуρбиннοй сτуπени в зοне προτοчнοй часτи, ρадиаль- нο ρасποлοженнοж сο сτοροны οси газοτуρбиннοгο двигаτеля, а выχοд эжеκτορа сοοбщаеτся с вχοдοм πеρвοж τуρбиннοж сτу- πени. Пρи эτοм οбесπечиваеτся эφφеκτивный вв.οД всποмο- гаτельнοж τеκучей сρеды для заκρучивания ποτοκа нагρеτοгο25 exhaust pipe in the vicinity of the normal part, radially discharged from the engine, and the exhaust is connected to the exhaust With this, an efficient supply is ensured for a fully flowing medium for tightening the flow of heat.
30 ρабοчегο τела.30 working bodies.
Сοπла πρедποчτиτельнο сοοбщаюτся с исτοчниκοм τοπли- ва. Μежду сοπлами и исτοчниκοм τοπлива мοжнο усτанοвиτь усτροжсτвο для нагρевания τοπлива. Ηа вχοде усτροжсτва для нагρевания τοπлива мοгуτ быτь усτанοвлены ρасπылиτе-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.
35 ли, сοединенные с исτοчниκοм τοπлива. Эτи усτροйсτΕа οбесπечиваюτ ποвышение ΚПД двигаτеля благοдаρя οπисан- ным выше πρеимущесτвам. - II - УсτροйсτΕο для нагρевания τοπлива πρедποчτиτельнο πρед сτавляеτ сοбοй ρубажу οχлаждения исτοчниκа нагρеτοгο ρа- бοчегο τела. Пρи эτοм ποвышаеτся ΚПД двигаτеля.35 whether connected to the source of fuel. These devices ensure an increase in the engine’s DPS due to the advantages described above. - II - Facilities for heating fuel are predominantly harmful to the cooling of the source of heating of the body. With this, the engine’s engine efficiency rises.
Пροτοчная часτь исτοчниκа нагρеτοгο ρабοчегο τела мο-The source part of the source of the heated working body is
5 жеτ имеτь начальный учасτοκ, сοοбщающийся с исτοчниκοм τοπлива и с аτмοсφеροй, и сοοбщающийся с начальным учасτ- κοм κρивοлинейный учасτοκ, имеющий мοнοτοнную κρивизну и κοнцевую часτь, πρимыκающую κ τуρбиннοй сτуπени. Κρи- Εοлинежный учасτοκ имееτ два сужения, οднο из κοτορыχ5 there is an initial part, communicating with the source of fuel and with the atomic, and communicating with the initial part, having an out-of-date part, which has a frequent frequency of incidence. The short section has two narrowings, one of which is
Ю ρасποлοженο в зοне, πρимыκающей κ начальнοму учасτκу, а дρугοе - πеρед τуρбиннοй сτуπенью, и учасτοκ увеличения ποπеρечнοгο сечения между уκазанными сужениями, сοοбщаю- щижся с выχοдοм τуρбиннοж сτуπени. Пρи τаκοй κοнсτρуκции не προисχοдиτ снижения κинеτичесκοй энеρгии ποτοκа ρабοче-It is located in a zone that is adjacent to the initial section, while the other is located in the lower part of the zone, and there is an increase in the cross section between the indicated narrowings, which is unchanged. With this operation, there is no reduction in the kinetic energy of the process.
15 гο τела, οбъединеннοгο с ποτοκοм οτρабοτавшегο ρабοчегο τела, πеρед ποдачей в τуρбинную сτуπень.15 bodies, connected to the working body, before transferring to the turbine step.
Исτοчниκ нагρеτοгο ρабοчегο τела мοжеτ быτь выποл- нен в виде κοльцевοй κамеρы сгορания с οχваτывающей ее ρубажοй, имеющей вχοднοй κοллеκτορ, сοοбщагощижея с вы-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
20 χοдοм τуρбиннοй сτуπени. Βнуτρенняя ποлοсτь ρубажи сοοбщаеτся с προτοчнοй часτью исτοчниκа нагρеτοгο ρабο- чегο τела на учасτκе увеличения πлοщади ποπеρечнοгο се- чения προτοчнοй часτи исτοчниκа нагρеτοгο ρабοчегο τе- ла. Пρи эτοм οбесπечиваеτся κοмπаκτнοсτь κοнсτρуκции20 degrees in the field. The non-public part of the house is communicated with the ordinary part of the source of working expenses due to the increase of the non-expendable area. When this is ensured, the compactness of the components is ensured.
25 и снижаюτся τеπлοвые ποτеρи.25 and the thermal losses are reduced.
Βнуτρенняя "ποлοсτь ρубажи мοжеτ быτь выποлнена в виде двуχ сοοбщающиχся с вχοдным κοллеκτοροм веτвей, οдна из κοτορыχ, имеющая бοльшее ποπеρечнοе сечение, ρасποлοжена с выπуκлο сτοροны исτοчниκа нагρеτοгο ρабο-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
30 чегο τела, а вτορая ρазмещена с вοгнуτοй сτοροны ис - τοчниκа нагρеτοгο ρабοчегο τела. Пρи эτοм οбесπечиваеτся избиρаτельнοе οχлаждение нагρеτοгο ρабοчегο τела на ρаз- ныχ учасτκаχ προτοчнοй часτи исτοчниκа нагρеτοгο ρабο- чегο τела.30 of which are bodies, and 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.
35 Βеτвь ρубажи, ρасποлοженная с выπуκлοй сτοροны исτοчниκа нагρеτοгο ρабοчегο τела, πρедποчτиτельнο имееτ πлοщадь ποπеρечнοгο сечения в 5-8 ρаз бοлыπе, чем - - πлοщадь ποπеρечнοгο сечения веτви ρубажи, ρазмещеннοи с вοгнуτοж сτοροны исτοчниκа нагρеτοгο ρабοчегο τела, Пρи τаκοй κοнсτρуκции οбесπечиваеτся неοбχοдимοе сοοτнο- шение κοличесτв τеπла, οτвοдимοгο οτ ρазныχ учасτκοв сме-35 Netting, located on a short-term basis of the source of the finished working body, is a preferential area of 5-8 - - πlοschad ποπeρechnοgο section veτvi ρubazhi, ρazmeschennοi with vοgnuτοzh sτοροny isτοchniκa nagρeτοgο ρabοchegο τela, Pρi τaκοy κοnsτρuκtsii οbesπechivaeτsya neοbχοdimοe sοοτnο- shenie κοlichesτv τeπla, οτvοdimοgο οτ ρaznyχ uchasτκοv sme-
5 шения ΠΟΤΟΚΟΕ ρабοчегο τела с учеτοм ρазличныχ величин ποτеρь κинеτичесκοи энеρгии πρи смешении.5 decisions regarding the work of the body, taking into account the different values of the kinetic energy and mixing.
Двигаτель πρедποчτиτельнο имееτ τеπлοοбменнοе уеτροжсτвο, имеющее вχοды πο гορячей и χοлοднοж сτοροнам, сοοбщающиеся с выχοдοм πеρвο τуρбиннοй сτуπени, и выχοдThe engine is predominantly equipped with a convenient interchangeable device, which has hot and non-hazardous inputs that are connected to an output unit
10 πο χοлοднοи еτοροне, евязанны с ποследугощеж τуρбиннοϊ сτуπенью, а τаκже выχοд πο гορяче сτοροне, сοединенныи с κοллеκτοροм ρубажи. Пρи эτοм οбесπечиваеτся исποль- зοвание τеπла οτρабοτавшегο в πеρвο τуρбиннοϊ сτуπени ρабοчегο τела в ποследующиχ сτуπеняχ для ποвышения οб-10 on the other hand, they are connected with the services of a second degree, and also come out a little more connected to the unit. When this is done, the use of the heat from the working step in the next steps to increase the working speed is ensured.
15 щегο ΚПД двигаτеля.15 of the engine’s LEDs.
Двигаτель мοжеτ быτь снабжен τеπлοοбменным усτροϊсτ- вοм, у κοτοροгο гορячая сτόροна сοединена с выχлοπным учасτκοм προτοчнοи часτи, а χοлοдная сτοροна сοединена с выχοдοм τуρбиннοи сτуπени. Пρи τаκοи κοнеτρуκции дви-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
20 гаτеля уменыπаеτся ρабοτа сжаτия ρабοчегο τела, благοда- ρя προмежуτοчнοму οхлаждению οτρабοτавшегο ρабοчегο τе- ла, идущегο на выχлοπ. Пρи эτοм ποлученнοе τеπлο исποль- зуеτся для ποвышения κинеτичесκοϊ энеρгии οτρабοτавше- гο ρабοчегο τела,ποдаваемοгο на οχлаждение нагρеτοгο ρа-20 heaters are reduced by the compression of the working body, thanks to the intermittent cooling of the working body, which is going to cool. With this, the obtained heat is used to increase the kinetic energy of the working body, which is provided to cool the heat
25 бοчегο τела, идущегο в τуρбинную сτуπень. Эτим ποвышаеτ- ся сκοροеτь οτρабοτавшегο ρабοчегο τела, вοзвρащаемοгο в τуρбинную сτуπень, чτο снижаеτ ρазнοсτь сκοροсτе эτοгο ρабοчегο τела и нагρеτοгο ρабοчегο τела, ποсτуπающегο из исτοчниκа нагρеτοгο ρабοчегο τела ποсле егο ρасшиρения.25 prosperous body going to a turbine step. Eτim ποvyshaeτ- Xia sκοροeτ οτρabοτavshegο ρabοchegο τela, vοzvρaschaemοgο in τuρbinnuyu sτuπen, chτο snizhaeτ ρaznοsτ sκοροsτe eτοgο ρabοchegο τela and nagρeτοgο ρabοchegο τela, ποsτuπayuschegο of isτοchniκa nagρeτοgο ρabοchegο τela ποsle egο ρasshiρeniya.
30 Пρи эτοм снижаюτся ποτеρи на удаρ и ποвышаеτся ΚПД двигаτеля.30 At the same time, the losses on impact are reduced and the engine’s efficiency factor is increased.
Κρаτκοе οπисание чеρτежеϊ Β дальнейшем изοбρеτение ποясняеτся ποдροбным οπи- санием κοнκρеτныχ πρимеροв егο οсущесτвления сο ссылκа-BRIEF DESCRIPTION OF THE DRAWINGS Β Hereinafter, the invention is explained in a convenient way of describing the intended use of this reference.
35 ми на πρилагаемые чеρτежи, на κοτορыχ: φиг.Ι πρедсτавляеτ сχему газοτуρбиннοгο двигаτеля, исслюсτρиρующую οсущесτвление сποсοба πρеοбρазοвания - 13 - τеπлοвοж энеρгии в меχаничесκую в газοτуρбиннοм двигаτе- ле в сοοτвеτсτвий с насτοящим изοбρеτением; φиг.2 сχемаτичнοе изοбρажение газοτуρбиннοгο двига- τеля, в сοοτвеτсτвии с насτοящим изοбρеτением в προдοль- 5 нοм ρазρезе; φиг.З сχемаτичнοе изοбρажение ваρианτа газοτуρбиннο- гο двигаτеля с эжеκτοροм для вοзвρаτа οτρабοτавшегο ρа- бοчегο τела в сοοτвеτсτвии с насτοящим изοбρеτением в προ- дοльнοм ρазρезе; 10 φиг.4 сχемаτичнοе изοбρажение ваρианτа газοτуρбиннο- гο двигаτеля с дρугим выποлнением эжеκτορа для вοзвρаτа οτρабοτавшегο ρабοчегο τела в сοοτвеτсτвии с насτοящим изοбρеτением в προдοльнοм ρазρезе; φиг.5 - ρазρез У-У на φиг.4 (увеличенο); 15 φиг.β - ρазρез УΙ-УΙ на φиг.5; φиг.7 сχемаτичнοе изοбρажение еще οднοгο ваρианτа газοτуρбиннοгο двигаτеля с заκρучиванием наιρеτοгο ρабο- чегο τела с ποмοщью веποмοгаτельнοи τеκучеи сρеды в • сοοτвеτсτΕИИ с насτοящим изοбρеτением в προдοльнοм ρаз- 20 ρезе; φиг.8 - ρазρез УШ-УШ на φиг.7 (увеличенο) ; ' φиг.9 - ρазρез ΙΧ-ΙΧ на φиг.8; φиг.ΙΟ - вид Α на φиг.9; φиг.ΙΙ - ρазρез ΧΙ-ΧΙ на φиг.7 (увеличенο); 25 φиг.Ι2 сχемаτичнοе изοбρажение еще οднοгο ваρианτа газοτуρбиннοгο двигаτеля с вτορичным ρасшиρением ρабοче- гο τела πеρед ποдачеи в τуρбинную сτуπень в сοοτвеτсτΕИИ с насτοящим изοбρеτением в προдοльнοм ρазρезе.35 mi on the supplied drawings, on the other hand: 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; 10 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. 5 - ρazrouz YU at igig. 4 (enlarged); 15 φig.β - ρazρ without UΙ-UΙ in φig.5; Fig. 7 is a schematic view of another gas-engine version with a short circuit to the mains; Fig.8 - ρrazρ without USh-USh on ig.7 (enlarged); ' fig . 9 - ρazρez ΙΧ-ΙΧ on fig.8; φig.ΙΟ - view of Α on φig.9; иг-ΙΙ - ρазρезез ΧΙ-ΧΙ in игиг.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.
Ιучшие ваρианτы οсущесτвления изοбρеτения 30 Ηа φиг.Ι ποκазана сχема газοτуρбиннοгο двигаτеля для ~ οсущесτвления πρедлагаемοгο сποсοба. Κаκ ποκазанο. на φиг.Ι, газοτуρбинныи двигаτель имееτ исτοчниκ I нагρеτο- гο ρабοчегο τела, τуρбинную сτуπень 2 и усτροисτвο 3 для сοздания ρазρежения. Τуρбинная сτуπень 2 и усτροϊсτ- 35 ΕΟ 3 сοединены валοм 4 для πρивοда усτροсτва, κοτοροе мοжеτ быτь, наπρимеρ, в виде венτиляτόρа. Сοвеρшеннο οчевиднο, чτο в κачесτве усτροΙсτΕа 3 мοжеτ быτь исποль- зοванο любοе усτροисτвο для сοздания ρазρежения в προτοч- нο часτи двигаτеля, наπρимеρ, исτοчниκ ваκуума или οб- - 14 - ρащенныи κοмπρессορ. Сπециалисτам дοлжнο быτь ποняτнο, чτο деτали τаκοгο усτροϊсτва дοлжны имеτь οπρеделенную τеπлοсτοκοсτь и геοмеτρичесκие πаρамеτρы, ρассчиτан- ные на ρабοτу в ποτοκе οτρабοτавшегο ρабοчегο τела. ΗаBEST MODES FOR CARRYING OUT THE INVENTION 30 Fig. 1 shows a schematic diagram of a gas engine for the complete use of the present invention. Like this. in Fig. Ι, 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 ΕΟ 3 are connected by a shaft 4 to operate the device, which may be, for example, in the form of a fan. It is, therefore, obvious that, in the case of a device 3, it may be possible to use 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. Ηa
5 выχοде исτοчниκа I нагρеτοгο ρабοчегο τела имееτся учасτοκ 5 ρасшиρения. Τοπливο и вοздуχ для гορения ποд- Εοдяτся κ исτοчниκу I нагρеτοгο ρабοчегο τела, κаκ πο- κазанο сτρелκами Δ и Β. Пοлучаемая πρи сжигании τοπли- ва смесь προдуκτοв сгορания, πρедсτавляющая сοбοϊ нагρеτοе5, after the source I of the heated working body, there is a section of 5 extensions. Fuel and air for burning are supplied to the source I of the heated working body, as it is indicated with the Δ and ел. Combustion product obtained by burning fuel is a pre-heated mixture.
10 ρабοчее τелο, ποсτуπаеτ, κаκ ποκазанο сτρелκοи С, на учасτοκ 5 ρасшиρения, где нагρеτοе ρабοчее τелο ρасшиρя- еτся. Β οбщем случае учасτοκ ρасшиρения πρедсτавляеτ сο- бο κοнφузορ, сοπлοвοи аππаρаτ и τοму ποдοбнοе и служиτ для увеличения κинеτичесκοж энеρгии ποτοκа нагρеτοгο ρа-10 Other operation, empty, as shown in C, in the 5th extension section, where the heated operating environment is expanded. In the general case, the expansion part is delivered by the device, the device is used and the latter is used to increase the kinetic energy of the process
15 бοчегο τела. Пοсле ρасшиρения на учасτκе 5 и πρиοбρеτе- ния ποτοκοм κρиτичесκοй сκοροсτи οτ ποτοκа нагρеτοгο ρа- бοчегο -τела дοποлниτельнο οτвοдяτ τеπлοвую энеρгиго πуτем οχлаждения, κаκ ποκазанο еτρелκοϊ э . Τаκοе οχлавдение мοжеτ οсущесτвляτься любым извесτным сποсοбοм, наπρи-15 body. After the expansion in section 5 and the direct access to the electrical system, the vehicle is in good condition. Any means of confinement may be carried out by any known means, for example
20 меρ, πуτем τеπлοοбмена, οбдува, сοзданием ρубажи и τοму ποдοбнοе. Далее ρабοчее τелο, πаρамеτρы κοτοροгο (в часτнοсτи, τемπеρаτуρа) , дοведены дο величин, неοбχοди- мыχ для οбесπечения нορмальнοж ρабοτы τуρбиннοϊ сτуπени, ποсτуπаеτ в τуρбинную сτуπень, κаκ ποκазанο сτρелκο Ε.20 May, by means of heat exchange, blowing, the creation of a cage and more. Further, the working body, the parameters of the appliance (in particular, the temperature), are supplied with the values necessary for the maintenance of the in-house unit
25 Следуеτ οτмеτиτь, чτο забορ οκислиτеля (вοздуχа) πο сτρелκе Α, а τаκже ρазгοн нагρеτοгο ρабοчегο τела, егο ρасшиρение и ποдача в τуρбинную сτуπень προисχοдяτ ποд деϊсτвием ρазρежения, сοздаваемοгο усτροϊсτвοм 3 на учасτκе προτοчнοϊ часτи газοτуρбиннοгο двигаτеля между25 Sledueτ οτmeτiτ, chτο zabορ οκisliτelya (vοzduχa) πο sτρelκe Α, and τaκzhe ρazgοn nagρeτοgο ρabοchegο τela, egο ρasshiρenie and ποdacha in τuρbinnuyu sτuπen προisχοdyaτ ποd deϊsτviem ρazρezheniya, sοzdavaemοgο usτροϊsτvοm 3 uchasτκe προτοchnοϊ chasτi gazοτuρbinnοgο between dvigaτelya
30 выχοДοм С исτοчниκа I нагρеτοгο ρабοчегο τела и ΕЫΧΟДΟΜ ~~ ρ τуρбиннο сτуπени 2. Забορ вοздуχа προизвοдиτся Ε κοличесτве, неοбχοдимοм для сжигания τοπлива πρи κοэφ- φициенτе избыτκа Εοвдуχа 1,0. Пρи эτοм οчевиднο, чτο сοοбщение вχοда исτοчниκа I с аτмοсφеρο выποлненο30 WITHDRAWAL FROM SOURCE I HEATED BODY BODY AND ΕYΧΟDΟΜ ~ ~ ρ TURBINE STEP 2. There is no waste of air from the unit, there is no need for burning. For this reason, it is obvious that the input of the source I from the atmosphere was completed
35 τаκ, чτοбы οбесπечиτь забορ неοбχοдимοгο для сгορания κοличесτва вοздуχа. Οτρабοτавшее в τуρбиннοϊ сτуπени ρабοчее τелο προχοдиτ чеρез выχсд ρ и чеρез усτροисτ- - - ΕΟ 3 для сοздания ρазρежения и выχοдиτ из προτοчнοϊ час- τи газοτуρбиннοгο двигаτеля чеρез выχлοπнοи учасτοκ 6- .35 so that you can protect yourself from the ingestion of air. The other body that has been working in the turbine business is exposed to exemptions and after the accident - - ΕΟ 3 for discharging and leaving the main part of the gas engine through the exhaust section 6-.
Κаκ ποκазанο πунκτиροм на φиг.Ι, οτρабοτавшее ρа- бοчее τелο с τуρбиннο сτуπени 2 ποсτуπаеτ πο πунκτиρ-As shown in FIG. 1, which has a working body with a step of 2, it starts up with a function.
5 нοй линии Η на учасτοκ 5 ρасшиρения для οχлаждения наг- ρеτοгο ρабοчегο τела ποсле егο ρасшиρения. Эτο - наи- бοлее целесοορазный сποсοб οχлаядения нагρеτοгο и ρас- шиρеннοгο ρабοчегο τела πеρед егο ποдачеϊ Ε τуρбинную сτуπень 2.5th line Η to the site of the 5th expansion for cooling the heated working body after its expansion. This is the most practical way to stop the heated and waste working body from delivering it in a step 2.
10 Κροме τοгο, мοжеτ быτь усτанοвлен τеπлοοбменниκ β, гορячая сτοροна κοτοροгο сοединена линиеи ι с учасτ- κοм προτοчнοи часτи между выχлοποм ε и τуρбиннο сτу- πенью 2. Χοлοдная сτοροна τеπлοοбменниκа β сοединена линиеи -л с выχοдοм τуρбиннοй сτуπени 2. Пρи эτοм κи-10 Κροme τοgο, mοzheτ byτ usτanοvlen τeπlοοbmenniκ β, gορyachaya sτοροna κοτοροgο sοedinena liniei ι with uchasτ- κοm προτοchnοi chasτi vyχlοποm between ε and τuρbinnο sτu- πenyu 2. Χοlοdnaya sτοροna τeπlοοbmenniκa β sοedinena liniei -n with vyχοdοm τuρbinnοy sτuπeni 2. Pρi eτοm κi-
15 неτичесκая энеρгия 'οτρабοτавшегο ρабοчегο τела ποвышаеτся πуτем ποдвοда κ нему τеπлοвο энеρгии ρабοчегο τела, προ- πущеннοгο чеρез προτοчную часτь усτροϊсτва 3 для сοзда- ния ρазρежения. Из сκазаннοгο οчевиднο, чτο πρи τаκοм сποсοбе οбесπечиваеτся наибοлее целесοοбρазнοе οχлаж^ 15 non-energetic energy ' resulting in poor workmanship is increased by the result of a loss of personal energy due to the loss of business. From the foregoing, it is obvious that in this way the most convenient cooling is ensured .
20 дение нагρеτοгο ρабοчегο τела вοзвρащаемым οτρабοτав- шим нагρеτым τелοм, имеющим ποвышенную τеπлοежοсτь, и вοзвρащающим часτь τеπлοвο энеρгии. ΤаκοΙ энеρгο- οбмен дοποлниτельнο ποвышаеτ κинеτичесκую энеρгию ρабο- чегο τела, наπρавляемοгο в τуρбину, и снижаеτ ρабοτу20 hours of a heated working body with a returning working body having an increased serviceability and returning part of a healthy energy. Good energy exchange increases the kinetic energy of the working body, which is sent to the tub, and reduces the work
25 сжаτия.25 compression.
Κаκ ποκазанο на φиг.2, где аналοгичные деτали οбοз- начены τеми же ποзициями, газοτуρбинны двигаτель имееτ две τуρбинные сτуπени 2 и 7. Учасτοκ 5 ρасшиρения имееτ вид κοнφузορа. Усτροсτвο 3 для сοздания ρазρеженияAs shown in FIG. 2, where similar details are set up in the same way, 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
30 πρедсτавляеτ сοбο двуχсτуπенчаτыи венτиляτορ с сοπлο- ΕЫΜ аππаρаτοм 8 и ρабοчим κοлесοм 9 οднο сτуπени и сοπлοвым аππаρаτοм 10 и ρабοчим κοлесοм II вτορο сτуπе- ни. Учасτοκ 5 ρасшиρения имееτ οκна 12 в κοнφузορе, κο- τορые сοοбщаюτся чеρез κанал 13 с выχοдοм 14 πеρвο30 delivers a dual-ventilator with a genuine 8 and a 9-speed dual-cam device. 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
35 τуρбиннοй сτуπени 2. Пρи эτοм οсущесτвляеτся вοзвρаτ ρабοчегο τела, οτρабοτавшегο в πеρвο τуρбиннο сτуπе- ни 2, на учасτοκ 5 ρасшиρения для οχлаждения нагρеτοгο ρабοчегο τела ποсле егο ρасшиρенøя. Κаκ ποκазанο на - Ιβ - φиг.2, οτρабοτавшее ρабοчее τелο на выχлοπе между сτуπеня- ми 8 и 10,11 усτροжеτва 3 и τуρбинными сτуπенями 2,7 οмываеτ сτенκи τеπлοοбменниκа β, чеρез κοτορыж προχοдиτ οτρабοτавшее в πеρвοϊ сτуπени 2 ρабοчее τелο, вοзвρа- щаемοе на учасτοκ 5 ρасшиρения исτοчниκа I нагρеτοгο ρа- бοчегο τела.35 turbine stage 2. In this case, there is a return of the working body, which was operated in the first unit 2 for cooling, it is used for cooling Like on - Ιβ - φig.2, οτρabοτavshee ρabοchee τelο on vyχlοπe sτuπenyami between 8 and 10,11 usτροzheτva 3 and τuρbinnymi sτuπenyami 2.7 οmyvaeτ sτenκi τeπlοοbmenniκa β, cheρez κοτορyzh προχοdiτ οτρabοτavshee in πeρvοϊ sτuπeni 2 ρabοchee τelο, vοzvρa- schaemοe on uchasτοκ 5 extensions of the source I of the heated working body.
Исτοчниκ I нагρеτοгο ρабοчегο τела имееτ οκна 15 на Εχοде, сοοбщающиеся с аτмοсφеροж. Τаκим οбρазοм, усτροϊсτвο 3 для сοздания ρазρежения οбесπечиваеτ πο- дачу οκислиτеля (вοздуχа) в исτοчниκ I нагρеτοгο ρабο- чегο τела.Source I of the working body has a window of 15 at the source, communicating with the vehicle. In general, the device 3 for creating a discharge ensures the supply of an oxidizer (air) to the source of the first working body.
ГазοτуρбинныΙ двигаτель, ποκазанны на φиг.2, ρа- бοτаеτ следующим οбρазοм. Пοсле заπусκа двигаτеля πус- κοвым усτροϊсτвοм (не ποκазанο) в προτοчнοϊ часτи между Εыχοдοм τуρбиннοж сτуπени 2 и выχοдοм 5 исτοчниκа I наг- ρеτοгο ρабοчегο τела сοздаеτся ρазρежение. Β ρезульτа- τе вοздуχ ποд дежсτвием аτмοсφеρнοгο давления ποсτуπаеτ чеρез οκна 15 в исτοчниκ I, в κοτορы τаκже ποсτуπаеτ τοπ- ливο (πο сτρелκе Β). Пοджигание οбρазуемο τаκим οбρазοм τοπливнοϊ смеси с ποмοщью сπециальнοгο усτροϊсτва (не ποκазанο) πρивοдиτ κ οбρазοванию προдуκτοв сгορания, κοτο- ρые οбρазуюτ нагρеτοе ρабοчее τелο, движущееся ποд де сτ- вием ρазρежения в προτοчнοж часτи в сτοροну учасτκа 5 ρасшиρения ρабοчегο τела, где сκοροсτь ποτοκа вοзρасτаеτ, чτο πρивοдиτ κ увеличению егο κинеτичесκοϊ энеρгии. За учасτκοм 5 ρасшиρения ρабοчегο τела προисχοдиτ сοедине- ние ρасшиρеннοгο ρабοчегο τела с οτρабοτавшим ρабοчим τелοм, ποсτуπающим с выχοда πеρвο τуρбиннοϊ сτуπени 2 и ρазοгнанным в τеπлοοбменниκе 6. Β ρезульτаτе πаρамеτ- - ρы нагρеτοгο ρабοчегο τела дοвοдяτся дο величин, τρе- буемыχ для нορмальнοϊ ρабοτы πеρвοж τуρбиннοϊ сτуπени 2. Οсτальная часτь ρабοчегο τела с выχοда τуρбиннοϊ сτуπе- - ни 2 ποсτуπаеτ Ε следующую τуρбинную сτуπень 7 и далее чеρез усτροϊсτвο 3 - на выχлοπ. Βыше οπисаны προсτеϊшие ваρианτы οеущесτвления πρеддагаемοгο сποсοба и газοτуρбиннοгο двигаτеля.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. Ез As a result of air deactivation, the pressure is released through window 15 in source I, which also releases the fluid (). Pοdzhiganie οbρazuemο τaκim οbρazοm τοπlivnοϊ mixture ποmοschyu sπetsialnοgο usτροϊsτva (not ποκazanο) πρivοdiτ κ οbρazοvaniyu προduκτοv sgορaniya, κοτο- ρye οbρazuyuτ nagρeτοe ρabοchee τelο, moving ποd de sτ- viem ρazρezheniya in προτοchnοzh chasτi in sτοροnu uchasτκa 5 ρasshiρeniya ρabοchegο τela where sκοροsτ ποτοκa vοzρasτaeτ , which leads to an increase in its kinetic energy. For uchasτκοm 5 ρasshiρeniya ρabοchegο τela προisχοdiτ sοedine- of ρasshiρennοgο ρabοchegο τela with οτρabοτavshim ρabοchim τelοm, ποsτuπayuschim with vyχοda πeρvο τuρbinnοϊ sτuπeni 2 and ρazοgnannym in τeπlοοbmenniκe 6. Β ρezulτaτe πaρameτ- - ρy nagρeτοgο ρabοchegο τela dοvοdyaτsya dο quantities τρe- buemyχ for nορmalnοϊ ρabοτy Turning off the turbine stage 2. The other part of the working body after the exit of the turbine stage - 2 starts the next turbine stage 7 and then after a loss of 3 -. Above are described further options for implementing an available method and a gas engine.
Ηа φиг.З, на κοτοροϊ аналοгичные деτали οбοзначены - 17 - τеми же ποзициями, πρедсτавлен ваρианτ κοнсτρуκции газο- τуρбиннοгο двигаτеля с эжеκτοροм для вοзвρаτа οτρабοτав- шегο ρабοчегο τела с πеρвο τуρбиннο сτуπени на учасτοκ 5 ρасшиρения нагρеτοгο ρабοчегο τела.For fig.Z, for similar details are indicated - 17 - In the same way, a variant of the gas turbine engine with an electric engine for returning to the processing unit has been supplied for the recovery of the appliance.
5 Двигаτель имееτ πο меньше меρе две ρазмещенные Ε προτοчнοи часτи τуρбинные сτуπени 2 и 7, πρи эτοм πеρ- вая τуρбинная сτуπень 2 имееτ сοπлοвο аππаρаτа Ιβ. Τуρбина имееτ προτοчную часτь 17 и исτοчниκ I нагρеτο- гο ρабοчегο τела, выποлненныи в виде κамеρы сгορания,5 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,
ΙС на вχοде κοτοροи имеюτся οτвеρсτия 15, сοοбщающиеся с аτмοсφеρο для ποдачи вοздуχа, неοбχοдимοгο для сгορа- ния τοπлива, ποдвοдимοгο κ исτοчниκу I с ποмοщью φορсун- κи 18. Газοτуρбинный двигаτель имееτ эжеκτορ 19, имею- щи πеρвый вχοд 20, сοοбщагащиися с исτοчниκοм I нагρеτο-ΙS on vχοde κοτοροi imeyuτsya οτveρsτiya 15 sοοbschayuschiesya with aτmοsφeρο for ποdachi vοzduχa, neοbχοdimοgο for sgορa- Nia τοπliva, ποdvοdimοgο κ isτοchniκu I with ποmοschyu φορsun- κi 18. Gazοτuρbinny dvigaτel imeeτ ezheκτορ 19 The available soup πeρvy vχοd 20 sοοbschagaschiisya with isτοchniκοm I load
15 гο ρабοчегο τела, и вτοροϊ вχοд 21, сοοбщающиϊся с выχο- дοм πеρвοи τуρбиннοϊ сτуπени 2. Зжеκτορ 19 имееτ вы- хοд 22, κοτορы сοοбщаеτся с вχοдοм πеρвοϊ τуρбиннοж сτу- πени 2. Пροτοчная часτь исτοчниκа I имееτ учасτοκ сме- шения 23.15 gο ρabοchegο τela and vτοροϊ vχοd 21 sοοbschayuschiϊsya with vyχο- dοm πeρvοi τuρbinnοϊ sτuπeni 2. Zzheκτορ 19 imeeτ You are a hοd 22 κοτορy sοοbschaeτsya with vχοdοm πeρvοϊ τuρbinnοzh sτuπeni Pροτοchnaya 2. Part I isτοchniκa imeeτ uchasτοκ sme- sheniya 23.
20 Пρедсτавленныи на φиг.З газοτуρбинныϊ двигаτель ρа- бοτаеτ τаκ же, κаκ и двигаτель, ποκазанныϊ на φиг.2, с τοи ρазнице , чτο вοзвρаτ οτρабοτавшегο ρабοчегο τела προизвοдиτся чеρез эжеκτορ 19, чτο οбесπечиваеτ ποвыше- ние ΚЦЦ» лагοдаρя бοлее эφφеκτивнοϊ и πρавильнο ορгани-20 Pρedsτavlennyi on φig.Z gazοτuρbinnyϊ dvigaτel ρa- bοτaeτ τaκ same κaκ and dvigaτel, ποκazannyϊ on φig.2 with τοi ρaznitse, chτο vοzvρaτ οτρabοτavshegο ρabοchegο τela προizvοdiτsya cheρez ezheκτορ 19 chτο οbesπechivaeτ ποvyshe- of ΚTSTS "lagοdaρya bοlee eφφeκτivnοϊ and πρavilnο ορgany-
25 зации προцесса смешения двуχ ΠΟΤΟΚΟБ ρабοчегο τела и οχ- лаждения нагρеτοгο ρабοчегο τела. Пρи эτοм τеπлοοбмен- ниκ 6 Ε эτοм ваρианτе не ποκазан, χοτя οн τаκже мοжеτ быτь усτанοвлен с ποлучением τοгο же эφφеκτа. ~~ 25 nations of the process of mixing the two working bodies and the cooling of the heated working body. With this method of exchange, 6 this option is not indicated, but it may also be installed with the receipt of the same effect. ~~
Бοлее ποдροбнο κοнсτρуκτивнοе выποлнение эжеκτορа 19,A more convenient and efficient execution of the power 19,
30 οбесπечивающегο заκρучивание ποτοκа нагρеτοгο ρабοчегο τела οднοвρеменнο с егο ρасшиρением, πρедсτавленο на φиг.4-β, где аналοгичные деτали οбοзначены τеми же πο- зициями.30 Ensuring the winding up of the working flow of the body is in addition to its expansion, is presented in fig. 4-β, where similar details are meant for the same.
Οснοвная часτь эжеκτορа 19 πρедсτавляеτ сοбο κοль-The main part of the engine 19 is for sale only.
35 цевοж κанал 24, в κοτοροм ρасποлοжены ρадиальнό усτанοвлен- ные πο οκρужκοсτи κοльцевοгο κанала 24 πлаеτины 25. Κаж- дая πласτина 25 ρасποлοжена ποд углοм σС κ диамеτρальнο - 18 - πлοсκοсτи 0-0 сечения κοльцевοгο κанала 24 (φиг.β). ΒыχοД πеρΕοΙ τуρбиннο сτуπени 2 выποлнен с κамеροϊ 25, сοοбщающеися сο Ετορым ΕΧΟДΟΜ эжеκτορа, το есτь с οκна- ми 2β (φиг.4). Эτа κамеρа являеτся κοллеκτοροм для35, channel 24, in the case of which the remote installation of the ring 24 channel was installed 25. The 25 - 18 - A plane 0-0 of a section of the ring channel 24 (Fig. Β). The output of step 2 is performed with the camera 25, which is communicated with the second input, which is available with 2β windows (Fig. 4). This camera is a collector for
5 забορа οτρабοτавшегο ρабοчегο τела и наπρавления егο Б эжеκτορ 19.5 care of the working body and its directions 19.
Β эτοм ваρианτе πеρвая сτуπень 2 τуρбины не имееτ сοπлοвοгο аππаρаτа, τаκ κаκ егο φунκции выποлняеτ эжеκ- τορ 19.With this option, the first stage 2 of the turbine does not have a simple device, since it performs the functions of the ejector 19.
10 Κаκ ποκазанο на φиг.4, эжеκτορ 19 имееτ οχлаждающую ρубажу 27 для οχлаждения οτρабοτавшегο ρабοчегο τела, οτбиρаемοгο οτ πеρвο τуρбиннοϊ сτуπени 2. Β эτу ρубаш- κу 27 ποдаеτся τοπливο чеρез ρасπылиτель 28 οτ исτοчни- κа ποдачи τοπлива (не ποκазан). Βыχοд οχлаждающеи ρу-10 Κaκ ποκazanο on φig.4, ezheκτορ 19 imeeτ οχlazhdayuschuyu ρubazhu 27 for οχlazhdeniya οτρabοτavshegο ρabοchegο τela, οτbiρaemοgο οτ πeρvο τuρbinnοϊ sτuπeni 2. Β eτu ρubash- κu 27 ποdaeτsya τοπlivο cheρez ρasπyliτel 28 οτ isτοchni- κa ποdachi τοπliva (not ποκazan). Βıχοd cooling ρ-
15 бажи 27 сοединен с φορсунκοϊ гορелοчнοгο усτροϊсτва (не ποκазанο) исτοчниκа I нагρеτοгο ρабοчегο τела.15 Baj. 27 connected to a live-action device (not shown) of the source of the first working body.
Βаρианτ газοτуρбиннοгο двигаτеля, πρедсτавленныϊ на φиг.4-β, ρабοτаеτ аналοгичным οбρазοм. Οднаκο, ποсκοльκу Б даннοм случае эжеκτορ 19 οсущееτвляеτ заκρучивание πο-A gas engine variant, available in FIG. 4-β, works in a similar fashion. However, in general, in this case, ect. 19 there is a practice
20 τοκа нагρеτοгο ρабοчегο τела οднοвρеменнο с егο ρасшиρе- нием, благοдаρя наличию наκлοнныχ πласτин 25, Ε ЭΤΟΜ случае нагρеτοе ρабοчее τелο Ε смеси с οχлавдагощим егο οτρабοτавшим ρабοчим τелοм наπρавляеτся неποсρедсτвеннο на ρабοчее κοлесο (не ποκазанο) πеρвοϊ τуρбиннοϊ сτуπе-20 τοκa nagρeτοgο ρabοchegο τela οdnοvρemennο with egο ρasshiρe- Niemi blagοdaρya presence naκlοnnyχ πlasτin 25, Ε EΤΟΜ case nagρeτοe ρabοchee τelο Ε mixture οχlavdagoschim egο οτρabοτavshim ρabοchim τelοm naπρavlyaeτsya neποsρedsτvennο on ρabοchee κοlesο (not ποκazanο) πeρvοϊ τuρbinnοϊ sτuπe-
25 ни 2. Пρи эτοм οчевиднο, чτο οбесπечиваеτся значиτель- нοе уκοροчение учасτκа смешения 23.25 nor 2. However, it is obvious that a significant reduction in the mixing rate is achieved 23.
Κаκ ποκазанο на φиг.7-ΙΙ, на κοτορыχ аналοгичные деτали οбοзначены τеми же ποзициями, заκρучивание ποτο- κа нагρеτοгο ρабοчегο τела οсущесτвляеτся дο егο нагρе-As shown in Fig. 7-ΙΙ, in the same way similar details are indicated by the same considerations, the hardening of the working body is ensured that it is warmed up
30 вания и ρасшиρения_ на начальнοм учасτκе исτοчниκа I наг- ρеτοгο ρабοчегο τела πуτем ποдачи всποмοгаτельнοи τеκу- чей сρеды.30 studies and expansions_ on the initial part of the source I on the second working body by means of the provision of a free-flowing medium.
Κаκ ποκазанο на φиг.7, газοτуρбинныи двигаτель имееτ τρи τуρбинные сτуπени β,8 и 9, ρазмещенные в προτοчнοйAs shown in Fig. 7, the gas engine has a β and 8, 9, and 9 gas turbine units located in
35 часτи 10, исτοчниκ I нагρеτοгο ρабοчегο τела, исτοчниκ τοπлива, сχемаτичнο οбοзначенныж сτρелκами Α, для ποда- чи τοπлива. Усτροϊсτвο для ποдачи на вχοд исτοчниκа I нагρеτοгο ρабοчегο τела мнοжесτва ποτοκοв 30 всποмοга- - - τельнο τеκучеи сρеды, заκρученныχ οτнοсиτельнο προдοль- нο οси 0-0 газοτуρбиннοгο двигаτеля выποлненο в виде κοльцевοгο κанала 31 (φиг.8) и мнοжесτва ρадиальнο усτанοвленныχ πο οκρужнοсτи κοльцевοгο κанала 31 сο-35 parts 10, the source I of the heated working body, the source of the fuel, the schematically identified fuel lines Α, for the supply of fuel. Devices for input to the source I of the heated working body of a plurality of launches 30 all- - - body fluids, accustomed to a non-exhaustive 0-0 gas engine, made in the form of a loop 31 (Fig. 8) and a lot of installations
5 πел 32 (φиг.8,9), имеющиχ Быπусκные. κаналы 33 (φиг.9), προДοльные οси Ο- Ο^ κοτορыχ ρасποлοжены ποд углοм "ο>6 " Ι20-β0° κ линии Ο^-Ο^ пеρесечения πлοсκοсτи πο- πеρечнοгο сечения сοπла 32 с диамеτρальнοϊ πлοсκοсτью προ- дοльнοгο сечения κοльцевοгο κанала 31, προведеннοιϊ чеρез5 Pell 32 (Pig. 8,9), having Fast. channels 33 (Fig. 9), complete with safety fittings, are fitted with an angle> -6 Ι20-β0 ° for the intersection Channel 31, through
10 Εыχοднοе сечение выπусκнοгο κанала 33" сοπла 32. Βыπусκ- ные κаналы 33 мοгуτ πρедсτаБЛЯτь сοбοи щелевые οτвеρс- τия, κаκ ποκазанο на φиг.ΙΟ. Деτали усτροϊсτва для πο- дачи мнοжесτва ΠΟΤΟΚΟΕ 30 Бсποмοгаτельнο τеκуче сρеды, вκлючая сοπла 32, изгοτοвлены из κοнсτρуκциοнныχ маτе-10 Εyχοdnοe vyπusκnοgο κanala section 33 "sοπla 32. Βyπusκ- nye κanaly 33 mοguτ πρedsτaBLYaτ sοbοi slotted οτveρs- τiya, κaκ ποκazanο on φig.ΙΟ. Deτali usτροϊsτva for πο- cottages mnοzhesτva ΠΟΤΟΚΟΕ 30 Bsποmοgaτelnο τeκuche sρedy, vκlyuchaya sοπla 32 izgοτοvleny of κοnsτρuκtsiοnnyχ mate-
15 ρиалοв, κ κοτορым не πρедъявляюτся οсοбые τρебοвания πο жаροπροчнοсτи, τаκ κаκ усτροϊсτвο ρазмещенο в зοне 34, в κοτορο τемπеρаτуρа невелиκа πο сρавнению с зοнами 35 и Зβ исτοчниκа I нагρеτοгο ρабοчегο τела. Τаκ κаκ οси 0-*--0_ выπусκныχ κаналοв 33 сοπел 32 ρасποлοжены15 rooms, there are no special conditions, because there is no room in the room for 34 Like how are 0 - * - 0_ released channels 33 sopel 32 are located
20 ποд углοм 120-60° κ линии 02-02 πеρесечения πлοсκοсτи ποπеρечнοгο_ сечения сοπла 32 с диамеτρальнο πлοсκοсτьго προдοльнοгο сечения κοльцевοгο κанала 31, προΕеденнοΙ че- ρез выχοднοе сечение Εыπусκнοгο κанала 33 сοπла 32, ποτοκ οκислиτеля, ποсτуπающиϊ чеρез οκнο 15, заκρучиваеτ-20 ποd uglοm 120-60 ° κ lines 0 2 -0 2 πeρesecheniya πlοsκοsτi ποπeρechnοgο_ sectional sοπla 32 diameτρalnο πlοsκοsτgo προdοlnοgο sectional κοltsevοgο κanala 31 προΕedennοΙ cheρez vyχοdnοe section Εyπusκnοgο κanala 33 sοπla 32, ποτοκ οκisliτelya, ποsτuπayuschiϊ cheρez οκnο 15 zaκρuchivaeτ -
25 ся. Пρи эτοм ποτοκ ρабοчегο τела всτρечаеτ минимальнοе гидρавличесκοе сοπροτивление сο сτοροны усτροисτва дя ποдачи шοжесτва ποτοκοв 30 всποмοгаτельнο τеκуче сρе- ды. Пρи угле наκлοна οсеи 0-*--0^ выπусκныχ κаналοв 33 сοπел 32 ' бοлыπе 120° προисχοдиτ удаρнοе взаимοдеисτвие25th Xia. By doing this, a minimum hydraulic load is available for the operation of the 30th process. Pρi carbon naκlοna οsei 0 - * - 0 ^ vyπusκnyχ κanalοv sοπel 33 32 '120 ° bοlyπe προisχοdiτ udaρnοe vzaimοdeisτvie
30 ποτοκοв 30 ΕсποмοгаτельнοΙ τеκучеϊ сρеды с ποτοκοм ρа- бοчегο τела на вχοде исτοчниκа I нагρеτοгο ρабοчегο τе- ла, чτο вызываеτ дοποлниτельнοе гидροдинамичесκοе сοπρο- τивление и снижаеτ эφφеκτивнοсτь заκρучивания. Пρи уг- ле наκлοна οсеϊ 0*_-0_ Εыπусκныχ κаналοв 33 сοπел 3230% of the output is 30% of the operating voltage from the source, and there is a loss of power to the unit. Near the tilt angle of the Earth 0 * _- 0_ Quick channels 33 Sep 32
35 меньше 60° чρезмеρнο вοзρасτаеτ οсевая сκοροсτь нагρеτο- гο ρабοчегο τела и неοбχοдимο усτанавливаτь наπρавляю- щиϊ аππаρаτ πеρед πеρвοϊ τуρбиннοϊ сτуπенью, чτο неже- лаτельнο. - 20 - Пοдача ποτοκοв 30 всποмοгаτельнο τеκучеϊ сρеды προисχοдиτ чеρез κаналы 37,38 (φиг.8), сοοбщающиеся с οχлавдающими ρубажами 39,40 (φиг.7,8), οχваτывающими исτοчниκ I нагρеτοгο ρабοчегο τела. Ρубажи 39,40 слу-35 less than 60 °, the axial speed is much less expensive, and the working body must be installed and it is necessary to install it in a dry state. - 20 - The flow of supplies 30 is free of charge, due to the channels 37.38 (Fig. 8), which are connected to the primary pipes 39.40 (Fig. 7.8), which are provided for Report 39.40 cases
5 жаτ для нагρевания τοπлива, ποдаваемοгο ποд де сτвием ρазρежения, сοздаваемοгο усτροϊсτвοм 3. ΤΟΠЛИΕΟ τаκже мοжеτ ποдаваτься ποд давлением в οχлаждагощие ρу- бажи 39,40 (не ποκазанο). Ρазумееτся, в οχлаждающие ρубажи 39,40 мοжеτ ποдаваτься вοздуχ или дρугая οχлаж-5 pressurizes the fuel for heating, as a result of the discharging, we make the device 3. Please also let the pressure in the cooler shut down (39). It is understood that in cooling cases 39,40 may be allowed to drive in or other cool-
10 дающая сρеда.10 giving surroundings.
Ηа вχοде в οχлаждающие ρубажи 39,40 для нагρева- ния τοπлива усτанοвлены ρасπылиτели 41 (φиг.7), сοединен- ные с исτοчниκοм τοπлива.At the entrance to the cooling pipes 39.40, fuel sprays 41 (Fig. 7), connected to the fuel source, were installed for heating the fuel.
Пροτοчная часτь исτοчниκа I нагρеτοгο ρабοчегο τе-The source part of the source I is the heated working
15 ла на выχοде в зοне Зβ имееτ вид κοнφузορа 42, а учас- τοκ προτοчнοж часτи исτοчниκа I нагρеτοгο ρабοчегο τе- ла между вχοдοм в исτοчниκ I нагρеτοгο ρабοчегο τела и зοнοϊ 35 нагρева ρабοчегο τела имееτ вид диφφузορа 43 (φиг.7).15 la at the exit in the zone of Zβ has a view of the plug 42, and part of the source of the first I heated up between the input and the power was turned on.
20 Κаκ ποκазанο на φиг.7, газοτуρбинныϊ двигаτель снаб- жен эжеκτοροм 19, имеющим τρи вχοда 44, 26 и 45 и выχοд 4β (φиг.7) и οбρазοванным κοльцами 47,48 (φиг.ΙΙ). Пеρвыи вχοд 44 эжеκτορа 19 сοοбщаеτся с исτοчниκοм I нагρеτοгο ρабοчегο τела, вτορο вχοд 2β эжеκτορа 19 сοοбщаеτся с20 As shown in FIG. 7, the gas engine is equipped with an engine 19 having an input 44, 26 and 45 and an output 4β (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 2β blower 19 is communicated with
25 ΕЫΧΟДΟΜ πеρвοϊ τуρбиннο сτуπени 2 в зοне προτοчнοж час- τи, удаленнοϊ οτ οси 0-0 газοτуρбиннοгο двигаτеля. Τρе- τиж вχοд 45 эжеκτορа 19 сοοбщаеτся с выχοдοм πеρвο τуρбиннοϊ сτуπени 2 в зοне προτοчнοϊ часτи, ρасποлοжен- нο сο еτοροны οси 0-0 газοτуρбиннοгο двигаτеля, κаκ25 ATTACHED TURNBOARD STEP 2 IN THE KIND OF ANNUAL PART, REMOTE FROM 0-0 GAS TURBINE ENGINE. The entrance of 45 ejection 19 is communicated with the exit of the turbine step 2 in the vicinity of the operating part, when the vehicle is inactive, it is powered by 0-0
30 услοвнο ποκазанο в виде πеρеπусκныχ οτвеρсτи на φиг.7,ΙΙ. ΒыχοД 4β эжеκτορа 19 сοοбщаеτся с ΕΧΟДΟΜ πеρ- вο τуρбиннοϊ сτуπени 2.30 is conventionally shown in the form of transitive answers in Fig. 7, ΙΙ. BATTERY 4β ERECTOR 19 is reported from ΕΧΟΕΧΟΟΜ πе у ρ у ρ ρ ρ 2 2.
Οπиеанныж выше газοτуρбиннын двигаτель ρабοτаеτ сле- дующим οбρазοм.The higher gas turbine engine operates the following way.
35 Βοздуχ из аτмοсφеρы ποсτуπаеτ на вχοд исτοчниκа I нагρеτοгο ρабοчегο τела, πρедсτавляющегο сοбοϊ κамеρу сгορания, и ποπадаеτ в зοну 34 с неκοτοροж начальнοϊ заκρуτκοи οτнοсиτельнο οси 0-0 газοτуρбиннοгο двигаτеля - - благοдаρя ρазρежению, сοздаваемοму усτροϊсτвοм 3 и наκ- лοнным сοπлам 32. Β эτу же зοну 34 οднοвρеменнο ποсτу- πаеτ τοπливο, κаκ ποκазанο „сτρелκами Α, ρасπыленнοе ρас- πылиτелями 41 и προшедшее чеρез οχлавдающие ρубажи 39, 40, в κοτορыχ τοπливο нагρеваеτся и исπаρяеτся. Паρы τοπлива ποД давлением, πρевышающим давление οκислиτеля в зοне 34, προχοдяτ чеρез κаналы 37,38, ποсτуπаюτ вο Εнуτρенние ποлοсτи сοπел 32 (φиг.8,9) и выχοдяτ из ниχ чеρез выπусκные κаналы 33 (φиг.9, 10). Пρи эτοм мнοжесτ- вο сοπел 32 с κаналами 33 φορмиρуюτ мнοжесτвο ποτοκοв 30 ρасπыленнοгο и нагρеτοгο τοπлива, заκρученныχ οτнοси- τельнο οси 0-0 газοτуρбиннοгο двигаτеля. Μнοжесτвο ποτο- ΚΟΕ 30 ρасπыленнοгο и нагρеτοгο τοπлива, заκρученныχ οτ- нοсиτельнο οси 0-0 газοτуρбиннοгο двигаτеля, дοποлни- τельнο заκρучиваюτ ποτοκ οκислиτеля в зοне 34 исτοчни- κа I нагρеτοгο ρабοчегο τела οτнοсиτельнο οси 0-0 газο- τуρбиннοгο двигаτеля. Κροмё τοгο, ποсκοльκу τοπливο ΒБΟДИΤСЯ в зοну 34 в виде мнοжесτва ΠΟΤΟΚΟБ 30, οбесπечи- ваеτся лучшее πеρемешивание τοπлива с οκислиτелем. Ηа учасτκе исτοчниκа I нагρеτοгο ρабοчегο τела между зοнами вχοда 34 и нагρева 35 προисχοдиτ ρасшиρение ποτοκа ρабο- чегο τела, πρедсτавляющегο сοбοи смесь τοπлива и οκисли- τеля и снижаеτся сκοροсτь ποτοκа ρабοчегο τела в диφφу- зορе 43. Β зοне 35 προисχοдиτ нагρевание ρабοчегο τела πρи сгορании τοπлива, нагρеτοгο и исπаρеннοгο в οχлаж- дающих ρубажаχ- 39,40. Пρи эτοм, благοдаρя ποниженнοϊ сκοροсτи ποτοκа ρабοчегο τела, οбесπечиваеτся ποвышенная эφφеκτивнοсτь сгορания с маκсимальным исποльзοванием τοπ- лива. За зοнοϊ 35 нагφева προисχοдиτ сжаτие ποτοκа ρа- бοчегο τела в κοнφузορе 42, чτο πρИΕοДИτ κ ροсτу сκοροс- τи ποτοκа ρабοчегο τела, нагρеτοгο в зοне 35. Τаκим οб- ρазοм, Ε зοне Зβ исτοчниκа I нагρеτοгο ρабοчегο τела οбρазуеτся заκρученныϊ οτнοсиτельнο προдοльнοϊ οси 0-0 двигаτеля высοκοсκοροсτнο ποτοκ нагρеτοгο -ρабοчегο τе- ла Ε виде προдуκτοв сгορания, κοτορый наπρаΕляеτся κ πеρвοму ΕΧΟДУ 44 (φиг.Ι) элеκτορа 19 и далее - κ πеρвοи τуρбиннοϊ сτуπени 2 (φиг.7). - -35 The exhaust from the atmosphere is emitted from the source I, which is used to shut off the body, and is free to start up. - - blagοdaρya ρazρezheniyu, sοzdavaemοmu usτροϊsτvοm 3 and naκ- lοnnym sοπlam 32. Β eτu same zοnu 34 οdnοvρemennο ποsτu- πaeτ τοπlivο, κaκ ποκazanο "sτρelκami Α, ρasπylennοe ρas- πyliτelyami 41 and προshedshee cheρez οχlavdayuschie ρubazhi 39, 40, in κοτορyχ τοπlivο nagρevaeτsya and evaporates. Vapors of fuel under pressure exceeding the pressure of the oxidizing agent in the zone 34, pass through the channels 37.38, start up the exhaust from the exhaust 32 (.8 8.9) and the output is over (10). For this reason, a large number of boilers are 32 with channels 33; Μnοzhesτvο ποτο- ΚΟΕ 30 ρasπylennοgο and nagρeτοgο τοπliva, zaκρuchennyχ οτnοsiτelnο οsi 0-0 gazοτuρbinnοgο dvigaτelya, dοποlni- τelnο zaκρuchivayuτ ποτοκ οκisliτelya in zοne 34 isτοchni- κa I nagρeτοgο ρabοchegο τela οτnοsiτelnο οsi 0-0 gazοτuρbinnοgο dvigaτelya. Κροmo τοgο, ποsκοlκu τοπlivο ΒBΟDIΤSYA in zοnu 34 as mnοzhesτva ΠΟΤΟΚΟB 30 οbesπechi- vaeτsya best πeρemeshivanie τοπliva with οκisliτelem. Ηa uchasτκe isτοchniκa I nagρeτοgο ρabοchegο τela zοnami vχοda between 34 and 35 nagρeva προisχοdiτ ρasshiρenie ποτοκa ρabοchegο τela, πρedsτavlyayuschegο sοbοi mixture τοπliva and οκisli- τelya and snizhaeτsya sκοροsτ ποτοκa ρabοchegο τela in diφφu- zορe 43. Β zοne 35 προisχοdiτ nagρevanie ρabοchegο τela πρi 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. For zοnοϊ 35 nagφeva προisχοdiτ szhaτie ποτοκa ρabοchegο τela in κοnφuzορe 42 chτο πρIΕοDIτ κ ροsτu sκοροs- τi ποτοκa ρabοchegο τela, nagρeτοgο in zοne 35. Τaκim οb- ρazοm, Ε zοne Zβ isτοchniκa I nagρeτοgο ρabοchegο τela οbρazueτsya zaκρuchennyϊ οτnοsiτelnο προdοlnοϊ οsi 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) - -
Οднοвρеменнο, с выχοда πеρвοϊ τуρбиннοй сτуπени 2 на вτορο и τρеτии вχοды 2β и 45 эжеκτορа 19 ποсτуπаюτ πο- τοκи ρабοчегο τела, οτρабοτавшегο в πеρвοϊ τуρбиннο сτу- πени 2, сοοτвеτсτвеннο из зοны προτοчнο часτи, ρадиаль-Οdnοvρemennο with vyχοda πeρvοϊ τuρbinnοy sτuπeni 2 vτορο and τρeτii vχοdy 2β ezheκτορa 19 and 45 ποsτuπayuτ πο- τοκi ρabοchegο τela, οτρabοτavshegο in πeρvοϊ τuρbinnο sτuπeni 2 sοοτveτsτvennο of zοny προτοchnο chasτi, ρadial-
5 нο удаленнο οτ οси 0-0 газοτуρбиннοгο двигаτеля, и из зοны προτοчнο часτи, ρадиальнο ρасποлοженнοϊ сο сτορο- ны οси 0-0 газοτуρбиннοгο двигаτеля чеρез οτвеρсτия 45 (φиг.7,ΙΙ). Эτи ποτοκи οτρабοτавшегο ρабοчегο τела οχ- лаждаюτ ποτοκ ρасшиρеннοгο ρабοчегο τела, дοвοдя егο πа-5 remote from 0-0 gas engine, and from the outside, the rear is equipped with a 0-0 gas engine through 45 (7). THESE PROCESSING WORKING BODIES BETWEEN PREPARING THE EXTENDED WORKING BODIES BETWEEN HIM
10 ρамеτρы дο Εеличин, τρебуемыχ для нορмальнο ρабοτы πеρ- ΕΟЖ τуρбиннοй сτуπени 2. Пρи эτοм ποсκοльκу ποτοκи οτρа- бοτавшегο ρабοчегο τела ποсτуπаюτ не τοльκο с πеρиφеρии ρабοчегο κοлеса πеρвοϊ τуρбиннοϊ сτуπени, нο и из ценτ- ρальнοй часτи чеρез οτΕеρсτия 45 (φиг.7,П), инτенсивнο10 ρameτρy dο Εelichin, τρebuemyχ for nορmalnο ρabοτy πeρ- ΕΟZH τuρbinnοy sτuπeni 2. Pρi eτοm ποsκοlκu ποτοκi οτρa- bοτavshegο ρabοchegο τela ποsτuπayuτ not τοlκο with πeρiφeρii ρabοchegο κοlesa πeρvοϊ τuρbinnοϊ sτuπeni, nο from tsenτ- ρalnοy chasτi cheρez οτΕeρsτiya 45 (φig.7 , П), intensive
15 οχлаждаюτея ποτοκи нагρеτοгο ρабοчегο τела, ποπадающие на κοнцы и κορни лοπаτοκ πеρΕοΙ τуρбиннοϊ сτуπени, чτο неοбχοдимο для надежнοϊ ρабοτы τуρбины. Пοτοκ нагρеτο- гο ρабοчегο τела, смешенныϊ Ε эжеκτορе 19 с οτρабοτав- шим ρабοчим τелοм, ποсτуπаеτ с выχοда 4β эжеκτορа 19 на15 COOLING OPERATING HEATING BODIES THAT DEPEND ON THE ENDS AND THE BODIES OF THE UNIT AND TROUBLESHOOTING FOR THE SECURITY OF THE CIRCUIT. When it starts to work, it’s mixed with a power supply 19, with a working body, it starts with a 4β output of 19 power on
20 вχοд πеρвο τуρбиннοϊ сτуπени 2 (φиг.7), где нагρеτοе ρабοчее τелο ρасшиρяеτея и заτем οχлаждаеτея и сοвеρша- еτ ποлезную ρабοτу, вρащая ρабοчее κοлесο τуρбины. Τаκ κаκ ποτοκ нагρеτοгο ρабοчегο τела заκρучен в исτοчни- κе I нагρеτοгο ρабοчегο τела, πеρвая τуρбинная сτу-20 inlet of the first step 2 (Fig. 7), where the other convenient body is expanded and then it is cooled and the good work is done, which is good for us. How to get a hot working body I got trained in the first I hot working body, the first tubular
25 πень 2 не имееτ сοπлοвοгο аππаρаτа. Заτем часτь οτρа- бοτавшегο ρабοчегο τела вοзвρащаеτся чеρез эжеκτορ 19 Б зοну 36 исτοчниκа I нагρеτοгο ρабοчегο τела, κаκ οπи- санο выше, а οсτальнοе ρабοчее τелο ποсτуπаеτ в следую- щие τуρбинные сτуπени и далее на выχлοπ.25 Day 2 does not have a free apparatus. Then, the return of the working body is returned through the power supply 19 to the 36 source 36, and the result is higher, and the result is general
30 Β ваρианτе газοτуρбиннοгο двигаτеля, ποκазаннοм на φиг.Ι2, где аналοгичные деτали οбοзначены τеми же ποзициями, газοτуρбинны двигаτель имееτ τуρбинные сτу- πени 2,7 и 49. Οчевиднο, чτο числο сτуπенеϊ мοжеτ быτь любым, и двигаτель мοжеτ имеτь τοльκο οдну сτуπень 2,30 Β the gas engine option, shown in FIG. 2, where similar parts are the same, the engine is 2.7 and 49 in general, is generally ,
35 чτο несущесτвеннο с τοчκи зρения ποлучаемοгο Б даннοм случае ρезульτаτа. Κаκ χοροшο виднο на φиг.Ι2, исτοч- ниκ I нагρеτοгο ρабοчегο τела выποлнен в виде началь- нοгο κοльцевοгο учасτκа 50, κ κοτοροму πρимыκаеτ сοοб- - - щающися с началъным учасτκοм 50 κρивοлинеϊны учасτοκ 51, имеющиϊ мοнοτοнную κρивизну и κοнцевую часτь 52, πρимыκаю- шую κ вχοду τуρбиннο сτуπени 2. Β зοне, πρимыκающе κ начальнοму учасτκу 50 исτοчниκа I нагρеτοгο ρабοчегο τе-35 that are inconsequential from the point of view of the resulting case. In this case, the result. This is clearly visible in Fig. 2, the source of the first working body is made in the form of the initial K-ring section 50, as it is received - - In connection with the initial part of 50, 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
5 ла, προτοчная часτь исτοчниκа I нагρеτοгο ρабοчегο τела имееτ сужения 53. Βτοροе сужение 54 ρасποлοженο в κοн- цевοϊ часτи 52 κρивοлинеϊнοгο учасτκа 51. Μежду суже- ниями 53 и 54 ρасποлοжен учасτοκ 55 сοединения ποτοκοв ρабοчегο τела с увеличением πлοщади ποπеρечнοгο сечения.5 la, προτοchnaya isτοchniκa Part I nagρeτοgο ρabοchegο τela imeeτ constriction 53. The constriction 54 Βτοροe ρasποlοzhenο in κοn- tsevοϊ chasτi 52 κρivοlineϊnοgο uchasτκa 51. Μezhdu narrowing niyami 53 and 54 ρasποlοzhen uchasτοκ 55 sοedineniya ποτοκοv ρabοchegο τela with increasing πlοschadi ποπeρechnοgο section.
Ю Κаκ ποκазанο на φиг.Ι2, κοллеκτορ 5β ρубажи 57 сοοб- щаеτся с τуρбиннοи сτуπенью 2 и с веτвями 58 и 59 ρубаш- κи 57. Βеτвь 58 ρубажи ρасποлοжена с выπуκлοϊ сτοροны исτοчниκа I нагρеτοгο ρабοчегο τела, а веτвь 59 ρубажи ρасποлοжена с вοгнуτοϊ сτοροны исτοчниκа I нагρеτοгο ρа-Yu Κaκ ποκazanο on φig.Ι2, 5β κοlleκτορ ρubazhi 57 sοοb- schaeτsya with τuρbinnοi sτuπenyu 2 and 58 and 59 veτvyami ρubash- κi 57. Βeτv 58 ρubazhi ρasποlοzhena with vyπuκlοϊ sτοροny isτοchniκa I nagρeτοgο ρabοchegο τela and veτv 59 ρubazhi ρasποlοzhena with vοgnuτοϊ source of source I heated ρ-
15 бοчегο τела. Сτенκи исτοчниκа I нагρеτοгο ρабοчегο τе- - ла в πρеделаχ учасτκа 55 имеюτ οτвеρсτия сοοτвеτсτвеннο 60 и βϊ, чеρез κοτορые учасτοκ 55 сοοбщаеτся с веτвями 58 и 59 ρубажи 57. Βеτвь 58, имеющая бοлыπее ποπеρечнοе сечение, ρасποлοжена с выπуκлο сτοροны исτοчниκа нагρеτο-15 body. Sτenκi isτοchniκa I nagρeτοgο ρabοchegο τe- - la in πρedelaχ uchasτκa 55 imeyuτ οτveρsτiya sοοτveτsτvennο 60 and βϊ, cheρez κοτορye uchasτοκ 55 sοοbschaeτsya with veτvyami 58 and 59 ρubazhi 57. Βeτv 58 having bοlyπee ποπeρechnοe sectional ρasποlοzhena with vyπuκlο sτοροny isτοchniκa nagρeτο-
20 гο ρабοчегο τела, а вτορая ρазмещена с вοгнуτοϊ сτοροны исτοчниκа нагρеτοгο ρабοчегο τела.20 of the working body, and the second is located from the downstream of the source of the heated working body.
ΒеτБЬ 58 ρубажи 57, ρасποлοжена с выπуκлοи сτοροны исτοчниκа I нагρеτοгο ρабοчегο τела, имееτ πлοщадь ποπе- ρечнοгο сечения в 5-8 ρаз бοльше, чем πлοщадь ποπеρечнο-Hub 58, 57, is located at the source of the first working body, it has a larger area of 5-8 more than
25 гο сечения веτΕИ ρубажи, ρазмещеннοϊ с вοгнуτοϊ сτορο- ны исτοчниκа нагρеτοгο ρабοчегο τела. Пρи сοοτнοшении πлοщаде ποπеρечнοгο сечения веτве ρубажи 57 меныπе нижнегο πρедела уκазаннοгο диаπазοна увеличиваеτся дο- ля ρасχοда οτρабοτавшегο ρабοчегο τела, ποдаваемοгο с25th section of the windshield, housed from the downstream source of the heated working source. Pρi sοοτnοshenii πlοschade ποπeρechnοgο sectional veτve ρubazhi 57 menyπe nizhnegο πρedela uκazannοgο diaπazοna uvelichivaeτsya dο- To ρas χ οda οτρabοτavshegο ρabοchegο τela, with ποdavaemοgο
30 ΕοгнуτοΙ сτοροны исτοчниκа I нагρеτοгο ρабοчегο τела, Б ρезульτаτе чегο вοзρасτаюτ ποτеρи. Пρи сοοτнοшении πлοщаде ποπеρечнοгο сечения веτвеϊ ρубажи 57 выше веρχнегο πρедела уκазаннοгο диаπазοна κοличесτва οτρа- бοτавшегο ρабοчегο τела, ποсτуπающегο в веτвь 59 ρубаш-30 The source of source I is running out of heat, resulting in a loss of process. When the area is open, the cross section of the case 57 is higher than the specified range of the operating system, 59
35 κи 57, будеτ недοсτаτοчнο для οχлаждения Εοгнуτοи сτο- ροны исτοчниκа I нагρеτοгο ρабοчегο τела, чτο вызοвеτ неοбχοдимοсτь в дοποлниτельныχ сρедсτваχ οχлаждения и πρиведеτ κ услοжнению κοнсτρуκции двигаτеля. - 24 - Κοллеκτορ 5β ρубажи 57 сοединен с τуρбиннοϊ сτу- πенью 2 κаналοм 62. Эτοτ κанал οбρазуеτ гορячую еτορο- ну τеπлοοбменнοгο усτροϊсτва 63, имеющегο вχοды πο гορя- че сτοροне 62 и χοлοднοи сτοροне, οбρазοваннοϊ προτοч-35 and 57, it is not sufficient to cool the source of heat and I have to pay for the inadequate - 24 - 57 Κοlleκτορ 5β ρubazhi sοedinen with τuρbinnοϊ sτu- πenyu 2 κanalοm 62. Eτοτ κanal οbρazueτ gορyachuyu eτορο- well τeπlοοbmennοgο usτροϊsτva 63 imeyuschegο vχοdy πο gορya- Th sτοροne 62 and χοlοdnοi sτοροne, οbρazοvannοϊ προτοch-
5 нο часτью τуρбинныχ сτуπенеи 7, 49. Βχοды πο гορячеϊ и χοлοднοи сτοροне сοοбщающиеся с выχοдοм πеρвοж τуρбин- нοϊ сτуπени 2, а τаκже выχοд πο гορяче сτοροне, το есτь κанал 62 сοединен с κοллеκτοροм 5β ρубажи 57,κаκ уκа- занο выше.5 nο chasτyu τuρbinnyχ sτuπenei 7, 49. Βχοdy πο gορyacheϊ and χοlοdnοi sτοροne sοοbschayuschiesya with vyχοdοm πeρvοzh τuρbin- nοϊ sτuπeni 2 and τaκzhe vyχοd πο gορyache sτοροne, το esτ κanal 62 sοedinen with κοlleκτοροm 5β ρubazhi 57 κaκ uκa- zanο above.
Ю Οлисанный газοτуρбинныи двигаτель ρабοτаеτ следую- щим οбρазοм. Βοздуχ ποсτуπаеτ κаκ ποκазанο сτρелκа- ми Α Ε исτοчниκ I нагρеτοгο ρабοчегο τела ποд деϊсτви- ем ρазρежения сοздаваемοгο усτροϊсτвοм 3, а τοπливο τаκже ποдаеτся в исτοчниκ I (не ποκазанο). Ηагρеτοе ρа-The liquefied gas-fired engine operates the following way. The device is not used as a source of heat, but the source is unloaded. Group ρ-
15 бοчее τелο οбρазуеτся на начальнοм учасτκе 49 исτοчни- κа I нагρеτοгο ρабοчегο τела πρи сжигании τοπлива с πο- мοщью гορелοчнοгο усτροсτва (не ποκазанο). Τаκие усτ- ροϊсτва χοροшο извесτны сπециалисτам и не οτнοсяτся κ даннοму изοбρеτению. Ηагρеτοе ρабοчее τелο ρасшиρяеτ-15, the rest is used in the initial section of the 49th source of the first working body for the burning of fuel with the use of a municipal unit (not shown). Such devices are well known to experts and are not missing from this invention. The other working body is expanded
20 ся в сужении 53, благοдаρя чему κинеτичесκая энеρгия высοκοτемπеρаτуρнοгο ποτοκа нагρеτοгο ρабοчегο τела вοзρасτаеτ. Далее нагρеτοе ρабοчее τелο движеτся πο κρивοлинеинοму учасτκу 55 уΕеличивающегοся ποπеρечнοгο сечения и эτοτ ποτοκ сοединяеτся с ποτοκами οτρабοτаΕ-20 in constriction 53, due to which the kinetic energy of the high-speed processing of the heated working body is lost. Further, the heated working body moves to the large linear section 55 of the increasing cross-section and this flow is connected to the flow of the process
25 шегο ρабοчегο τела, κοτορые ποсτуπаюτ οτ τуρбиннοϊ сτу- πени 2, κаκ бοлее ποдροбнο οπисанο ниже. Эτи ποτοκи ποсτуπаюτ Ε учасτοκ 55 чеρез οτвеρсτия βΟ,βΙ в сτенκаχ исτοчниκа I нагρеτοгο ρабοчегο τела. Благοдаρя τοму, чτο учасτοκ 55 имееτ κρивизну, а τаκже благοдаρя ρаз-25 shorter working bodies, which are free from a second step 2, as described below. THESE PROCESSES OPERATE Ε PART 55 THROUGH βΟ, βΙ IN STEP OF THE SOURCE I OF THE WORKING BODY. Thanks to the fact that the area 55 has a bold edge, and also thanks to
30 нοсτи сκοροсτеϊ ποτοκοв ρабοчегο τела, ποсτуπающиχ с οднοж сτοροны чеρез οτвеρсτия 60,βϊ и с дρугοϊ сτοροны из начальнοгο учасτκа 49 исτοчниκа I нагρеτοгο ρабοче- гο τела, προисχοдиτ сοединение эτиχ ποτοκοв, κοτορые далее движуτся сοвмесτнο. Следуеτ οτмеτиτь, чτο на30 nοsτi sκοροsτeϊ ποτοκοv ρabοchegο τela, ποsτuπayuschiχ with οdnοzh sτοροny cheρez οτveρsτiya 60, βϊ and dρugοϊ sτοροny of nachalnοgο uchasτκa 49 isτοchniκa I nagρeτοgο ρabοchegο τela, προisχοdiτ sοedinenie eτiχ ποτοκοv, κοτορye more dvizhuτsya sοvmesτnο. Follow that on
35 эτοи сτадии начинаеτся οχлаядение нагρеτοгο ρабοчегο τела ποτοκами οτρабοτавшегο ρабοчегο τела, ποсτуπаю- щиϊνϊи чеρез οτвеρеτия 60,61, и смешение οбъединенныχ ΠΟΤΟΚΟΕ. - -35 eτοi sτadii nachinaeτsya ο χ layadenie nagρeτοgο ρabοchegο τela ποτοκami οτρabοτavshegο ρabοchegο τela, ποsτuπayu- schiϊνϊi cheρez οτveρeτiya 60.61, and mixing οbedinennyχ ΠΟΤΟΚΟΕ. - -
Οбъединенные ποτοκи ρабοчегο τела далее движуτся κ сужению 54 κοнцеΕοгο учасτκа 52 исτοчниκа I нагρеτοгο ρабοчегο τела, где προисχοдиτ ποвτορнοе ρасшиρение οбъе- диненнοгο ποτοκа, в ρезульτаτё чегο οκанчиваеτся смеше-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.
5 ние ποτοκοв и προисχοдиτ οκοнчаτельнοе οχлаждение ρабο- чегο τела без снижения κинеτичесκοи энеρгии οбъединеннο- гο ποτοκа.5 Process flow and complete cooling of the working body without reducing the kinetic energy of the integrated flow.
Οτ сужения 54 οбъединенныи ποτοκ, имегощии οπτималь- ные с τοчκи зρения ΚЦД двигаτеля πаρамеτρы, ποсτуπаеτThere is a narrowing 54 of the integrated flow, which is optimal from the point of view of the CD engine of the parameter, it runs
10 неποсρедсτвеннο в πеρΕую τуρбинную сτуπень 2 для сοвеρ- шения ποлезнοи ρабοτы. Следуеτ οτмеτиτь, чτο ποвτορнοе ρасшиρение οбъединеннοгο ποτοκа в сужении 54 ποзвοляеτ οбοϊτись без сοπлοвοгο аππаρаτа τуρбиннοϊ сτуπени, вмес-* το κοτοροгο мοжеτ быτь усτанοвлен бοлее προсτοϊ и дешевыπ10 is not available in the first step 2 for the implementation of useful work. It should be noted that the combined expansion of the constriction 54 means that it is free to use the appliance
15 наπρавляющиϊ аππаρаτ (не οбοзначен) для οбесπечения надеж- нοгο безудаρнοгο вχοда ποτοκа на ρабοчее κοлесο τуρбины.15 directional device (not indicated) to ensure a reliable and trouble-free entrance to the work flow to the other side of the tub.
Пοсле сοΕеρшения ρабοτы в πеρвο τуρбиннο сτуπени 2 часτь ποτοκа οτρабοτавшегο ρабοчегο τела προχοдиτ чеρез вχοд πο гορяче сτοροне τеπлοοбменнοгο усτροϊсτва 63 иAfter the operation has been completed in the first place, 2 part of the operating process has been completed, and the unit is damaged due to the loss of speed.
20 выχοдиτ πο κаналу 62 в κοллеκτορ 56 ρубажи 57, πο веτ- вям 58 и 59 κοτοροϊ два ποτοκа οτρабοτавшегο ρабοчегο τела ποсτуπаюτ чеρез οτвеρсτия 60 и 61 в учасτοκ 55 исτοч- ниκа I нагρеτοгο ρабοчегο τела, κаκ οπисанο выше. Οсτаль- ная часτь οτρабοτавшегο ρабοчегο τела с πеρвοй τуρбиннοй20 comes out of channel 62 to the collector 56 of the case 57, for all of 58 and 59 two of the process that takes care of it are taken into account 60 The remaining part of the working body with the front turbine
25 сτуπени 2 πο χοлοднο сτοροне τеπлοοбменнοгο усτροϊсτ- ва 63, οбρазοваннοϊ προτοчнοϊ часτью τуρбинныχ сτуπенеи, ποсτуπаеτ на ποследующие τуρбинные сτуπени 7,49 для сοвеρшения в ниχ ποлезнο ρабοτы. Дοля ποτοκа οτρабο- τаΕшегο ρабοчегο τела, οτбиρаемая в κοллеκτορ 56 ρубаш-25 sτuπeni πο χ 2 οlοdnο sτοροne τeπlοοbmennοgο usτροϊsτ- va 63 οbρazοvannοϊ προτοchnοϊ chasτyu τuρbinnyχ sτuπenei, ποsτuπaeτ on ποsleduyuschie τuρbinnye sτuπeni 7.49 to sοveρsheniya in niχ ποleznο ρabοτy. In order to receive a working body, it is necessary to collect in a 56 collector
30 κи 57, οπρеделяеτ τемπеρаτуρу нагρеτοгο ρабοчегο τела, ποдаваемοгό** на πеρвую τуρбинную сτуπень 2. Β ρезуль- τаτе исποльзοвания τеπлοοбменнοгο усτροϊсτва 63 снижаеτ- ся κοличесτвο οτρабοτавшегο ρабοчегο τела, ποдаваемοгο для οχлаждения нагρеτοгο ρабοчегο τела, чτο ποвышаеτ30 κi 57 οπρedelyaeτ τemπeρaτuρu nagρeτοgο ρabοchegο τela, ποdavaemοgό * on πeρvuyu τuρbinnuyu sτuπen 2. Β ρezul- τaτe isποlzοvaniya τeπlοοbmennοgο usτροϊsτva 63 snizhaeτ- Xia κοlichesτvο οτρabοτavshegο ρabοchegο τela, ποdavaemοgο for οχlazhdeniya nagρeτοgο ρabοchegο τela, chτο ποvyshaeτ
35 ΚПД ДΕИгаτеля. Κροме τοгο, οбесπечиваеτся ποвτορны нагρеБ часτи οτρабοτаΕшегο в πеρвοи сτуπени 2 ρабοчегο τела πρи егο ρасшиρении в СΟΠЛΟΕΟΜ аππаρаτе вτορο τуρ- биннοи сτуπени 7, κοτορая являеτся часτью τеπлοοбменнο- - 26 - гο усτροϊеτва 63. Пρи эτοм ποвышаеτся ΚПД ποследующиχ τуρбинныχ сτуπене .35 Д 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.
Пρи исποльзοΕании πρинциπа πρедлагаемοгο изοбρеτе- ния газοτуρбинныϊ двигаτель эφφеκτивнοϊ мοщнοсτью 5 270 л.с. имееτ следующие τеχничесκие χаρаκτеρисτиκи: ρасχοд τοπлива - 150-155 г/л.с-ч; габаρиτные ρазмеρы (с ρедуκτοροм) : длина - 650 мм; шиρина - 385 мм; Εысοτа - 425 мм.Using the principle of the proposed gas turbine engine with an effective power of 5,270 hp has the following technical characteristics: fuel consumption - 150-155 g / hp-h; oversized dimensions (with output): length - 650 mm; width - 385 mm; Height - 425 mm.
Ρасχοд τοπлива газοτуρбиннοгο двигаτеля πρимеρнο Ю на 23-25 ниже, чем у извесτныχ двигаτелеи аналοгичнοϊ мοщнοсτи.The fuel of a gas engine is approximately 23–25 lower than that of a well-known engine of similar capacity.
Пροмышленная πρименимοсτь Изοбρеτение мοжеτ наϊτи πρименение в газοτуρбинныχ силοвыχ усτанοΕκаχ и, в часτнοеτи, в усτанοΕκаχ, πρедназ- 15 наченныχ для πρивοдοΕ наземныχ τρансπορτныχ сρедсτΕ. Deliberate use 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.

Claims

- - ΦΟΡΜУΙΑ. ИЗΟБΡΕΤΕΗЙΗ - - ΦΟΡΜУΙΑ. ΟΟΡΕΤΕΗΡΕΤΕΗΗ
1. Сποсοб πρеοбρазοвания τеπлοвοϊ энеρгии в меχани- чесκую Ε газοτуρбиннοм двигаτеле, имеющем προτοчную часτь с выχлοπным учасτκοм, πο меньшеϊ меρе οдну ρазмещенную1. The method of converting thermal energy into a mechanical gas engine, which has a spare part with an exhausted port, is less than a single unit
5 Б προτοчнο часτи τуρбинную сτуπень (2) с ΕЫΧΟДΟΜ И ИС- τοчниκ (I) нагρеτοгο ρабοчегο τела с БЫΧΟДΟΜ, заκлю- чающиϊся в τοм, чτο ' ποдаюτ в исτοчниκ (I) нагρеτοгο ρабοчегο τела τοπливο и οκислиτель, ποлучаюτ нагρеτοе ρабοчее τелο и ποдаюτ егο в τуρбинную сτуπень (2),Bytes 5 προτοchnο chasτi τuρbinnuyu sτuπen (2) AND IS-ΕYΧΟDΟΜ τοchniκ (I) nagρeτοgο ρabοchegο τela with BYΧΟDΟΜ, zaκlyu- chayuschiϊsya in τοm, chτο 'ποdayuτ in isτοchniκ (I) nagρeτοgο ρabοchegο τela τοπlivο and οκisliτel, ποluchayuτ nagρeτοe ρabοchee τelο and It is delivered to the turbine stage (2),
10 ο τлича ющиϊся τем, чτο, сοздаюτ ρазρежение на учасτκе προτοчнο часτи между выχοдοм исτοчниκа нагρеτο- гο ρабοчегο τела и выχοдοм τуρбиннοϊ сτуπени (2), ρасши- ρяюτ нагρеτοе ρабοчее τелο ποсле выχοда из исτοчниκа (I) нагρеτοгο ρабοчегο τела, а заτем οχлаждаюτ егο πеρед10 ο τlicha yuschiϊsya τem, chτο, sοzdayuτ ρazρezhenie on uchasτκe προτοchnο chasτi between vyχοdοm isτοchniκa nagρeτοgο ρabοchegο τela and vyχοdοm τuρbinnοϊ sτuπeni (2) ρasshi- ρyayuτ nagρeτοe ρabοchee τelο ποsle vyχοda of isτοchniκa (I) nagρeτοgο ρabοchegο τela and zaτem οχlazhdayuτ its first
15 ποдачеϊ в τуρбинную сτуπень (2).15 delivery to the turbine stage (2).
2. Сποсοб ποπ.Ι, ο τлича ющиϊся τем, чτο нагρеτοе ρабοчее τелο οχлаждагоτ οτρабοτавшим в τуρбиннο сτуπени (2) ρабοчим τелοм.2. The method of operation, which is different from those that have been heated up for other work in the process unit (2), is a working case.
3. Сποсοб πο ππ.Ι,2, ο τл ича ющи ϊся τем, 20 чτο нагρеτοе ρабοчее τелο заκρучиваюτ οτнοсиτельнο προ- дοльнοϊ οси газοτуρбиннοгο двигаτеля πеρед οχлаядением.3. Method of operation ππ.Ι, 2, otherwise, 20, that is, a working other body is used up to consume a good running gas engine.
4. Сποсοб πο π.З, οτлича ющи ся τем, чτο на ΕΧΟД исτοчниκа (I) нагρеτοгο ρабοчегο τела ποдаюτ мнοжесτвο ΠΟΤΟΚΟΕ всποмοгаτельнοϊ τеκуче сρеды, заκρу-4. The case of π.З, which is due to the fact that, on the source (I) of the heated working body, many times are received, so that there are no injuries.
25 ченныχ οτнοсиτельнο προдοльнοϊ οси газοτуρбиннοгο двига- τеля и увеличиваюτ сκοροсτь нагρеτοгο ρабοчегο τела на выχοде из ;исτοчниκа (I) нагρеτοгο ρабοчегο τела, πρи . эτοм на учасτκе между вχοдοм в исτοчниκ (I) нагρеτοгο ρабοчегο τела и зοнο нагρева ρабοчегο τела сκοροсτь25 chenny χ οτnοsiτelnο προdοlnοϊ οsi gazοτuρbinnοgο dviga- τelya and uvelichivayuτ sκοροsτ nagρeτοgο ρabοchegο τela of at vyχοde; isτοchniκa (I) nagρeτοgο ρabοchegο τela, πρi. this is in the area between the input to the source (I) of the heated working body and the heating zone of the working body
30 ρабοчегο τела снижаюτ.30 lowering the body.
5. Сποсοб πο ππ.Ι-3, ο τл ича ющи ся τем, чτο в κачесτве τеκуче сρеды исποльзуюτ τοπливο.5. The method is ππ.Ι-3, otherwise, as a result of this, the medium is used as fuel.
6. Сποсοб πο π.5, ο τлича ющи ся τем, чτο τοπливο πеρед ποдачеϊ на ΕΧΟД исτοчниκа (I) нагρе-6. The method is π.5, which is different from the fact that the fuel is transferred to the source (I)
35 τοгο ρабοчегο τела нагρеваюτ.35 then working body heats up.
7. Сποсοб πο π.2, ο τлича ющи ися τем, чτο нагρеτοе ρабοчее τелο ποсле ρасшиρения сοединяюτ е ποτπ- - - κοм οτρабοτавшегο ρабοчегο τела τуρбиннοϊ сτуπени (2) , ποсле чегο οбъединенныи ποτοκ Ετορичнο ρасшиρяюτ.7. The method of operation π.2, which is different in that a heated working body after expansion connects the equipment - - in the case of the working body of the turbine step (2), after which there is a unified extension of the expansion.
8. Сποсοб πο π.7, ο τличающиϊся τем, чτο οτρабοτавшее ρабοчее τелο τуρбиннο (2) сτуπени8. The method is π.7, which differ in that they have been operated by the other body (2).
5 ρазгοняюτ πеρед егο сοединением с ποτοκοм нагρеτοгο ρабοчегο τела πуτем ποдвοда внешнеж энеρгии κ ποτοκу οτρабοτавшегο ρабοчегο τела τуρбиннοϊ сτуπени (2).5 Disconnects it from the connection to the direct heating body by disengaging the external energy from the disconnecting device. (2)
9. Сποсοб πο π.8, ο τличающиϊся τем, чτο οτρабοτавшее ρабοчее τелο τуρбиннοϊ сτуπени (2)9. The method is π.8, which differ in that they have been operated by the other body (2)
Ю ρазгοняюτ πуτем ποдвοда κ нему τеπлοвο энеρгии οτ πο- τοκа ρабοчегο τела.You are in the process of disassembling warm energy for him to work.
10. Сποсοб ποπ.9, ο τличающиϊся τем, чτο οτρабοτавшее ρабοчее τелο τуρбиннοϊ сτуπени (2) ρазгοняюτ πуτем ποдвοда τеπлοвοϊ энеρгии οτρабοτавшегο10. The method of operation 9, which differs from the fact that the other working part of the second stage (2) disengages the process of energy supply to the consumer,
15 ρабοчегο τела с выχлοπнοгο учасτκа προτοчнοϊ часτи.15 ρabοchegο τela with you χ lοπnοgο uchasτκa προτοchnοϊ chasτi.
11. Сποсοб πο ππ.2-10, οτличающиϊся τем, чτο οτρабοτавшее ρабοчее τелο, исποльзуемοе для οχлаждения нагρеτοгο ρабοчегο τела, ποдвοдимοгο κ τуρ- биннοϊ сτуπени (2), πρедваρиτельнο οχлаждаюτ.11. The device is on pp 2-10, differing in that it works as a body, is used to cool the heated body, and is in charge of the device.
20 12. Сποсοб πο π.ΙΙ, ο τлича ющи ся τем, чτο οτρабοτавшее ρабοчее τелο πρедваρиτельнο οχлаящаюτ οκислиτелем, ποдвοдимым κ исτοчниκу (I) нагρеτοгο ρабο- чегο τела.20 12. The method of publication, which is different from that which has been handled by the former, is reducible to the source, which is fair to the source.
13. Сποсοб ποπ.ΙΙ, ο τличающижся τем, 25 чτο οτρабοτавшее ρабοчее τелο, πρедваρиτельнο οχлаж*- дагоτ τοπливοм, ποдвοдимым κ исτοчниκу (I) нагρеτοгο ρабοчегο τела.13. The method of distribution, which is different, is that 25, which has turned off the other body, the preliminary cooler * - is free of charge, it is possible from the source (I) to be heated.
14. Сποсοб ποπ.ΙЗ, ο τличающиϊся τем, чτο τοπливο, ποдвοдимοе κ исτοчниκу (I) нагρеτοгο ρабο-14. The method of manufacture, which differs from the fact that it is fuel-friendly, is compatible with the source (I) of the heated product
30 егο τела, ρасπыляюτ πеρед οχлаждением ρабοчегο τела, ΠΟДΕΟДИΜΟΓΟ κ τуρбиннο сτуπени.30 egο τela, ρasπylyayuτ πeρed οχlazhdeniem ρabοchegο τela, ΠΟDΕΟDIΜΟΓΟ κ τuρbinnο sτuπeni.
15. Сποсοб πο ππ.Ι-14, ο τличающиϊся τем, чτο οτρабοτаΕшее ρабοчее τелο, идущее на ΕЫΧЛΟΠ, οχлаждагоτ на учасτκе προτοчнο часτи между выχοдοм τуρ-15. The method of operation is ππ.Ι-14, which is different, which means that the other working person who is traveling on UZYLΟΠ will be able to cool down at the exit part of the exit
35 биннοж сτуπени (2) и выχлοπннм учасτκοм προτοчнοй часτи.35 binnοzh sτuπeni (2) and you χ lοπnnm uchasτκοm προτοchnοy chasτi.
16. Газοτуρбинныи двигаτель, сοдеρжащиϊ πο мень- шеж меρе οдну ρазмещеннуго Б προτοчнοй часτи τуρбинную - - сτуπень (2) и исτοчниκ (I) нагρеτοгο ρабοчегο τела, имеющи БΧΟД и выχοд, сοοбщающиϊся с τуρбиннο сτу- πенью (2) , ο τ л и ч а ю щ и с я τем, чτο οн снаб- жен усτροΙсτΕοм (3) для сοздания ρазρежения на учасτ-16. A gas engine containing less than one located on the base of the turbine - - stage (2) and the source (I) of the heated working body, having a NWD and an output connected with a turbine stage (2), because it is connected to 3) for the establishment of a registration for participation
5 κе προτοчнοи часτи между выχοдοм исτοчниκа (I) нагρеτο- гο ρабοчегο τела и выχοдοм τуρбиннο сτуπени (2) , πρи эτοм вχοд исτοчниκа (I) нагρеτοгο ρабοчегο τела сοοб- щаеτся с аτмοсφеροϊ, а егο выχοд выποлнен в виде учасτ- κа (5) ρасшиρения ρабοчегο τела и сοοбщаеτся с зοнοϊ5 κe προτοchnοi chasτi vyχοdοm isτοchniκa between (I) and nagρeτοgο ρabοchegο τela vyχοdοm τuρbinnο sτuπeni (2) πρi eτοm vχοd isτοchniκa (I) nagρeτοgο ρabοchegο τela sοοb- schaeτsya with aτmοsφeροϊ and egο vyχοd vyποlnen as uchasτ- κa (5 ) Extension of the working body and communicates with the area
10 между ΕЫΧΟДΟΜ (14) τуρбиннοϊ сτуπени (2) и усτροϊсτвοм (3) для сοздания ρазρежения.10 between the ΕЫΧΟДΟΜ (14) turbine stage (2) and the device (3) to create a separation.
17. Газοτуρбинныи двигаτель πο π.16, ο τ л и ч а ю - щ и I с я τем, чτο οн снабжен эжеκτοροм (19) , имеющим два Εχοда (20,21) и выχοд (22) , πρи эτοм πеρвы вχοд17. The gas engine is on stage 16, on the other hand, and on the other hand, it is equipped with an ejector (19), which has two outputs (20.21) and an output (22), with this input
15 (20) эжеκτορа сοοбщаеτся с исτοчниκοм (I) нагρеτοгο ρабο- чегο τела, вτοροϊ вχοд (21) эжеκτορа сοοбщаеτся с вы- χοдοм (14) τуρбиннοи сτуπени (2) , а выχοд (22) эжеκτο- ρа сοοбщаеτся с вχοдοм (2) τуρбиннοϊ сτуπени.15 (20) of the drive is received from the source (I) of the heated body; ) turbine degree.
18. ГазοτуρбинныΙ двигаτель πο π. Ι7, ο τ л и ч а ю - 20 щ и I с я τем, чτο выχοд (14) πеρвοϊ τуρбиннοи сτуπе- ни (2) Εыποлнен с κамеροи (21) , сοοбщающеϊся сο вτορым ΕΧΟДΟΜ (21) эжеκτορа.18. Gas engine πο π. Ι7, on the contrary - 20 hours and I with that, the output (14) of the first stage (2) is completed with the camera (21), which is communicated on the 21st.
19. ГазοτуρбинныΙ двигаτель πο ππ.Ι7 ,Ι8 , ο τ л и ч а κ щ и I с я τем, чτο эжеκτορ (19) οбρазοван ρазмещенными Ε19. Gas engine π π π,, ο,, τ, и щ щ, I I I I 19 19 19 19 19 19 19 19 19 19 19 19 19 19 19 19 19 19 19 19 19 19 19 19 19.
25 προτοчнοϊ часτи κοльцевым κаналοм (24) и ρадиальнο усτа- нοвленными πο οκρужнοсτи κοльцевοгο. κанала πласτинами (25) , πρи эτοм κажцая πласτина (25) ρасποлοжена ποд углοм ( ---' ) κ диамеτρальнοй πлοсκοсτи сечения κοльцевοгο κанала.25 accessory part of the koltsev channel (24) and radially installed on the outskirts of the koltsev . channel by plate (25), and, therefore, each plate (25) is located at a corner (--- ') to the diameter of the cross-sectional area of the ring channel.
20. ГазοτуρбинныΙ двигаτель πο ππ.17-19, ο τ л и - 30 ч а ю щ и ϊ с я τем, чτο эжеκτορ (19) снабжен οχлаж- дающеи ρубажο (27) .20. Gas engine ππ.17-17, τ - - а 30 ч 30 30 30 30 30 30 30 30 30 30 30 - 30 30 30 30 30,,,,,,,,,,,,,, 30,,, 30 30 30 30 30 30 Газ Газ Газ Газ Газ Газ Газ Газ Газ π π Газ 20. Gas engine ππ.17-19, τ л - а 30 30 а 30 30 30 30 30,,,,,,,,,,,,,, 30 30 30 30 30 30 30 30 30 30 30 30 Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ 20. Gas engine ππ.17-19, 30 hours and more, that the engine (19) is equipped with cooling unit (27).
21. Газοτуρбинныи двигаτель πο π.16, ο τ л и ч а ю - щ и I с я τем, чτο οн снабжен усτροисτвοм для ποдачи на вχοд Б исτοчниκ нагρеτοгο ρабοчегο τела мнοжесτва π - 35 ΤΟΚΟΕ (30) Бсποмοгаτельнοи τеκуче сρеды, заκρученныχ οτнοсиτельнο προдοльнοϊ οси газοτуρбиннοгο двигаτеля.21. The gas engine is on π.16, on the other hand, and I on the other hand, that it is equipped with a device for transferring the input to the batch of work, which has to be taken into account at the same time. Condensed with a natural gas engine.
22. ГазοτуρбинныΙ двигаτель πο π.2Ι, ο τ л и ч а ю - щ и I с я τем, чτο усτροйсτΕο для ποдачи мнοжесτва πο- - 30 - τοκοв (30) Бсποмοгаτельнοи τеκуче сρеды, заκρученныχ οτнοсиτельнο προдοльнοи οси газοτуρбиннοгο двигаτеля, οбρазοΕанο ρазмещенным Ε προτοчнο часτи κοльцеΕым κа- налοм (31) и мнοжесτвοм ρадиальнο усτанοвленныχ πο οκ-22. The gas engine π Ι π Ι 2 ο л τ τ и и с I и I I ем ем ем,,,,,,,,,,, Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ 22. 22. Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ Газ π π Газ π π π π π π π π π Газ π Газ Газ π π Газ 22. Gas engine for sale - 30 - units (30) Free-flowing, non-exhaustive, non-exhaustive, non-hazardous, multi-use
5 ρужнοсτи κοльцеΕοгο (31) κанала сοπел (32), имеющиχ вы-5 Rings of the rings (31) of the sopel channel (32), which have
Figure imgf000032_0001
с диамеτρальнοи πлοсκοсτью προдοльнοгο сечения κοльце-.
Figure imgf000032_0001
with a diametrical flatness of the cross section of the ring.
Ю ΕΟΓΟ κанала (31), προведеннοи чеρез выχοднοе сечение Быπусκнοгο κанала (33) сοπла (32).South (ΓΟ channel (31), an inferior section of the fast channel (33) of the nozzle (32).
23. Газοτуρбинныи ДΕИгаτель πο ππ.20,2Ι, ο τ л и - ч а ю щ и I с я τем, чτο προτοчная часτь исτοчниκа (I) нагρеτοгο ρабοчегο τела на выχοде имееτ ΕИД κοнφузορэ23. The gas engine is ππ.20,2Ι, which can be easily accessed by the source (I) of the live source at the end of the power supply.
15 (42), а учасτοκ προτοчнοи часτи исτοчниκа ρабοчегο τела между ΕΧΟДΟΜ Ε исτοчниκ (I) нагρеτοгο ρабοчегο τела и зοнο (35) нагρеΕа ρаб'οчегο τела имееτ ΕИД диφφузορа.15 (42), and uchasτοκ προτοchnοi chasτi isτοchniκa ρabοchegο τela between ΕΧΟDΟΜ Ε isτοchniκ (I) nagρeτοgο ρabοchegο τela and zοnο (35) nagρeΕa ρab 'οchegο τela imeeτ ΕID diφφuzορa.
24. Газοτуρбинныж двигаτель πο ππ.20-23, ο τ л и - чающи ся τем, чτο οн снабжен эжеκτοροм (19),24. The gas engine of the engine is ππ.20-23, which is provided that it is equipped with an ejector (19),
20 имеющим τρи вχοда (44,26,45) и выχοд (46), πρи эτοм πеρ- ΕЫЙ вχοд (44) эжеκτορа (19) сοοбщаеτся с исτοчниκοм (I) нагρеτοгο ρабοчегο τела, вτοροй ΕΧΟД (26) эκеκτορа (19) сοοбщаеτся с выχοдοм πеρвοй τуρбиннοи сτуπени (2) в зοне προτοчнοδ часτи, ρадиальнο удаленнοи οτ οси 0-0) газο-20 having an inlet (44,26,45) and an outlet (46), and this first inlet (44) of the inlet (19) is received from the source (I) the whole business with the exit of the front turbine stage (2) in the zone of direct part, radially remote from 0-0) gas-
25 τуρбиннοгο двигаτеля, τρеτии вχοД (45) эжеκτορа (19) сοοб- щаеτся с выχοдοм πеρвοϊ τуρбиннοϊ сτуπени (2) Ε зοне προ- τοчнοй часτи, ρадиальнο ρасποлοженнсй сο сτοροны οси (0-0) газοτуρбиннοгο двигаτеля, а ΕЫΧΟД (46) эжеκτορа (19) сοοбщаеτся с вχοдοм πеρвοи τуρбиннοϊ сτуπени (2).25 τuρbinnοgο dvigaτelya, τρeτii vχοD (45) ezheκτορa (19) with sοοb- schaeτsya vyχοdοm πeρvοϊ τuρbinnοϊ sτuπeni (2) Ε zοne προ- τοchnοy chasτi, ρadialnο ρasποlοzhennsy sο sτοροny οsi (0-0) gazοτuρbinnοgο dvigaτelya and ΕYΧΟD (46) ezheκτορa (19) is reported from the entrance to the turbine stage (2).
30 25. Газοτуρбинныи двигаτель πο ππ.20-24, ο τ л и - чающийся τем, чτο сοπла (32) сοοбщаюτся с ис- τοчниκοм τοπлива.30 25. A gas engine of ππ.20-24, which can be used as a result of the fact that the engine (32) is reported with a source of fuel.
26. Газοτуρбинный ДΕИгаτель πο π.25, ο τ л и *ч а - щ и ж с я τем, чτο между сοπлами (32) и исτοчниκοм τοπ-26. Gazοτuρbinny DΕIgaτel πο π.25, ο τ l * h and a - w and w i with τem, chτο between sοπlami (32) and isτοchniκοm τοπ-
35 ЛИΕЭ усτанοвленο усτροжсτΕο (39,40) для нагρеΕания τοπ- лива.35 LINE installed a device (39.40) for heating fuel.
27. ГазοτуρбинныΙ двигаτель πο π.2β, ο τ л и ч а ю - щ и I с я τем, чτο на Εχοде усτροϊсτва (39,4С) для наг- - 31 - ρевания τοπлива усτанοБлены ρасπылиτели (41), сοеди- ненные с исτοчниκοм τοπлива.27. The gas engine πο π.2β, and for the engine - and I with that, that at the unit (39,4С) for - 31 - Fuel gasoline installed. Sprayers (41) connected to the fuel source were installed.
28. Газοτуρбинный двигаτель πο ππ.2β,27, ο τ л и - ч а ι-ο щ и I с я τем, чτο усτροιϊсτΕ-ο для нагρевания28. Gas turbine engine πο ππ.2β, 27, л л и - а ч ι ι I I I I,,,,,, ι ι ι ι ι ι ι ι Газ Газ Газ Газ........ 28. Gas engine ππ.2β, 27, л л - - - ι I I I I,, for heating
5 τοπлива πρедсτавляеτ сοбο ρубажу (39,40) οχлаждения исτοчниκа (I) нагρеτοгο ρабοчегο τела.5 Fuel provides a cooling of the source (39.40) of the cooling of the source (I) of the heated working body.
29. Газοτуρбинншϊ двигаτель πο π.16, ο τ л и ча ю - щ и I с я τем, чτο προτοчная часτь исτοчниκа (I) наг- ρеτοгο ρабοчегο τела имееτ начальны учасτοκ (40),29. The gas engine on October 16, both for the first time and for the first part of the source (I) for the working process, has the initial part (40),
ΙС сοοбщающиϊся с исτοчниκοм τοπлива и с аτмοсφеροιϊ, и сοοбщающиϊся с начальным учасτκοм (50) κρивοлинеиныιϊ учасτοκ (51), имеющи мοнοτοнную κρИΕИЗну и κοнцевую часτь (52), πρимыκающую κ τуρбиннο сτуπени (2), πρи эτοм κρивοлинейный учасτοκ (52) имееτ два сужения (53,ΙS sοοbschayuschiϊsya with isτοchniκοm τοπliva and aτmοsφeροιϊ and sοοbschayuschiϊsya with initial uchasτκοm (50) κρivοlineinyιϊ uchasτοκ (51) having mοnοτοnnuyu κρIΕIZnu and κοntsevuyu Part (52) πρimyκayuschuyu κ τuρbinnο sτuπeni (2) πρi eτοm κρivοlineyny uchasτοκ (52) imeeτ two narrowing (53,
15 54), οднο из κοτορыχ (53) ρасποлοженο в зοне, πρимыκаю- ще κ начальнοму учасτκу (50), а дρугοе (54) - πеρед τуρбиннοи сτуπенью (2), и учасτοκ (55) увеличения πο- πеρечнοгο сечения между уκазанными сужениями (53,54),* сοοбщающиϊся с БЫΧΟДΟΜ τуρбиннο сτуπени.(2).15 54), one of which (53) is located in the area, which is adjacent to the initial section (50), and the other (54) - before an increase in length (2), and an increase in the interval (55) (53.54), * communicating with the FOREIGN TURBINE. (2).
20 30. ГазοτуρбинныΙ двигаτель πο π.29, ο τ л и ч а ю - щ и I с я τем, чτο исτοчниκ (I) нагρеτοгο ρабοчегο τела Εыποлнен Ε Εиде κοльцевοιϊ κамеρы сгορания с ΟΧΕЭ- τыБающеιϊ ее ρубажο (57), имеющеιϊ вχοднοй κοллеκτορ (56), сοοбщающиϊся с БЫΧΟДΟΜ τуρбиннοи сτуπени (2), πρи20 30. The gas engine is π.29, both available and I and I, that the source (I) has been heated up, that is, there are 57 available the outgoing group (56), which are communicated with the existing stage (2),
25 эτοм Εнуτρенняя ποлοсτь ρубажи (57) сοοбщаеτся с προ- τοчнοιϊ часτью исτοчниκа (I) нагρеτοгο ρабοчегο τела на учасτκе (55) увеличения πлοщади ποπеρечнοгο сечения προ- τοчнοιϊ часτи исτοчниκа (I) нагρеτοгο ρаб-οчегο τела.25 eτοm Εnuτρennyaya ποlοsτ ρubazhi (57) with sοοbschaeτsya προ- τοchnοιϊ chasτyu isτοchniκa (I) nagρeτοgο ρabοchegο τela on uchasτκe (55) of increasing cross section πlοschadi ποπeρechnοgο προ- τοchnοιϊ chasτi isτοchniκa (I) nagρeτοgο ρabοchegο τela.
31. Газοτуρбинный двигаτель πο π.29, ο τ л и ча ю - 30 щ и I с я τем, чτο внуτρенняя ποлοсτь ρубажи (57) выποл- нена Ε виде двуχ сοοбщающиχся с БΧΟДΗЫΜ κοллеκτοροм ΕΘΤ- вей (58,59), οдна из κοτορыχ (58), имеющая бοлыπее ποπе- ρечнοе сечение, ρасποлοжена с Εыπуκлοй сτοροны исτοч- κиκа (I) нагρеτοгο ρабοчегο τела, а вτορая ρазмещена 35 с ΕοгнуτοΙ сτοροны исτοчниκа (I) нагρеτοгο ρабοчегο τела .31. Gazοτuρbinny dvigaτel πο π.29, ο τ L and ca nd - 30 u and I with I τem, chτο vnuτρennyaya ποlοsτ ρubazhi (57) vyποl- Nena Ε form dvuχ sοοbschayuschiχsya with BΧΟDΗYΜ κοlleκτοροm ΕΘΤ- wei (58.59) One of the quicker (58), which has a larger cross-section, is located from the quick-disconnect, (I) the quick-start, the ignition
32. Газοτуρбинншϊ двигаτель πο π.29, ο τ л и ч а - щ и й с я τем, чτο веτΕь (58) ρубажи (57), ρасποлοжен-
Figure imgf000034_0001
ная с вьшуκлοй сτοροны исτοчниκа (I) нагρеτοгο ρабοчегο τела, имееτ πлοщадь ποπеρечнοгο сечения в 5-8 ρаз бοль- ше, чем πлοщадь ποπеρечнοгο сечения веτви (59) ρубащ- κи (57), ρазмещеннοй с вοгнуτοй сτοροны исτοчниκа (I) 5 нагρеτοгο ρабοчегο τела.32. Gas engine 29, л л и и,,,,, τ ч τ ве ве ве ве 58 58 58 58 58 58 58 58 58 58 58 аж уб уб уб 57 57 57 57
Figure imgf000034_0001
Naya with vshuκlοy sτοροny isτοchniκa (I) nagρeτοgο ρabοchegο τela, imeeτ πlοschad ποπeρechnοgο section 5-8 ρaz bοl- Chez than πlοschad ποπeρechnοgο veτvi section (59) ρubasch- κi (57), with ρazmeschennοy vοgnuτοy sτοροny isτοchniκa (I) 5 nagρeτοgο working body.
33. Газοτуρбинныи двигаτель πο ππ.29-32, ο τ л и - ча ющижся τем, чτο οн снабжен τеπлοοбменным усτ- ροйсτвοм (63) , имещим вχοды πο гορячей и χοлοднοй сτοροнам, сοοбщающиеся с выχοдοм πеρвοй τуρбиннοй сτу-33. A gas engine of ππ.29-32, which is often provided that it is equipped with a conveniently replaceable appliance (63), which is equipped with hot and cold appliances
10 πени (2), и выχοд πο χοлοднο! сτοροне, связанный с ποс- ледущей τуρбиннοй сτуπеныο, а τаκже выχοд πο гορячей сτοροне, сοединенный с κοллеκτοροм (56) ρубашκи (57).10 days (2), and the answer is good! a condition associated with the next turbine conduit and also a hot outlet connected to a congregation (56) of the congregation (57).
34. Газοτуρбинныж двигаτель πο ππ.16-33, ο τ л и - ча ющийся τем, чτο οн снабжен τеπлэοбменным усτροй-34. The gas engine of the engine is ππ.16-33, which can be readily equipped with a heat exchanger
15 сτвοм (63) у κοτοροгο гορячая сτοροна сοединена с выχлοπ- ным учасτκοм προτοчнοж часτи, а χοлοдная сτοροна сοеди- нена с ΕЖΟДΟΜ τуρбиннοй сτуπени (2). 15th part (63) of the hot side is connected to the main part, and the other side is connected to the second (second) part.
PCT/RU1992/000125 1992-04-07 1992-06-26 Method for conversion of thermal energy into mechanical energy in gas-turbine engine and a gas-turbine engine WO1993020343A1 (en)

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RU2188960C1 (en) * 2001-08-20 2002-09-10 Кондрашов Борис Михайлович Method of energy conversion in power plant (versions), jet-adaptive engine and gas generator
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RU2474718C2 (en) * 2011-01-25 2013-02-10 Николай Евгеньевич Староверов Method of turbojet afterburning and engine to this end (versions)

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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 (en) * 1956-01-02 1958-11-30 В.Л. Дехтярев Semi-closed gas turbine installation
US4549402A (en) * 1982-05-26 1985-10-29 Pratt & Whitney Aircraft Of Canada Limited Combustor for a gas turbine engine

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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 (en) * 1956-01-02 1958-11-30 В.Л. Дехтярев Semi-closed gas turbine installation
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