DE102004028950A1 - Conversion of thermal energy e.g. piston engine exhaust gases into kinetic energy includes accelerating a gas at temperature and pressure values exceeding those of the ambient air through a jet and mixing with colder ambient air - Google Patents
Conversion of thermal energy e.g. piston engine exhaust gases into kinetic energy includes accelerating a gas at temperature and pressure values exceeding those of the ambient air through a jet and mixing with colder ambient air Download PDFInfo
- Publication number
- DE102004028950A1 DE102004028950A1 DE200410028950 DE102004028950A DE102004028950A1 DE 102004028950 A1 DE102004028950 A1 DE 102004028950A1 DE 200410028950 DE200410028950 DE 200410028950 DE 102004028950 A DE102004028950 A DE 102004028950A DE 102004028950 A1 DE102004028950 A1 DE 102004028950A1
- Authority
- DE
- Germany
- Prior art keywords
- gas
- mixing
- ambient air
- kinetic energy
- temperature
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
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
- F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/60—Fluid transfer
- F05D2260/601—Fluid transfer using an ejector or a jet pump
Landscapes
- 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)
Abstract
Description
Die Wandlung von Energieträgern wie Öl, Kohle, Holz oder Gas in kinetische Energie erfolgt über den Umweg der Wandlung in thermische Energie und unter Nutzung der Gasgesetze. Die erzielbaren kinetischen Wirkungsgrade sind abhängig vom jeweiligen Kreisprozeß und liegen praktisch immer unter 50 % der verfügbaren Energiemenge.The Transformation of energy sources like oil, coal, Wood or gas in kinetic energy takes place via the detour of the transformation in thermal energy and using the gas laws. The achievable Kinetic efficiencies are dependent on the respective cycle and lie practically always less than 50% of the available energy.
Die häufigsten verwendeten technischen Vorrichtungen sind der Kolbenmotor, die Gasturbine und die Dampfturbine.The common used technical devices are the piston engine, the Gas turbine and the steam turbine.
Ihr Nachteil ist neben dem hohen technischen Aufwand besonders ihr schlechter energetischer Wirkungsgrad. Die Ursache liegt in der Unmöglichkeit, den zur Gasausdehnung oder zum Druckaufbau notwendigen Teil an Arbeit vollständig in kinetische Energie zu wandeln.you Disadvantage is in addition to the high technical effort especially her worse energetic efficiency. The cause lies in the impossibility the part of work necessary for gas expansion or pressure build-up Completely to transform into kinetic energy.
Das offene Wandlungsverfahren entspannt das erwärmte Gas oder den Wasserdampf nicht volumenmäßig, sondern durch Massenzuwachs. Dabei wird der Umstand ausgenutzt, daß bei Temperaturerhöhung eines Gases Arbeit gegen den atmosphärischen Luftdruck zu leisten ist, die dann beim Eindringen des Luftdruckes in einen beschleunigten Gasstrom wieder zurückgegeben wird.The open conversion process relaxes the heated gas or water vapor not in volume, but by mass growth. The fact is exploited that when the temperature increases a Gas's work against the atmospheric Air pressure is to be provided, which then when the air pressure is returned to an accelerated gas flow again.
Damit wird der technische Aufwand für thermische Energiewandler deutlich gesenkt. Das betrifft auch die Anforderungen an die Warmfestigkeit von Bauteilen.In order to is the technical effort for thermal energy converter significantly lowered. That also affects the Requirements for the heat resistance of components.
Ausführungsbeispielembodiment
Die von einem Freikolben-Gaserzeuger abgegebenen Gase werden in eine Strahlpumpe geleitet und dort der Druck in Beschleunigung gewandelt. Dabei gelangt Kaltluft des atmosphärischen Luftdruckes durch das Injektionsrohr in die Mitte der Stromröhre und vermischt sich mit dem heißen Gas. Dieses erfährt dadurch eine Abkühlung. Die Geschwindigkeit des Gasstrahles verändert sich durch die eindringende Kaltluft nicht.The Gases released by a free-piston gas generator become one Directed jet pump and there converted the pressure in acceleration. there gets cold air of the atmospheric Air pressure through the injection tube in the middle of the flow tube and mixes with the hot one Gas. This experiences thereby a cooling off. The speed of the gas jet changes due to the penetration Cold air not.
Diese Gas besitzt durch die Beschleunigung und die Masse kinetische Energie, die mit einer Peltonturbine in Drehzahl und Drehmoment gewandelt wird.These Gas has kinetic energy through acceleration and mass, which is converted into speed and torque with a Pelton turbine.
Claims (5)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE200410028950 DE102004028950A1 (en) | 2004-06-14 | 2004-06-14 | Conversion of thermal energy e.g. piston engine exhaust gases into kinetic energy includes accelerating a gas at temperature and pressure values exceeding those of the ambient air through a jet and mixing with colder ambient air |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE200410028950 DE102004028950A1 (en) | 2004-06-14 | 2004-06-14 | Conversion of thermal energy e.g. piston engine exhaust gases into kinetic energy includes accelerating a gas at temperature and pressure values exceeding those of the ambient air through a jet and mixing with colder ambient air |
Publications (1)
Publication Number | Publication Date |
---|---|
DE102004028950A1 true DE102004028950A1 (en) | 2005-12-29 |
Family
ID=35455067
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE200410028950 Withdrawn DE102004028950A1 (en) | 2004-06-14 | 2004-06-14 | Conversion of thermal energy e.g. piston engine exhaust gases into kinetic energy includes accelerating a gas at temperature and pressure values exceeding those of the ambient air through a jet and mixing with colder ambient air |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE102004028950A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL1030998C2 (en) * | 2006-01-25 | 2007-07-26 | Hendrikus Peter Van Der Waal | Pneumatically operating drive device. |
-
2004
- 2004-06-14 DE DE200410028950 patent/DE102004028950A1/en not_active Withdrawn
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL1030998C2 (en) * | 2006-01-25 | 2007-07-26 | Hendrikus Peter Van Der Waal | Pneumatically operating drive device. |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US10101092B2 (en) | Power generation system including multiple cores | |
Turan | Effect of reference altitudes for a turbofan engine with the aid of specific–exergy based method | |
DE4301100C2 (en) | Process for operating a combined cycle power plant with coal or oil gasification | |
FR2411400A1 (en) | GAS TURBINE ENGINE PROPULSION SIMULATOR | |
EP2119900A3 (en) | Gas turbine engine having a device for bleeding turbine flow into the fan bypass duct | |
Turgut et al. | Exergy analysis of a turbofan aircraft engine | |
BR112023004067A2 (en) | HEAT BUILDER | |
DE102004028950A1 (en) | Conversion of thermal energy e.g. piston engine exhaust gases into kinetic energy includes accelerating a gas at temperature and pressure values exceeding those of the ambient air through a jet and mixing with colder ambient air | |
Brilliant | Analysis of scramjet engines using exergy methods | |
DE102006050967B3 (en) | Vapor mixture for a thermal engine, to generate electricity, uses a polar and a non-polar fluid at low temperatures and pressures | |
DE20313279U1 (en) | Steam power plant | |
DE2200102B2 (en) | Device for generating a working gas flow | |
DE861848C (en) | Steam generator with charged combustion chamber | |
RU2272916C2 (en) | Steam-gas turbine plant | |
DE102021003976A1 (en) | Process and device for separating CO2 from gases | |
DE3643401A1 (en) | Method and device for a flue-gas-free condensation power station | |
CH133564A (en) | Internal combustion engine with turbocharger driven by means of an exhaust gas turbine. | |
DE918131C (en) | Device for generating mechanical energy from the gases of jet propulsion with intermittently repeated combustion of air in tubes that are open on the one hand | |
DE102008060024A1 (en) | Turbo compressor process for compressing compressible fluids, involves working turbo compressor in closed circuit with injectors of type A, B or C, through which mass flows | |
Jinghong et al. | Performance analysis on direct contact condensation refrigeration cycle of high temperature gas with super-cooled liquid | |
Hudson et al. | Theoretical and Computational analyses on the wet compression process | |
Jong-Yun | A Study of Simplified Test Rig for High Altitude Simulation | |
DE1129772B (en) | Deflagration turbine with open, lockable, fixed or rotating combustion chambers | |
AT216837B (en) | Gas turbine plant with a half-open circulation | |
DE2507789A1 (en) | Thermal power rotary engine - mixes vapourised fluid with heavy substance injects it onto turbine running wheels |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
8122 | Nonbinding interest in granting licenses declared | ||
8139 | Disposal/non-payment of the annual fee |