DE3144347A1 - Combustion engine - Google Patents

Combustion engine

Info

Publication number
DE3144347A1
DE3144347A1 DE19813144347 DE3144347A DE3144347A1 DE 3144347 A1 DE3144347 A1 DE 3144347A1 DE 19813144347 DE19813144347 DE 19813144347 DE 3144347 A DE3144347 A DE 3144347A DE 3144347 A1 DE3144347 A1 DE 3144347A1
Authority
DE
Germany
Prior art keywords
combustion engine
rotor
energy
torque
engine according
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Withdrawn
Application number
DE19813144347
Other languages
German (de)
Inventor
Hans P. 5100 Aachen Carjell
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to DE19813144347 priority Critical patent/DE3144347A1/en
Publication of DE3144347A1 publication Critical patent/DE3144347A1/en
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/005—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the engine comprising a rotor rotating under the actions of jets issuing from this rotor

Abstract

Published without abstract

Description

TITEL:TITLE:

VER8RENNUNGSKRAFTMASCHINE ANWENDUNGSGEBIET: DIE ERFINDUNG BETRIFTT EINE VERBRENNUNGSKRAFTMASCHINE ZUR ERZEUGUNG EINES DREHMOMENTS ZUM ANTRIEB VON MASCHINEN.ISOLATION FORCE MACHINE FIELD OF APPLICATION: THE INVENTION AFFECT A COMBUSTION ENGINE FOR GENERATING TORQUE TO DRIVE MACHINERY.

ZWECK: ZWECK DER VERBRENNUNGSKRAFTMASCHINE IST DIE UMWANDLUNG DER CHEMISCHEN ENERGIE EINES BRENNSTOFFES IN DIE MECHA-NISCHE ENERGIE EINES DREHMOMENTS UND IN WAERMEENERGIE.PURPOSE: THE PURPOSE OF THE COMBUSTION ENGINE IS THE CONVERSION OF CHEMICAL ENERGY OF A FUEL INTO THE MECHA-NICAL ENERGY OF A TORQUE AND IN THERMAL ENERGY.

STAND DER TECHNIK: ES IST BEKANNT, DASS DURCH STAUSTRAHLTRIEBWERKE AN DEN ENDEN DER ROTORBLAETTER EINES HUBSCHRAUBERS DIE MECHA-NISCHE ENERGIE EINES DREHMOMENTS AUS DER CHEMISCHEN ENERGIE EINES BRENNSTOFFES GEWONNEN WERDEN KANN.STATE OF THE ART: IT IS KNOWN THAT THAT BY REAR JETS AT THE ENDS OF A HELICOPTER'S ROTOR BLADES THE MECHA-NICAL ENERGY OF A TORQUE CAN BE OBTAINED FROM THE CHEMICAL ENERGY OF A FUEL.

KRITIK DES STANDES DER TECHNICK: DIESES ANTRIEBSPRINZIP WURDE HIER AUFGEGEBEN, WEIL DIE DREHZAHLEN, DIE FUER EINEN WIRTSCHAFTLICHEN BETRIEB DER STAUSTRAHLROHRE NOTWENDIG SIND, FUER DEN BETRIEB EINES HUBSCHRAUBERROTORS ZU HOCH LIEGEN. AUF ANDEREN GEBiETEN WURDE DAS PRINZIP BISHER NICHT ANGEWANDT.PRIOR ART CRITIC: THIS DRIVE PRINCIPLE BECAME HERE ABANDONED BECAUSE THE SPEEDS NEED FOR ECONOMICAL OPERATION OF THE NOZZLE TUBES ARE NECESSARY TO HIGH TO OPERATE A HELICOPTER ROTOR. ON OTHER THE PRINCIPLE HAS NOT BEEN APPLIED TO AREAS.

AUFGABEN: DER ERFINDUNG LIEGT DIE AUFGABE ZUGRUNDE, EINE VERBREN-NUNGSKRAFTMASCHINE ZUR ERZEUGUNG EINES DREHMOMENTS ZU BAUEN, DIE AUSSER EINEM ROTOR KEINE BEWEGLICHEN TEILE ENTHAELT.TASKS: THE INVENTION IS BASED ON THE TASK, A COMBUSTION POWER MACHINE TO BUILD A TORQUE THAT CANNOT BE MOVED BUT A ROTOR PARTS INCLUDED.

LOESUNG: DIESE AUFGABE WIRD ERFINDUNGSGEMAESS DADURCH GELOEST, DASS STAUSTRAHLTRIEBWERKE AM AEUSSEREN UMFANG EINES ROTORS EINEN TANGENTIALEN SCHUB ERZEUGEN.SOLUTION: THIS TASK IS SOLVED IN ACCORDANCE WITH THE INVENTION THAT REAR JETS CREATE A TANGENTIAL THRUST ON THE OUTSIDE OF A ROTOR.

WEITERE AUSGESTALTUNG: DIE FUER DEN BETRIEB DER STAUSTRAHLTRIEBWERKE ERFORDER-LICHE ROTORDREHZAHL BEIM START DER MASCHINE WIRD DURCH EIN HILFSAGGREGAT ERZIELT.FURTHER DESIGN: THE FOR THE OPERATION OF THE JETS REQUIRED ROTOR SPEED WHEN STARTING THE MACHINE IS GIVEN BY AN AUXILIARY UNIT ACHIEVED.

ERZIELBARE VORTEILE: DIE MIT ERFINDUNG ERZIELBAREN VORTEILE BESTEHEN BESONDERS DARIN, DASS AUSSER EINEM ROTOR, DER AN SEINEM AEUSSEREN UMFANG DIE TRIEBWERKE TRAEGT, DIE EINEN TANGENTIALEN SCHUB ERZEUGEN, KEINE WEITEREN BEWEGLICHEN TEILE ERFORDERLICH SIND.ACHIEVABLE ADVANTAGES: THE ADVANTAGES ACHIEVABLE WITH THE INVENTION EXIST PARTICULARLY THAT EXCEPT A ROTOR THAT HAS THE ENGINES ON ITS OUTSIDE PERIOD DOES NOT CARRY ANY MORE MOVING PARTS THAT CREATE A TANGENTIAL THRUST REQUIRED ARE.

Claims (3)

PATENTANSPRUECHE: 1jVERBRENNUNGSKRAFTMASCHINE ZUR UMWANDLUNG VON CHEMISCHER ENERGIE EINES BRENNSTOFFES IN MECHANISCHE ENERGIE EINES DREHMOMENTS UND WAERMEENERGIE, GEKENNZEICHNET DURCH STAUSTRAHLTRIEBWERKE, DIE AUF DEM AEUSSEREN UMFANG EINES ROTORS IN TANGENTIALER RICHTUNG EINEN SCHUB ERZEUGEN.PATENT CLAIMS: 1j INTERNAL COMBUSTION MACHINE FOR THE CONVERSION OF CHEMICAL ENERGY OF A FUEL INTO MECHANICAL ENERGY OF A TORQUE AND THERMAL ENERGY, CHARACTERIZED BY REAR JETS ON THE OUTER SCOPE OF A ROTOR GENERATE A THRUST IN TANGENTIAL DIRECTION. 2. VERBRENNUNGSKRAFTMASCHINE NACH ANSPRUCH 1, GEKENNZEICHNET DURCH EINEN ROTOR, DER BEIM START DURCH EIN HILFSAGGREGAT AUF DIE ZUM BETRIEB VON STAUSTRAHLTRIEBWERKEN NOTWENDIGF DREHZAHL GEBRACHT WIRD.2. COMBUSTION ENGINE ACCORDING TO CLAIM 1, CHARACTERIZED BY A ROTOR WHEN STARTED BY AN AUXILIARY UNIT TO OPERATE RUNNING ENGINES REQUIRED SPEED IS REQUIRED. 3. VERBRENNUNGSKRAFTMASCHINE NACH ANSPRUCH 1 BIS 2, GEKENNZEICHNET DURCH DIE AUSNUTZUNGSMOEGLICHKEIT DER WAERMEENERGIE DER VERBRENNUNGSGASE IN EINER ABGASTURBINE ODER IN EINEM WASSERROHRKESSEL.3. COMBUSTION ENGINE ACCORDING TO CLAIMS 1 TO 2, MARKED THROUGH THE POSSIBILITY OF USING THE THERMAL ENERGY OF THE COMBUSTION GASES IN ONE EXHAUST TURBINE OR IN A WATER PIPE BOILER.
DE19813144347 1981-11-07 1981-11-07 Combustion engine Withdrawn DE3144347A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE19813144347 DE3144347A1 (en) 1981-11-07 1981-11-07 Combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19813144347 DE3144347A1 (en) 1981-11-07 1981-11-07 Combustion engine

Publications (1)

Publication Number Publication Date
DE3144347A1 true DE3144347A1 (en) 1983-08-04

Family

ID=6145911

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19813144347 Withdrawn DE3144347A1 (en) 1981-11-07 1981-11-07 Combustion engine

Country Status (1)

Country Link
DE (1) DE3144347A1 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0300979A1 (en) * 1987-07-10 1989-01-25 Filippo Cristaldi Motor with turning ram jets
EP0662193A1 (en) * 1992-09-14 1995-07-12 LAWLOR, Shawn P. Method and apparatus for power generation
US5709076A (en) * 1992-09-14 1998-01-20 Lawlor; Shawn P. Method and apparatus for power generation using rotating ramjet which compresses inlet air and expands exhaust gas against stationary peripheral wall
US6298653B1 (en) 1996-12-16 2001-10-09 Ramgen Power Systems, Inc. Ramjet engine for power generation
US6446425B1 (en) 1998-06-17 2002-09-10 Ramgen Power Systems, Inc. Ramjet engine for power generation

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0300979A1 (en) * 1987-07-10 1989-01-25 Filippo Cristaldi Motor with turning ram jets
EP0662193A1 (en) * 1992-09-14 1995-07-12 LAWLOR, Shawn P. Method and apparatus for power generation
EP0662193A4 (en) * 1992-09-14 1997-01-15 Shawn P Lawlor Method and apparatus for power generation.
US5709076A (en) * 1992-09-14 1998-01-20 Lawlor; Shawn P. Method and apparatus for power generation using rotating ramjet which compresses inlet air and expands exhaust gas against stationary peripheral wall
US6347507B1 (en) 1992-09-14 2002-02-19 Ramgen Power Systems, Inc. Method and apparatus for power generation using rotating ramjets
US6510683B1 (en) 1992-09-14 2003-01-28 Ramgen Power Systems, Inc. Apparatus for power generation with low drag rotor and ramjet assembly
US6298653B1 (en) 1996-12-16 2001-10-09 Ramgen Power Systems, Inc. Ramjet engine for power generation
US6334299B1 (en) 1996-12-16 2002-01-01 Ramgen Power Systems, Inc. Ramjet engine for power generation
US6434924B1 (en) 1996-12-16 2002-08-20 Ramgen Power Systems, Inc. Ramjet engine for power generation
US6446425B1 (en) 1998-06-17 2002-09-10 Ramgen Power Systems, Inc. Ramjet engine for power generation

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Legal Events

Date Code Title Description
8141 Disposal/no request for examination