DE468961C - Internal combustion engine with eccentric rotary piston compressor - Google Patents

Internal combustion engine with eccentric rotary piston compressor

Info

Publication number
DE468961C
DE468961C DEZ13045D DEZ0013045D DE468961C DE 468961 C DE468961 C DE 468961C DE Z13045 D DEZ13045 D DE Z13045D DE Z0013045 D DEZ0013045 D DE Z0013045D DE 468961 C DE468961 C DE 468961C
Authority
DE
Germany
Prior art keywords
compressed air
compressor
combustion engine
rotary piston
eccentric rotary
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.)
Expired
Application number
DEZ13045D
Other languages
German (de)
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
Publication date
Priority to DEZ13045D priority Critical patent/DE468961C/en
Application granted granted Critical
Publication of DE468961C publication Critical patent/DE468961C/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2730/00Internal-combustion engines with pistons rotating or oscillating with relation to the housing
    • F02B2730/01Internal-combustion engines with pistons rotating or oscillating with relation to the housing with one or more pistons in the form of a disk or rotor rotating with relation to the housing; with annular working chamber
    • F02B2730/012Internal-combustion engines with pistons rotating or oscillating with relation to the housing with one or more pistons in the form of a disk or rotor rotating with relation to the housing; with annular working chamber with vanes sliding in the piston
    • F02B2730/013Vanes fixed in the centre of the housing; Excentric rotors
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Compressor (AREA)

Description

Explosionsbrennkraftmaschine mit Exzenter-Drehkolbenkompressor Gegenstand der Erfindung ist eine Explo- sionsbrennkraftrnaschine mit Exzenter-Dreh- kolbenkompressor nach Patent 424 047, nach welchem zwischen der Druckseite und der Ansaugseite des Kompressors Eine durch einen. oder mehrere Schieber gesteuene Verbindung hergestellt ist, insbesondere um den Kom- pressor zum Anlassen und zur Erzeugung von Druckluft für Hilfszwecke verwenden zu können. Der Erfindungsgegenstand ist auf der Zeichnung meiner Ansführungsform veran- schauUcbt, und zwar in. einem Längsschnitt durch den Kompressor nebst fieilwelsex An- sicht. Der Kompressor ist z. B. für leinen aus. sechs Zylindern bestehenden 'Zweitaktmotor durchgebildet. Im Kompressorgehäuse i dreht sich, exzentrisch zu diesem, die als Schwung- ring ausgebildete Trommel 4, in welcher mit- tels drehbar gelagerter Zapfen, entsprechend der Zylinderzahl, sechs Flügel 8, 9,, 1 o, 11, 12, 13 radial verschiebebar angeordnet sind. Jeder Flügel besitzt sein Gleitstück 6, das in. -einer zum Gehäuse i konzentrischen Nut 7 geführt ist. In den Einlaßkanal 15 des Kompressors ist, wie beim Hauptpatent, ein Dreiwegehahn 14 eingebaut, durch den der Einla.ßkanal ent- weder mit dem Saugrohr 45 .oder mit ,einer Leitung 16 verbunden werden kann, welch letztere an den DruckItuftbehälter 17 ange- schlossen ist. Ungefähr an der Stelle der größten Entfernung des Umfanges der Trom- mel4 von der Gehäusewand ist ein., zweiter Hahn 18 angeordnet, der durch einen Hebel- arm 19 an einer Stange 2o angreift, die mit dem SteMebie1 2 i des Dreiwegehahnes 14 derart verbunden. ist, daß beide Hähne 14 und i Sentweder gleichzeitig oder, z. B. unter Zwischenschaltung eines federnden 'Zwischen, gliedes, auch ieinzeln bewegt werden können. Auf der Auslaßseite führt ein Kanal 22 zu einem Hahn 23, der durch Hebel 24 einstellbar ist und mit dem Kanal 25 in Verbindung ge- bracht werden kann, der den Zylindern 2 die Ladung zuführt. Bei. einer anderen Stellung verbindet der Hahn 23 den Kanal 22 miteiner Rohrleitung 26, in die,ein Rückächlagventil 27 eingebaut isst und welche Druckluft aus dem Kompressor nasch dem Behälter 17 fördert. Hinter dem Rückschlagventil27 zweigt bei der dargestellten Anordnung eine Leitung 28 ab, um Zerstäuberluft zum Brennstoffzerstäuber 29 zu leiten, der in dem Kopf 3 jedes Zylinders angeordnet ist.Explosive internal combustion engine with eccentric rotary piston compressor The subject of the invention is an explo- sion internal combustion engine with eccentric rotary piston compressor according to patent 424 047, according to which between the print side and the Suction side of the compressor One through one. or several slide controlled connection is established, in particular in order to pressor for tempering and producing Use compressed air for auxiliary purposes too can. The subject of the invention is on the Drawing of my form of quotation looks, in a longitudinal section by the compressor together with fieilwelsex view. The compressor is z. B. for linen off. six cylinder two-stroke engine trained. Rotates in the compressor housing i eccentric to this, the swing rin g trained drum 4, in which means of rotatably mounted pin, accordingly the number of cylinders, six wings 8, 9, 1 o, 11, 12, 13 are arranged to be radially displaceable. Everyone Wing has its slider 6, which is in to the housing i concentric groove 7 out is. In the inlet duct 15 of the compressor is as in the main patent, a three-way valve 14 built in through which the inlet duct neither with the suction pipe 45. or with, one Line 16 can be connected, which the latter connected to the compressed air tank 17 is closed. Roughly at the location of the greatest distance of the circumference of the mel4 from the housing wall is a., second Valve 18 arranged, which is operated by a lever arm 19 engages a rod 2o, which with the SteMebie1 2 i of the three-way valve 14 so connected. is that both taps 14 and i Sentweder simultaneously or, e.g. More colorful Interposition of a springy 'intermediate, member can also be moved individually. A channel 22 leads to the outlet side a cock 23 which can be adjusted by lever 24 and is connected to channel 25 can be brought to the cylinders 2 the Charge. At. In another position, the tap 23 connects the channel 22 to a pipe 26, in which a back pressure valve 27 is incorporated and which conveys compressed air from the compressor to the container 17. In the arrangement shown, a line 28 branches off downstream of the check valve 27 in order to conduct atomizing air to the fuel atomizer 29, which is arranged in the head 3 of each cylinder.

Für den Fall der Verwendung Beines zweistufigen Kompressors wird die höhere Stufe mit einer Leitung 3 5 in Verbindung gebracht, die einerseits an die zum Druckluftbehälter führende Leitung 26 und andererseits an eine zu den Zerstäubierdüsen führende Leitung 35 angeschlossen ist.In the case of using Beines two-stage compressor, the higher level associated with a line 3 5, the one hand to the line 26 leading to the compressed air tank and, on the other hand, to one to the atomizing nozzles leading line 35 is connected.

Claims (2)

PATENTANSPRÜCHE: i. Explosionsbrennkraftmaechine mit Exzenter-Drehkolbenkompressor nach Patent 424 047, dadurch gekennzeichnet, daß der am Austrittsende des Kompressors ange-,ordnete (23) derart ausgebildet ist, daß je nach Einstellung die vom Kompressor aus Kanal (22) zutretende Druckluft durch Abzweigung (25) zum Spülen, Laden, Auf- und überladen der Brennkraftmaschinenzylinder weitergeleitet wird und eine zweite Abzweigung (26) den Druckluftbehälter (17) speist, von welcher Abzweigung eine Druckluftleitung (28) zu den Einspritzdüsen (29) führt, um. diese dauernd unter Druckluft zu halten und deinen sofortiges Einströmen in die Zylinder bei Offenstellung der Einspritzdüsen zu gewährleisten. PATENT CLAIMS: i. Explosive combustion engine with eccentric rotary piston compressor according to patent 424 047, characterized in that the at the outlet end of the compressor arranged, arranged (23) is designed such that, depending on the setting, the compressor Compressed air entering from duct (22) through branch (25) for flushing, loading, and overloading the engine cylinder is forwarded and a second Branch (26) feeds the compressed air tank (17), from which branch a compressed air line (28) to the injection nozzles (29) leads to. to keep this permanently under compressed air and your immediate flow into the cylinders when the injectors are open to ensure. 2. Explosionsbrennkraftmasebine nach Anspruch i, dadurch gekennzeichnet, daß bei. Vorhandensein eines zweistufigen Kompressors die höhere Stufe mjt einer Leitung (3 5) i- Verbindung steht, die einerseits an die zum Druckluftbehälber führende Leitsong (26) und andererseits an eine zu den. Zerstäuherdüsen führende Leit'mg (33) angeschlossen isst.2. Explosion combustion engine according to claim i, characterized in that that at. If there is a two-stage compressor, the higher stage with one Line (3 5) i-connection is on the one hand to the one leading to the compressed air tank Leitsong (26) and on the other hand to one of the. Atomizing nozzles leading lead (33) connected eats.
DEZ13045D Internal combustion engine with eccentric rotary piston compressor Expired DE468961C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DEZ13045D DE468961C (en) Internal combustion engine with eccentric rotary piston compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEZ13045D DE468961C (en) Internal combustion engine with eccentric rotary piston compressor

Publications (1)

Publication Number Publication Date
DE468961C true DE468961C (en) 1928-11-26

Family

ID=7622983

Family Applications (1)

Application Number Title Priority Date Filing Date
DEZ13045D Expired DE468961C (en) Internal combustion engine with eccentric rotary piston compressor

Country Status (1)

Country Link
DE (1) DE468961C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE932639C (en) * 1934-12-02 1955-09-05 Daimler Benz Ag Two-stroke internal combustion engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE932639C (en) * 1934-12-02 1955-09-05 Daimler Benz Ag Two-stroke internal combustion engine

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