SI22457A - Rotating internal combustion engine with external compressor - Google Patents
Rotating internal combustion engine with external compressor Download PDFInfo
- Publication number
- SI22457A SI22457A SI200700015A SI200700015A SI22457A SI 22457 A SI22457 A SI 22457A SI 200700015 A SI200700015 A SI 200700015A SI 200700015 A SI200700015 A SI 200700015A SI 22457 A SI22457 A SI 22457A
- Authority
- SI
- Slovenia
- Prior art keywords
- pressure
- compressor
- cylinder
- internal combustion
- engine
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 11
- 235000021438 curry Nutrition 0.000 claims 1
- 230000006835 compression Effects 0.000 abstract description 8
- 238000007906 compression Methods 0.000 abstract description 8
- 230000004888 barrier function Effects 0.000 abstract description 5
- 238000010276 construction Methods 0.000 abstract description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 230000003111 delayed effect Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C11/00—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
- F01C11/002—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of similar working principle
- F01C11/004—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of similar working principle and of complementary function, e.g. internal combustion engine with supercharger
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C1/00—Rotary-piston machines or engines
- F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F01C1/34—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members
- F01C1/356—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the outer member
- F01C1/3562—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the outer member the inner and outer member being in contact along one line or continuous surface substantially parallel to the axis of rotation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
- F02B53/02—Methods of operating
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
Abstract
Description
ROTACIJSKI MOTOR Z NOTRANJIM ZGOREVANJEM IN ZUNANJIMROTATION ENGINE WITH INTERNAL COMBUSTION AND EXTERNAL
KOMPRESORJEMCOMPRESSOR
Predmet izuma je rotacijski motor z notranjim zgorevanjem, pri katerem je kompresija ustvarjena ločeno z zunanjim kompresorj em.The subject of the invention is a rotary internal combustion engine in which compression is created separately with an external compressor.
Tehnični problem, ki ga rešuje izum je takšna konstrukcija motorja, ki bo omogočala večji izkoristek energije v primerjavi z dosedanjimi poznanimi motorji z notranjim zgorevanj em.A technical problem solved by the invention is such an engine construction that will allow for greater energy utilization in comparison with the known internal combustion engines.
Znanih rešitev je precej, najbolj znana sta Quaziturbine in Wanklov motor. Pomanjkljivosti teh motorjev so predvsem tesnjenje ter majhna ročica sile na os vrtenja. V bistvu velik del sil deluje celo proti smeri vrtenja in ga tako zavira, s tem pa se izgublja veliko energije.There are many known solutions, the most famous being the Quaziturbine and the Wankl engine. The disadvantages of these engines are mainly the sealing and the small force on the axis of rotation. In fact, a large part of the force even acts against the direction of rotation and thus inhibits it, thereby losing a lot of energy.
Tehnični problem je po izumu rešen z ločitvijo sesalnega in kompesijskega takta od zgorevalne komore s pomočjo ločenega kompresorja ter obliko bata v valju, kjer zgorevalni prostor ločuje premična zapornica, katere pomik omogoča sama oblika bata. V cilinder prihaja že stisnjen zrak.The technical problem according to the invention is solved by separating the suction and compression stroke from the combustion chamber by means of a separate compressor and the piston shape in the cylinder, where the combustion chamber is separated by a movable barrier, the displacement of which is facilitated by the piston shape itself. The compressed air is already entering the cylinder.
Podrobneje so značilnosti izuma pojasnjene v nadaljevanju s pomočjo slik, ki prikazujejo:The features of the invention are explained in more detail below by means of figures showing:
Slika 1 KompresorFigure 1 Compressor
Slika 2 MotorFigure 2 Engine
Opis delovanja kompresorja (slika 1):Description of compressor operation (Figure 1):
Bat zajame veliko količino zraka in iz cilindra iztisne domala čisto vsega. Zaradi oblike bata(4) se proti koncu pritiski ustvarjajo počasi in ne sunkovito in tudi iztiskanje zraka zaradi oblike bata omogoča izjemne kompresijske lastnosti. Volumen se ne manjša premo sorazmerno ampak proti koncu počasneje, taka velika sila na majhen volumen pa omogoča velike pritiske. Pritisk premične zapore(3) na stene bata(4) vršimo z vzmetjo(2).The piston captures a large amount of air and expels almost everything from the cylinder. Due to the shape of the piston (4), pressures are created slowly and not at the end, and the air displacement due to the shape of the piston also provides exceptional compression properties. The volume does not shrink in proportion but slower towards the end, and such a large force on a small volume allows great pressures. The pressure of the movable bar (3) is applied to the piston walls (4) by a spring (2).
Večjo količino zraka imamo shranjeno v tlačni posodi(1), katera se polni z kompresorjem oziroma več kompresorji, kateri imajo poleg polnjenja tlačne posode(1) tudi funkcijo izkoriščanja energije pri zaviranju prevoznega sredstva. To dosežemo s postavitvijo treh kompresorjev, ki imajo različno zmogljivost, na pogonsko os ali osi. Kompresorji so različnih zmogljivosti glede na tlak, ki ga hočemo ustvariti oziroma na količino potrebnega zraka, pa tudi zavorne sile. Tako ustvarimo več stopenj kompresije-upora. Popuščanje pedala za plin v večjih stopnjah pomeni kontrolo zaviranja. Tako bi na pedal namestili 7 stopenj zaviranja, katere dobimo s tremi kompresorji. 1.stopnja-1.kompresor, 2.stopnja2. kompresor... 4. stopnja l.in 2. kompresor... 7. stopnja l.,2. in 3. kompresor. Voznik si tako sam uravnava moč zaviranja, katero omogoči kompresijsko zaviranje kompresorja, potreben zrak pa se shranjuje v tlačni posodi (1). Na ta način imamo shranjevanje energije z minimalnimi izgubami, saj se tlak v posodi ne manjša s časom. Ta zrak potem izkoristimo v motorju v kompresijskem taktu.A large amount of air is stored in the pressure vessel (1), which is filled with a compressor or several compressors, which in addition to filling the pressure vessel (1) also have the function of energy utilization when braking the vehicle. This is achieved by placing three compressors of different capacity on the drive axle or axles. The compressors are of different capacities depending on the pressure we want to create or the amount of air required, as well as the braking force. This creates several levels of compression-resistance. Releasing the accelerator pedal to a greater degree means braking control. This would put 7 brake levels on the pedal, which comes with three compressors. 1st stage-1st compressor, 2nd stage2. compressor ... 4th level l.in 2nd compressor ... 7th level l., 2. and 3. compressor. The driver thus regulates the braking power, which enables the compressor to brake compressor, and the required air is stored in the pressure vessel (1). This way, we save energy with minimal losses, as the pressure in the tank does not decrease with time. This air is then used in the engine in compression stroke.
Priklop kompresorjev na pogonsko os ali osi se vrši po potrebi in sicer ob padcu pritiska v tlačni posodi(1) ter ob zaviranju. S tem izkoriščamo energijo pri zaviranju, ki je bila do sedaj izgubljena.The compressors must be connected to the drive axle or axles, if necessary, in case of pressure drop in the pressure vessel (1) and when braking. This utilizes the energy in braking that has been lost so far.
Kompresorji se vključijo tudi ob padcu pritiska v tlačni posodi in sicer:Compressors are also activated when pressure drops in the pressure vessel, namely:
1) tlak v posodi pade pod minimalno mejo => vklopi se1) the pressure in the tank drops below the minimum limit => switch on
1.kompresor za nižje tlake in večjim pretokom zraka1.compressor for lower pressures and higher air flow
2) tlak še vedno pada => vklopi se 2. ali celo 3. kompresor.2) the pressure is still dropping => the 2nd or even 3rd compressor starts.
Delovanje motorja (slika 2):Engine operation (Figure 2):
Iz tlačne posode(1) je zrak speljan preko reducirnega ventila(8) v komoro ob cilindru motorja(7), kar nam omogoča konstanten delavni tlak. Iz te komore spuščamo v cilinder motorja želeno količino zraka s pomočjo računalniško vodenega ventila(6). Gorivo dodamo po že splošno znanih principih vbrizgavanja in ekspanzija zavrti bat(4). Pri bencinskem motorju potrebujemo, kot znano, vžigalno svečko za potrebno iskro. Trenutek vžiga ne sme biti preden premična zapornica (3) ne doseže najnižje točke, saj bi velik pritisk na steno premične zapornice onemogočil pomik premične zapornice navzdol in s tem bi nastala »luknja« oz. izguba kompresije. Vžig pa lahko poljubno zavlačujemo, kar nam omogoči večanje delavne prostornine (računalniško vodeno) in s tem tudi fleksibilnost motorja glede na potrebe. Glede na to, da je prostornina valja relativno zelo velika, lahko kompresijo v celoti izkoristimo preko celega valja. Pritisk premične zapore (3) na stene bata (4) vršimo z vzmetjo (2) ali kako drugače.From the pressure vessel (1), the air is drawn through a pressure reducing valve (8) into the chamber next to the cylinder of the engine (7), which allows us constant operating pressure. From this chamber, the desired amount of air is discharged into the engine cylinder by means of a computer-controlled valve (6). The fuel is added according to already known injection principles and the expansion of the rotated piston (4). With a gasoline engine, we need, as is known, a spark plug for the required spark. The moment of ignition must not be before the movable barrier (3) reaches the lowest point, as a large pressure on the wall of the movable barrier would prevent the movable barrier from moving downwards, thus creating a "hole" or "hole". loss of compression. However, ignition can be delayed at any time, which allows us to increase the working capacity (computer controlled) and thus the flexibility of the engine according to needs. Given that the volume of the cylinder is relatively large, compression can be fully utilized throughout the cylinder. The pressure of the movable lock (3) on the walls of the piston (4) is made by a spring (2) or otherwise.
Claims (3)
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SI200700015A SI22457A (en) | 2007-01-23 | 2007-01-23 | Rotating internal combustion engine with external compressor |
| DE200710027950 DE102007027950A1 (en) | 2007-01-23 | 2007-06-18 | Rotatable internal combustion engine with external compressor |
| PCT/SI2008/000005 WO2008091231A1 (en) | 2007-01-23 | 2008-01-23 | Rotary internal combustion engine with external compressor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SI200700015A SI22457A (en) | 2007-01-23 | 2007-01-23 | Rotating internal combustion engine with external compressor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SI22457A true SI22457A (en) | 2008-08-31 |
Family
ID=39433000
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SI200700015A SI22457A (en) | 2007-01-23 | 2007-01-23 | Rotating internal combustion engine with external compressor |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE102007027950A1 (en) |
| SI (1) | SI22457A (en) |
| WO (1) | WO2008091231A1 (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR101760362B1 (en) | 2010-12-10 | 2017-07-24 | 엠에이피 에너지 에스피에이 | Direct circular rotary internal combustion engines with toroidal expansion chamber and rotor without moving parts |
| WO2013033732A1 (en) * | 2011-09-01 | 2013-03-07 | Furnari Joseph | Rotational engine |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1846298A (en) * | 1926-06-24 | 1932-02-23 | Alcznauer Geza | Rotary engine |
| US3204616A (en) * | 1963-01-10 | 1965-09-07 | Harold G Eastman | Rotor engine |
| DE2818278A1 (en) * | 1978-04-26 | 1979-11-08 | Norbert Umlauf | Continuous combustion rotary piston engine - has air compressed into external store vessel, preheater and continuous combustion chamber for expansion |
| US5138994A (en) * | 1987-03-25 | 1992-08-18 | Laszlo Maday | Supercharged rotary piston engine |
| DE4305669A1 (en) * | 1993-02-24 | 1994-08-25 | Miao Hua | Elliptical rotary internal combustion engine |
| AU5242599A (en) * | 1998-07-31 | 2000-02-21 | The Texas A & M University System | Quasi-isothermal brayton cycle engine |
| US6347611B1 (en) * | 2000-07-17 | 2002-02-19 | Ellis F. Wright | Rotary engine with a plurality of stationary adjacent combustion chambers |
| JP2006513346A (en) * | 2003-01-09 | 2006-04-20 | レボリューション・エンジン・コーポレーション | Variable compression engine |
-
2007
- 2007-01-23 SI SI200700015A patent/SI22457A/en not_active IP Right Cessation
- 2007-06-18 DE DE200710027950 patent/DE102007027950A1/en not_active Withdrawn
-
2008
- 2008-01-23 WO PCT/SI2008/000005 patent/WO2008091231A1/en not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| WO2008091231A1 (en) | 2008-07-31 |
| DE102007027950A1 (en) | 2008-07-24 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| OO00 | Grant of patent |
Effective date: 20070202 |
|
| KO00 | Lapse of patent |
Effective date: 20140910 |