Momentum driven fuel injection of steam and fuel vapor for compression ignition engines
10018109 ยท 2018-07-10
Inventors
Cpc classification
F02M43/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M55/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B47/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M25/022
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M61/1826
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M53/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M61/1893
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M61/1806
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M25/0221
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M25/03
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02T10/12
GENERAL 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
International classification
F02B47/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M55/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M25/022
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M25/03
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M53/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M61/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
The present invention directly affects two primary limitations of diesel fuel: poor vaporization and ease of auto-ignition. Superheated fuel is injected within a cone of steam. As a result, fuel is fully vaporized and steam controls ignition by momentarily isolating fuel from air. In order to achieve high vapor velocities, the present invention uses momentum of circulating fuel and water to propel them through the injector. Momentum is preserved by transfer valves that transfer moving liquids between through paths and injection paths. Momentum is further preserved by an injector design that minimizes turbulence that would absorb energy and reduce injected velocity. The fuel and water may be superheated before injection to convert to steam and vapor upon the release of pressure when injected into the combustion chamber. The injector may also be used to achieve high injection velocity for liquid fuel injection without heating.
Claims
1. A high velocity liquid and vapor fuel injection apparatus for diesel engines comprising: fuel; water; sets of pressure pump and circulation pumps for water; sets of pressure pumps and circulation pumps for fuel; an injector; injector through passages, wherein said circulation pumps maintain constant flow through said injector through passages; injector outlet passages, wherein said apparatus uses momentum in said through passages to generate forces within said injector outlet passages to increase injection velocity; injector transfer valve, wherein said transfer valves momentarily divert flow in said injector through passages into said injector outlet passages; and exhaust heated heat exchangers.
2. The fuel injection apparatus of claim 1, wherein pressure of said fuel pressure pump prevents vaporization of superheated said fuel until the fuel is injected into the injector outlet passage.
3. The fuel injection apparatus of claim 1, wherein pressure of said water pressure pump prevents vaporization of superheated said water until said water is injected into said injector outlet passage.
4. The fuel injection apparatus of claim 1, wherein said injector outlet passage wall-to-wall spacing maintains pressure to initially prevents vaporization of superheated said fuel, but allows vaporization of said fuel as the wall-to-wall spacing increases causing pressure reduction such that the liquid fuel vaporizes before injection into a combustion chamber.
5. The fuel injection apparatus of claim 1, wherein said injector outlet passage wall-to-wall spacing prevents vaporization of superheated said water, but allows vaporization as the wall-to-wall spacing increases thereby allowing pressure to drop such that liquid water vaporizes before injection into a combustion chamber.
6. The fuel injection apparatus of claim 1, wherein said injector outlet passages are common for fuel and water.
7. The fuel injection apparatus of claim 1, wherein separate outlet injector passages are provided for said fuel and said water.
8. The fuel injection apparatus of claim 7, wherein said outlet injector passages are coaxial, formed by one tube within another.
Description
BRIEF DESCRIPTION OF DRAWINGS
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DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS
(9) Embodiments of the present invention utilize momentum to inject fuel farther into the combustion chamber resulting in better combustion. A transfer valve allows fuel traveling at a high rate of speed to be diverted within the injector and injected into the combustion chamber. Momentum produces higher velocity than do present high pressure common rail injection systems. Some embodiments also superheat fuel and water prior to injection.
(10) Superheated water may be used in combination with superheated fuel with a plume of steam enclosing a plume of fuel vapor. As fuel and air mix into steam, the steam may cool and delay combustion until ignition starts at the tip of the injected fuel-steam jet.
(11) The time to ignition at the tip of the fuel-steam jet may be controlled by adjusting the delay from the start of steam injection to the start of fuel vapor injection. If fuel vapor were injected ahead of steam, combustion would begin immediately. Starting steam first, delays air-fuel mixing and controls ignition at the tip of the jet.
(12) Once fuel ignites at the tip of the jet, pressure begins to build and combustion spreads. Timing of the fuel versus steam injection may also adjust the Pressure Rise Rate.
(13) The onset of hot main combustion is the same for both light and heavy loads. The leading edge of the steam fuel vapor injection is very similar for low and heavy loads. For low load conditions, fuel vapor injection would be brief. However, steam injection may be unchanged. Steam would carry the jet across the cylinder which would ignite at the leading edge. For light or heavy loads, timing of fuel and steam injection at the leading edge may be the same. However, for heavy loads, fuel vapor injection would continue longer. As a result, combustion would continue longer consuming fuel delivered later for heavy loads.
(14) The above paragraphs have described use of steam to isolate fuel vapor from air and thereby control combustion events. Another embodiment of the present invention is to use increased injection velocity. Hypersonic velocities are a possibility. For hypersonic velocity, fuel will travel faster than a pressure wave from initial combustion. That would enable fuel delivered later to pass through the combustion surface and pass into fresh air.
(15) Superheated fuel may remain liquid until it enters the combustion chamber. Momentum may be largely preserved, if fuel forward velocity is greater than lateral expansion velocity.
(16) Another embodiment utilizes superheated fuel to vaporize within the injector outlet passages. This option has the advantage of converting the thermal energy of the super-heated fuel into forward velocity which would be much greater than that of liquid fuel.
(17) The superheated fuel is injected as a liquid or a vapor. For small passage diameters, interference with closely spaced walls narrows the effective passage and creates too much back pressure for vapor to propagate ahead of the liquid. When the passage diameter is widened at the outlet end, superheated fuel vaporizes. The length of this widened section may be designed to produce a collimated beam of injected vapor fuel. Velocity of the collimated beam may be several times sonic velocity.
(18) In another embodiment, superheated fuel and superheated water are gated into common passages. In this embodiment, the sequence and timing of fuel and water injection may control combustion. Consider a sequence of water (steam), fuel and water (steam). Steam would first cool and dilute the air in the injection path. In addition, delay between the start of water injection and fuel injection may control ignition timing. Starting steam early would delay the time until fuel at the tip mixed through the steam, into air and ignited. Adjusting the time between start of steam and start of fuel may control ignition timing at the tip of the fuel injection. Initiating combustion at the tip would involve less fuel and would thereby reduce Pressure Rise Rate (PRR) and reduce stress on engine components which is of critical importance.
(19) Another sequence might be: water, fuel and water, and water. The effects noted above would be the same. However, combining fuel and water would dilute fuel vapor slowing ignition and increasing mixing. In addition, velocity for the combined fluids would be higher providing better penetration.
(20) The embodiments of the present invention have the following advantages: 1) Fuel is injected as a vapor; 2) The start of main combustion may be controlled; 3) Mixing is well advanced before combustion starts; 4) The air charge is not diluted or cooled; 5) Mixing and combustion may complete early in the combustion process; 6) The combustion process is substantially the same for varying loads.
(21) Rapid Fuel Delivery
(22) In the present invention, fuel and water momentum accelerate delivery. Transfer valves in the injectors are placed in the fuel rail so that circulating liquid continuously passes through the transfer valves. At injection, the liquid flow is transferred into the injection path. Momentum of liquid flowing into the transfer valves sustains constant liquid flow which is now delivered into the injection path.
(23) Turbulence in the injector passages dissipates energy and reduces velocity. For this reason passages in the injector must provide laminar flow as much as possible. One embodiment that helps meet that requirement is the use of micro-tubing. This tubing may be formed with large smooth radius turns between the inlet transfer valve and the injector outlets which minimize the number of turbulence producing transitions. Micro tubing is commercially available with internal diameters as low as 0.007 inches.
(24) Success of the apparatus depends on the injector which must do at least four things. First, inject high velocity fuel vapor and steam. Second, place fuel vapor within a protective sheath of steam. Third, deliver fuel vapor and steam independently. Fourth, rapidly deliver fuel vapor and steam quantities required.
(25) A better understanding of the present invention can be obtained when the following detailed description of the preferred embodiments is considered in conjunction with the following drawings, in which:
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(28) Without the heaters (301),
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(36) The present invention has potential to carry out the objects and attain the ends and advantages mentioned, as well as others inherent therein. While the invention has been depicted, described, and defined by reference to exemplary embodiments of the invention, such references do not imply a limitation on the invention, and no such limitation is to be inferred. The depicted and described embodiments of the invention are exemplary only, and are not exhaustive of the scope of the invention. Consequently, the invention is intended to be limited only by the spirit and scope of the appended claims, giving full cognizance to equivalents in all respects.