GB2029508A - Fuel injector valve with contoured flow nozzle - Google Patents
Fuel injector valve with contoured flow nozzle Download PDFInfo
- Publication number
- GB2029508A GB2029508A GB7927179A GB7927179A GB2029508A GB 2029508 A GB2029508 A GB 2029508A GB 7927179 A GB7927179 A GB 7927179A GB 7927179 A GB7927179 A GB 7927179A GB 2029508 A GB2029508 A GB 2029508A
- Authority
- GB
- United Kingdom
- Prior art keywords
- valve
- fuel
- metering
- fuel injection
- orifice
- 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.)
- Granted
Links
- 239000000446 fuel Substances 0.000 title claims abstract description 65
- 239000007921 spray Substances 0.000 claims abstract description 16
- 238000000926 separation method Methods 0.000 claims abstract description 6
- 238000002347 injection Methods 0.000 claims description 26
- 239000007924 injection Substances 0.000 claims description 26
- 239000012530 fluid Substances 0.000 claims description 7
- 230000007423 decrease Effects 0.000 claims description 3
- 230000003247 decreasing effect Effects 0.000 abstract 1
- 125000006850 spacer group Chemical group 0.000 description 6
- 238000007493 shaping process Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 239000010763 heavy fuel oil Substances 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000033228 biological regulation Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000009833 condensation Methods 0.000 description 1
- 230000005494 condensation Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 238000002788 crimping Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000001815 facial effect Effects 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000010408 sweeping Methods 0.000 description 1
- 238000009736 wetting Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/04—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
- F02M61/06—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series the valves being furnished at seated ends with pintle or plug shaped extensions
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
A transitional surface 144 connects the valve seat 126 to the metering orifice to gradually change the direction of fuel flow to avoid separation and unstable flow. The valve tip 122 narrows into a pintle 128 which extends through the metering orifice and ends in a deflection cap 130 which shapes the spray into a hollow-cone pattern. The valve tip between the pintle and closure surface 124 has a contoured surface 146 which with the nozzle bore provides an increasing flow area to a plateau value downstream of the closure surface, the flow area then smoothly decreasing from that value to where fuel exits the metering orifice. <IMAGE>
Description
SPECIFICATION
Injector valve with contoured valve seat and needle valve interface
The invention pertains generally to injector valves and is more particularly directed to injector valves having increased fuel flow rates.
Fuel injectors of the electromagnetic solenoid type have been commonly utilized in "multipoint" electronic fuel injection (EFI) systems in the automotive field. Such injectors are located at each cylinder of the engine and spray an atomized chrge of fuel into the intake manifold near the associated intake valve. As the intake valve opens, the atomized fuel and air from the intake manifold are drawn into the cylinder and are combusted. By controlling the duration of the operational times of the injectors with a pulse width modulated control signal from an electronic pulse width computer, the precision of fuel delivery has been greatly improved for the internal combustion engine. The fuel is metered accurately with respect to the many and varied operating parameters of the engine including manifold air pressure, rotational velocity, temperature and others.With this precision is the ability to improve fuel economy, control emissions, or increase driveability such that the conventional carburetor will probably be displaced in the future by the EFI system as the most prevelant fuel control device.
Another recent development in the fuel control field that may hasten the demise of the conventional carburetor is the "single point"
EFI system which, like its counterpart the "multipoint" EFI system, depends upon the precision of electronically controlling an electromagnetic solenoid injector.
"Single point" systems usually have one injector for the delivery of fuel to a plurality of cylinders of an engine at a single injection point instead of the "multipoint" system where a one-to-one correspondence occurs.
These injections points may be variably placed inside the intake manifold or the throttle bores of an air flow regulation device leading to the intake manifold. If placed in the throttle bores, these injectors may be located above or below the throttle blades for the most advantageous configuration depending on the particular injector structure. With the substitution of one injector for a plurality of injectors, the "single point" EFI system redues complexity and expense compared to many "multipoint" schemes while retaining most of the attendant
EFI system advantages vis à vis the conventional carburetor.
It is desirable to inject such "singie point" systems at least once per engine event (revolution) or even as fast as each intake valve opening. Since one injector replaces a piurality of injectors, sometimes as many as four for an eight-cylinder engine with a two-plane manifold, the "single point" injector generally must have a higher fuel flow rate than a corresponding "multipoint" injector. For use in higher displacement engines a higher flow rate electromagnetic solenoid injector would additionally be highly desirable whether "multipoint" or "single point".
This higher flow rate, because of the preferred single point injection timing, must be accomplished without the sacrifice of injector speed. If possible, it would be desirable for increased control that the injector speed should even be increased. If a higher flow rate is obtained at the expense of operating speed, such an injector will not be as advantageous as if both goals are achieved. The slower the injector opening time, the less overall fuel capacity the injector will be capable of delivering in the high speed range of the engine.
Presently in the art an increased flow rate for an injection valve can be obtained by increasing the metering orifice cros-sectional area, increasing the input pressure, or a combination of both. An increase in the input fuel pressure to a single point system would, however, require the additional expense of a higher pressure fuel pump and pressure regulator combination and is, therefore, unacceptable to the basic premise of single point systems, the reduction of complexity.
However, increasing the metering orifice cross-sectional area by scaling up a conventional "multipoint" injector to a "single point" flow rate creates other problems. Initially, the opening time and thus operation capability of the injector is detrimentally affected because of the increase in the mass of the needle valve. The mass of the needle valve increases in proportion to the volume increase of the material and not linearly with the increase in flow rate. Also, the flow paths of conventional "multipoint" valves are unfavorably restricted for "single point" applications and do not have sufficient flow area therethrough to efficiently handle the increased flow rate to a larger metering orifice.
Such "multipoint" valves are illustrated in
US Patents 4 007 800 issued to Hans, et al., and 3 967 597 issued to Schlagmuller, et al.
They disclose the use of a needle valve in an electromagnetic injector having flats cut on four sides of the shaft. This configuration unduly restricts flow through the injector valve and increases needle mass when utilized in a high flow injector.
A US Patent 3 069 099 issued to Graham illustrates a fuel injection nozzle with a threesided spring retainer plate. Although this configuration does not restrict fuel flow in the pressure operated injection nozzle shown it is not advantageously suitable for precision electromagnetic solenoid injection valves where exact metering and sure closure are required.
Another problem encountered in scaling up a conventional "multipoint" injector to a "single point" flow rate is that many injectors will not produce a stable flow at different pressures and times. At one particular pressure, for example, the static flow rate will be different some of the time and the instability unpredictable as to occurrence. This defect seems to worsen at higher flow rates and higher pressures, and is unacceptable in the "single point" flow rate and pressure range. Changes of between 5%-7% have been noted in the same injector operated at a particular pressure. The unpredictability of a flow rate from an injector will destroy the precision that the
EFI systems have brought to the fuel metering art.
This unstable flow problem seems to be centered in the valve seat metering orifice interface where the cylindrical metering orifice truncates the cone of the valve seat. At higher flow reates it is believed that the fuel accelerates through the closure surface and valve seat interface and then, at unpredictable intervals, will not smoothly flow into the exit orifice. If separation occurs at the exit orifice, the fuel will not be precisely metered by the area between the outer wall of the orifice and a pintle of the valve tip. This effect is similar to the "vena contracta" phenomenon found in hydraulics where a fluid under pressure flows around a sharp corner and has an extreme change of momentum and therefore separates from the surface of an orifice.
With high flow injector valves the angle at which the valve seat intersects the cylindrical metering orifice is relatively large because of the shallow cone angle of the valve seat necesary to produce high flow rates with minimal lift from the needle valve. Reducing this intersection angle without modifying the minimal lift conical valve seat would be highly desirable. A modification to the valve seat and valve tip interface of an injector is illustrated at Fig. 4 of a US Patent 3 241 768 issued to
Croft, but is for the purpose of developing a constant flow area.
Another problem that prior art injection valves with high flow rates incur is a residual fuel drop being retained on the injector or injector tip surface which effects the precision of fuel injection on subsequent openings. The residual fuel left on the injector will also cause contamination if it evaporates and can obstruct the metering orifice.
Spray pattern shaping has been attempted with ''multipoint" fuel injectors and with "single point" injectors. The shaping of the pattern is important in the "single point" applications, since one injector is entraining the fuel
in the air flow at a particular time and the consequent charge is to be delivered to particular multiples of the cylinders. If the air fuel ratio precision is to be maintained and cylinder-to-cylinder distribution errors minimized, the flow pattern must be correctly designed and reproducible with every injection. This will minimize wall wetting and unwanted condensation of the fuel on the throttle and other surfaces.
One of the spray patterns becoming popular in "single point" injection is the hollow-cone pattern where the fuel is limited to a volume between two differently-sized cones having their apex at the injector tip. It would be advantageous to be able to reproduce such a pattern with the same injector structure over a wide range of operating pressures and flow rates.
Therefore, the present invention proposes a fuel injection valve having a high flow rate metering portion comprising: a valve housing having a fuel flow passage which communicates fuel from a pressurized source to a truncated conical valve seat which intersects a cylindrical metering orifice; a needle valve, reciprocal in said valve passage, including a valve tip having a closure surface which is operable to close the injection valve when brought into contact with said valve seat, said valve tip forming an interface area with said valve seat downstream of said closure surface; characterized in that a transitional surface connects said valve seat to said orifice, said transitional surface changing the direction of the fluid flow through the interface area of the valve gradually so as not to induce separation from the transitional surface.
The invention will now be described with reference to the accompanying drawings, wherein:
Figure 1 is a cross-sectional side view of an injector housing and needle valve metering combination shown in a closed position that has been constructed in accordance with the invention;
Figure 2 is a cross-sectional side view of the injector housing and needle valve combination illustrated in Fig. 1 which is shown in an open position;
Figure 3 is an enlarged fragmentary side view in cross-section of the contoured valve seat and needle valve interface for the metering combination illustrated in Figs. 1 and 2; and
Figure 4 is a graphical representation of the flow area as a function of various positional points along the valve seat and needle valve interface illustrated in Fig. 3.
An injector valve metering portion having a
"single point" fuel flow rate is illustrated in
Fig. 1 in a closed position and comprises a valve housing 100 and needle valve 107
mounted in an injector housing 104 of the valve. The construction of the injector valve other than the metering portion is not shown
as it is conventional and not pertinent to a
discussion of the invention. Such portions
could, for example, comprise a solenoid con
nected at the armature to the needle valve
107 as illustrated in the referenced Hans, et
al., the disclosure of which is incorporated by
reference.
The valve housing 100 is received into a
mounting chamber 102 of an injector housing
104 and is spaced exactly by a C-shaped spacer washer 106 which has its dimensions accurately controlled by machining both facial surfaces. The valve housing 100 is held securely in the mounting chamber 102 by crimping the rim 114 of the injector housing
104 over an outside shoulder of the valve housing. A suitable O-ring 11 2 is used to seal the interface of the mounting chamber 102 and the valve housing 100.
The valve housing 100 is provided with an essentially central valve housing bore 11 6.
The needle valve 107 comprises a shank
portion 108 which fits through C-shaped spacer 106 and then flares into a radially outgo
ing spacer collar 110. The spacer collar 110 adjoins a generally triangular cross-section medial section having three equilateral bearing surfaces 118 spaced equally about the valve housing bore 11 6 to center the needle valve 107 within the bore.
The medial section connects to a valve tip 1 22 having a closure surface 1 24 which mates with a truncated conical valve seat 1 26 and then narrows to finally become an elongated pintle 1 28. The pintle 1 28 extends through a cylindrical metering orifice 1 32 and terminates in a deflection cap 1 30. The bearing surfaces 11 8 slide within the bore 11 6 and are connected by relieved surfaces 1 20 forming fuel flow passages between them and the valve housing bore 116.
Fuel uner pressure flows into the fuel passages between the needle valve and valve housing bore 11 6 from a pressurized source (not shown) which feeds fuel through the opening in the spacer washer 106. The fuel is prevented from exiting an annular fuel passage formed between the cylindrical orifice 1 32 and the pintle 1 28 by means of a closure force 105 forcing the needle valve tip into sealing relationship with the valve seat 126.
In Fig. 2, fuel is metered from the valve by applying an opening force 1 34 lifting the needle valve 107 away from the seat and allowing fuel to pass through the closure surface 1 24 and valve seat interface 1 26 and, thereafter, the orifice 1 32. The needle valve 107 is lifted to where the spacer collar 110 abuts washer 106. The opening force 1 34 and closure force 105 can be provided by a number of means such as a solenoid, pressure, or mechanical.
When the valve is open, fuel is metered through the annular passage formed by the pintle 1 28 and cylindrical metering orifice 1 32. The flow area of the passage is precisely controlled to permit a desired amount per unit time at the operating pressure of the valve to be injected. The fuel flow is shaped into a hollow-cone pattern by the deflection cap 1 30. The pattern has an outer cone angle A and an inner cone angle B between which substantially all of the fuel flow is contained.
Fig. 3 shows an enlarged cross-section view of the interface between the valve tip 1 22 and the valve seat 1 26. It is seen from the figure that the valve seat and metering orifice intersection, which was previously a sharp corner with a relatively large angle as indicated by dotted line 140, has been contoured into a transitional surface 1 44 which smoothly changes the direction from the conical face of the valve seat to the cylindrical orifice. The transitional surface 144 is shown as a curve beginning at the exit orifice and sweeping to where it becomes tangent to the valve seat surface 126.
This shape is the preferred form and can be in cross-section a circular arc or higher ordered curve, but any transitional surface which changes fuel direction gradually enough to not cause separation or cavitation in the fuel flow would be acceptable for the interface. The simplest form of the transitional surface could be a truncated conical surface beginning at the valve seat and connecting the cylindrical metering orifice. The transitional conical surface could have a greater slope than the valve seat, but less than the vertical angle of the metering orifice.
To compliment the transitional area, the valve tip 1 22 between the closure surface and the pintle has also been contoured from its previous shape, as shown by the dotted line at 142, to the present surface illustrated at 146. Taking cross-sectional flow area at different positions between the valve tip and the valve seat interface, it is seen in Fig. 4 that the flow area decreases from point A to point
B because of the closure surface and valve seat restriction. From point B to point D it gradually increases to where a plateau level is reached at points D-F. From point F to the flow area of the annular passage, I, the flow area gradually and smoothly decreases.
The flow area between points B and points
F allows the fuel to recover pressure lost going through the restricted area form A to B and slows the velocity. From point F the smooth entry of the fuel along the transitional surface into the exit orifice 1 32 keeps the fluid from dropping below the vapor pressure so the flow rate is stable and cavitation and separation are prevented.
The contour of the valve tip 1 22 and the contour of the transitional surface 144 both contribute to providing a metering valve which is stable in flow rate. Each can, however, be used individually to effect stability in injection valves, but the features preferably are used in combination to create a uniting of their individual contributions.
The shaping of the hollow cone spray pattern is accomplished by the deflection cap 1 30 which is formed on the end of the pintle as a cone with a flat deflection edge 1 38 and small fillet 1 50 connecting to the shaft of the pintle 128. A spray axis C-C indicates the direction of fluid momentum as the fuel exits the orifice 1 32. Assuming a constant pressure for the injector, the hollow-cone spray pattern is generated by controlling three variables which are: the annular flow area of the fuel passage between the metering orifice and pintle, the distance between the injector housing end and the flat deflection surface 148 designated D1, and the difference in the orifice diameter and the diameter of the base of the deflection cap designated d2.
Generally, the smaller the distance d1, the wider the spray pattern will be when the injector is open. Similarly, the smaller the distance d2 is, the wider the spray pattern angle. One limitation is that the distance d, must be greater than that necessary to prevent restriction of the metering orifice as the delfection cap 1 30 is for the purpose of separating the shaping function from the metering function in the present value.
The fuel flow, as it comes out and impinges upon the deflection surface 148, changes the direction of the fluid flowing the deflection distance d2 to form the two hollow-cone spray. The fluid deflected substantially perpendicular to the spray axis C-C by the deflection surface 1 38 will cause movement away from spray axis in the horizontal direction by a component related to the amount of flow and the amount of flow deflected. The larger the amount of flow deflected to that of the entire flow, the smaller the angles of the hollow-cone pattern.
As an example, a hollow-cone spray patter with an inner cone angle B of 60 and an outer cone angle A of 30 can be formed by an injector having a metering orifice of .84mm diameter and a pintle diameter of .56mm. The distance d1 for this injector would be approximately .41 mm and the distance d2 would be .025mm, or having a deflection cap with an outside base diameter of .81 mm. Such an injector would be designated to run at approximately 2.8 kg/cm2 and have a single float point flow rate of about 20 kg/hr.
A lower pressure injector running at approximately 1 kg/cm2 and the same flow rate with an inner cone angle B of 30 and an outer cone angle A of 10 can be advantageously manufactured by having a metering orifice of 1.12 mm with a pintle outside diameter of .64mm. This valve would have distance d1 of .61 mm. For this spray angle, a difference of .050mm, or distance d2, between the outside diameter of the base of the deflection cap and the metering orifice is desired, or where the base of the deflection cap equals 1.07mm in diameter.
While the preferred embodiments of the invention have been shown, it will be obvious to those skilled in the art that modifications and changes may be made to the disclosed systems without departing from the spirit and scope of the invention as defined by the
Claims (10)
1. A fuel injection valve having a high flow rate metering portion comprising: a valve housing having a fuel flow passage which communicates fuel from a pressurized source to a truncated conical valve seat which intersects a cylindrical metering orifice; a needle valve, reciprocal in said valve passage, including a valve tip having a closure surface which is operable to close the injection valve when brought into contact with said valve seat, said valve tip forming an interface area with said valve seat downstream of said closure surface, characterized in that a transitional surface connects said valve seat to said orifice, said transitional surface changing the direction of the fluid flow through the interface area of the valve gradually so as not to induce separation from the transitional surface.
2. A fuel injection valve with a metering portion according to claim 1, characterized in that said transitional surface is formed as a truncated conical surface with a greater conical slope than said valve seat.
3. A fuel injection valve with a metering portion according to claim 2, characterized in that said transitional surface is formed as a curvature connecting said valve seat and said metering orifice.
4. A fuel injection valve with a metering portion according to claim 3, characterized in that said radius of curvature is formed by a circular radius being extended from the inlet end of said metering orifice to where it is tangent to said conical valve seat.
5. A fuel injection valve with a metering portion according to anyone of claims 1 to 4, characterized in that said valve tip narrows into a pintle which extends through said metering orifice, said valve tip being contoured between said closure surface and said pintle such that the flow area of the valve tip and valve seat interface increases to a plateau value and subsequently decreases smoothly to where the fuel exits the metering orifice.
6. A fuel injection valve with a metering portion according to claim 5, characterized in that said valve tip terminates in a deflection cap having a deflection surface ending in an edge substantially perpendicular to the injector spray axis.
7. A fuel injection valve with a metering portion according to claim 6, characterized in that said deflection surface controllably forms a hollow-cone spray pattern with an inner cone angle and outer cone angle by varying the distance of the deflection surface with respect to the end of the exit orifice.
8. A fuel injection valve with a metering portion according to claim 7, characterized in that said inner and outer cone angles are controllably formed by varying the distance between the diameter of the base of said deflection surface and the diameter of said metering orifice.
9. A fuel injection valve with a metering portion according to claim 8, characterized in that said inner and outer cone angles are controllably formed by varying the flow area of the annular fuel passage formed between said pintle and said metering orifice.
10. A fuel injection valve substantially as described and as shown in the accompanying drawings.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US94052278A | 1978-09-08 | 1978-09-08 |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2029508A true GB2029508A (en) | 1980-03-19 |
GB2029508B GB2029508B (en) | 1983-03-30 |
Family
ID=25474967
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7927179A Expired GB2029508B (en) | 1978-09-08 | 1979-08-03 | Injector valve with contoured valve seat and needle valve interface |
Country Status (6)
Country | Link |
---|---|
JP (1) | JPS5537598A (en) |
CA (1) | CA1124146A (en) |
DE (1) | DE2935850A1 (en) |
FR (1) | FR2435607B1 (en) |
GB (1) | GB2029508B (en) |
IT (1) | IT1122944B (en) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0042799A2 (en) * | 1980-06-23 | 1981-12-30 | The Bendix Corporation | Electromagnetic fuel injector |
FR2487012A1 (en) * | 1980-07-16 | 1982-01-22 | Lucas Industries Ltd | FUEL INJECTOR FOR ENGINE |
WO1987000583A1 (en) * | 1985-07-19 | 1987-01-29 | Orbital Engine Company Proprietary Limited | Direct fuel injection by compressed gas |
WO1987007334A2 (en) * | 1986-05-31 | 1987-12-03 | Robert Bosch Gmbh | Fuel injection valve |
DE3710467A1 (en) * | 1986-05-31 | 1987-12-03 | Bosch Gmbh Robert | IC engine fuel injection valve - has electromagnetically operated valve needle with toroidal surface cooperating with valve seat |
EP0283154A1 (en) * | 1987-03-14 | 1988-09-21 | LUCAS INDUSTRIES public limited company | Fuel injection nozzle |
GB2219627A (en) * | 1988-06-10 | 1989-12-13 | Orbital Eng Pty | Nozzles for in-cylinder fuel injection |
US5890659A (en) * | 1995-12-05 | 1999-04-06 | Robert Bosch Gmbh | Valve closing body and process and device for producing sealing seats on valve closing bodies |
WO1999058844A1 (en) * | 1998-05-08 | 1999-11-18 | Mtu Motoren- Und Turbinen-Union Friedrichshafen Gmbh | Fuel injection nozzle for an internal combustion engine |
WO2000065226A1 (en) * | 1999-04-27 | 2000-11-02 | Siemens Automotive Corporation | Fuel injector with a transition region |
US6920690B1 (en) | 1999-04-27 | 2005-07-26 | Siemens Vdo Automotive Corp. | Method of manufacturing a fuel injector seat |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5863620A (en) * | 1981-10-09 | 1983-04-15 | C Uyemura & Co Ltd | Carrier for surface treatment apparatus |
JPS58120865U (en) * | 1982-02-09 | 1983-08-17 | 松下電器産業株式会社 | fuel injection valve |
JPS6019957A (en) * | 1983-07-12 | 1985-02-01 | Japan Electronic Control Syst Co Ltd | Nozzle for fuel injection valve of internal-combustion engine, and method of manufacturing said nozzle |
JPS63196477U (en) * | 1987-06-05 | 1988-12-16 | ||
JP2508777B2 (en) * | 1987-12-21 | 1996-06-19 | いすゞ自動車株式会社 | Fuel injection nozzle for direct injection diesel engine |
US5241938A (en) * | 1990-03-14 | 1993-09-07 | Aisan Kogyo Kabushiki Kaisha | Injector with assist air passage for atomizing fuel |
FR3112186A1 (en) * | 2020-07-02 | 2022-01-07 | Schrader | Pressure regulator for spraying a fluid and associated process |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB726248A (en) * | 1952-04-12 | 1955-03-16 | Bosch Gmbh Robert | Improvements in fuel injection valves for internal combustion engines |
GB906603A (en) * | 1958-06-14 | 1962-09-26 | Motorpal Jihlava | Improvements in and relating to fuel injection nozzles for internal combustion engines |
GB921949A (en) * | 1961-06-10 | 1963-03-27 | Orange G M B H L | Fuel injection valve with fuel-controlled valve needle |
GB1076184A (en) * | 1963-05-01 | 1967-07-19 | Ass Eng Ltd | Fuel injectors for internal combustion engines |
GB1191119A (en) * | 1966-06-29 | 1970-05-06 | Ambac Ind | Fuel Injection Nozzle |
GB1521641A (en) * | 1976-01-20 | 1978-08-16 | Sud Maintenance | Electromagnetic fuel injectors for internal combustion engines and method of manufacturing them |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE72869C (en) * | G. A, list, V. list und J. kosakoff in Moskau | Device for overheating and gasifying liquid hydrocarbons | ||
DE589552C (en) * | 1933-12-11 | Werke Kiel Akt Ges Deutsche | Injection valve for internal combustion engines | |
FR1082680A (en) * | 1952-04-12 | 1954-12-31 | Bosch Gmbh Robert | Fuel injector |
DE1156602B (en) * | 1959-06-26 | 1963-10-31 | Bosch Gmbh Robert | Injector |
DE2034078A1 (en) * | 1970-07-09 | 1972-01-13 | Bosch Gmbh Robert | Electromagnetic injection valve for timing and stroke measurement |
-
1979
- 1979-05-30 CA CA328,649A patent/CA1124146A/en not_active Expired
- 1979-08-03 GB GB7927179A patent/GB2029508B/en not_active Expired
- 1979-08-14 FR FR7920676A patent/FR2435607B1/en not_active Expired
- 1979-09-03 IT IT25437/79A patent/IT1122944B/en active
- 1979-09-05 DE DE19792935850 patent/DE2935850A1/en not_active Ceased
- 1979-09-07 JP JP11434379A patent/JPS5537598A/en active Granted
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB726248A (en) * | 1952-04-12 | 1955-03-16 | Bosch Gmbh Robert | Improvements in fuel injection valves for internal combustion engines |
GB906603A (en) * | 1958-06-14 | 1962-09-26 | Motorpal Jihlava | Improvements in and relating to fuel injection nozzles for internal combustion engines |
GB921949A (en) * | 1961-06-10 | 1963-03-27 | Orange G M B H L | Fuel injection valve with fuel-controlled valve needle |
GB1076184A (en) * | 1963-05-01 | 1967-07-19 | Ass Eng Ltd | Fuel injectors for internal combustion engines |
GB1191119A (en) * | 1966-06-29 | 1970-05-06 | Ambac Ind | Fuel Injection Nozzle |
GB1521641A (en) * | 1976-01-20 | 1978-08-16 | Sud Maintenance | Electromagnetic fuel injectors for internal combustion engines and method of manufacturing them |
Cited By (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0042799A3 (en) * | 1980-06-23 | 1982-01-13 | The Bendix Corporation | Electromagnetic fuel injector |
EP0042799A2 (en) * | 1980-06-23 | 1981-12-30 | The Bendix Corporation | Electromagnetic fuel injector |
FR2487012A1 (en) * | 1980-07-16 | 1982-01-22 | Lucas Industries Ltd | FUEL INJECTOR FOR ENGINE |
GB2190707B (en) * | 1985-07-19 | 1990-01-04 | Orbital Eng Pty | Direct fuel injection by compressed gas |
WO1987000583A1 (en) * | 1985-07-19 | 1987-01-29 | Orbital Engine Company Proprietary Limited | Direct fuel injection by compressed gas |
GB2190707A (en) * | 1985-07-19 | 1987-11-25 | Orbital Eng Pty | Direct fuel injection by compressed gas |
WO1987007334A2 (en) * | 1986-05-31 | 1987-12-03 | Robert Bosch Gmbh | Fuel injection valve |
EP0393328A1 (en) * | 1986-05-31 | 1990-10-24 | Robert Bosch Gmbh | Fuel injection valve |
WO1987007334A3 (en) * | 1986-05-31 | 1987-12-30 | Bosch Gmbh Robert | Fuel injection valve |
DE3710467A1 (en) * | 1986-05-31 | 1987-12-03 | Bosch Gmbh Robert | IC engine fuel injection valve - has electromagnetically operated valve needle with toroidal surface cooperating with valve seat |
EP0283154A1 (en) * | 1987-03-14 | 1988-09-21 | LUCAS INDUSTRIES public limited company | Fuel injection nozzle |
US5090625A (en) * | 1988-06-10 | 1992-02-25 | Orbital Engine Company Proprietary Limited | Nozzles for in-cylinder fuel injection systems |
AU612038B2 (en) * | 1988-06-10 | 1991-06-27 | Orbital Engine Company Proprietary Limited | Improvements relating to nozzles for in-cylinder fuel injection systems |
GB2219627A (en) * | 1988-06-10 | 1989-12-13 | Orbital Eng Pty | Nozzles for in-cylinder fuel injection |
GB2219627B (en) * | 1988-06-10 | 1992-10-28 | Orbital Eng Pty | Improvements relating to nozzles for in-cylinder fuel injection systems |
US5890659A (en) * | 1995-12-05 | 1999-04-06 | Robert Bosch Gmbh | Valve closing body and process and device for producing sealing seats on valve closing bodies |
WO1999058844A1 (en) * | 1998-05-08 | 1999-11-18 | Mtu Motoren- Und Turbinen-Union Friedrichshafen Gmbh | Fuel injection nozzle for an internal combustion engine |
WO2000065226A1 (en) * | 1999-04-27 | 2000-11-02 | Siemens Automotive Corporation | Fuel injector with a transition region |
US6502769B2 (en) | 1999-04-27 | 2003-01-07 | Siemens Automotive Corporation | Coating for a fuel injector seat |
US6526656B2 (en) | 1999-04-27 | 2003-03-04 | Siemens Automotive Corporation | Coating for a fuel injector seat |
US6920690B1 (en) | 1999-04-27 | 2005-07-26 | Siemens Vdo Automotive Corp. | Method of manufacturing a fuel injector seat |
Also Published As
Publication number | Publication date |
---|---|
JPS6363746B2 (en) | 1988-12-08 |
JPS5537598A (en) | 1980-03-15 |
DE2935850A1 (en) | 1980-03-20 |
FR2435607A1 (en) | 1980-04-04 |
FR2435607B1 (en) | 1985-10-25 |
CA1124146A (en) | 1982-05-25 |
GB2029508B (en) | 1983-03-30 |
IT1122944B (en) | 1986-04-30 |
IT7925437A0 (en) | 1979-09-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |