WO1999023674A1 - Cascading electromagnetic armature - Google Patents
Cascading electromagnetic armature Download PDFInfo
- Publication number
- WO1999023674A1 WO1999023674A1 PCT/US1998/023342 US9823342W WO9923674A1 WO 1999023674 A1 WO1999023674 A1 WO 1999023674A1 US 9823342 W US9823342 W US 9823342W WO 9923674 A1 WO9923674 A1 WO 9923674A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- conductive
- sleeve
- core
- armature
- cascading
- Prior art date
Links
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F3/00—Cores, Yokes, or armatures
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F7/00—Magnets
- H01F7/06—Electromagnets; Actuators including electromagnets
- H01F7/08—Electromagnets; Actuators including electromagnets with armatures
- H01F7/081—Magnetic constructions
Definitions
- the present invention relates to solenoids.
- the present invention relates to an improved structure for a cascading electromagnetic armature for a solenoid that may be used in the operation of compression release-type engine retarders.
- Compression release-type engine retarders are well-known in the art.
- Engine retarders are designed to convert temporarily an internal combustion engine of either the spark ignition or compression ignition type into an air compressor.
- a compression release retarder decreases the kinetic energy of an engine by opposing the upward motion of the engine's pistons on the compression stroke.
- As a piston travels upward on its compression upstroke the gases that are trapped in the cylinder are compressed. The compressed gases oppose the upward motion of the piston.
- an exhaust valve is opened to "release" the compressed gases.
- the pressure having been released from the cylinder the piston cannot recapture the energy stored in the compressed gases on the subsequent expansion downstroke. In so doing, the engine develops retarding power to help slow down the vehicle.
- a properly designed and adjusted compression release-type engine retarder can develop retarding power that is a substantial portion of the power developed by the engine on positive power.
- Compression release-type retarders of this type supplement the braking capacity of the primary vehicle wheel braking system. In so doing, these retarders may substantially extend the life of the primary wheel braking system of the vehicle.
- the basic design of a compression release type engine retarding system is disclosed in Cummins, United States Patent No. 3,220,392.
- the compression release-type engine retarder disclosed in the Cummins patent employs a hydraulic system to control the operation of the exhaust valves to effect the compression release event. The hydraulic control system engages the engine's existing valve actuation system, namely, the rocker arms of the engine.
- the hydraulic control system of the compression release retarder When the engine is operating under positive power, the hydraulic control system of the compression release retarder is disengaged from the valve control system, so that no compression release event occurs.
- compression release retarding When compression release retarding is desired, the engine is deprived of fuel and the hydraulic control system of the compression release brake engages the valve control system of the engine. The valve control system drives the compression release retarder to produce compression release events at the appropriate times.
- the hydraulic systems of compression release engine retarders typically have a number of components.
- a solenoid valve is typically actuated to supply engine oil to fill the hydraulic circuits of the compression release engine retarder. when retarding is desired.
- Solenoids typically contain some type of slidable armature assembly which is biased in a direction opposite to a magnetic force applied by the coil. When the coil is energized, the magnetic force builds up to attract the armature assembly until the force is sufficient to overcome the bias.
- Cylindrical type solenoids typically consist of a coil or winding surrounding a central hollow core in which an armature of soft iron or low carbon steel is slidably located.
- Figure 1 is an example of a short stroke solenoid actuator 10 having a flat ended armature 170.
- the solenoid 10 includes a conductive frame 110, a conductive coil 120, a conductive flux member 130, and an end cap 140, all of which define a central bore 150 in the solenoid.
- Located within the bore 150 are an armature 170 and a pole member 180.
- a slidable plunger 190 is provided in a central bore through the pole member 180.
- the conductive frame 110, conductive flux member 130, and the pole member 180 may be made preferably of soft iron or fully annealed low carbon steel.
- the armature 170 comprises a solid plug of conductive material slidably disposed in the bore 150.
- the armature 170 may be cylindrical in shape and may have a conical or flat end 172, depending on the working stroke desired.
- Flat ended armatures are generally used for short stroke applications.
- Conical ended armatures may have a 90° cone for medium stroke units or a 60° cone for longer stroke devices.
- the movement of the armature 170 towards the pole member 180 is restricted by contact with the poie member. In its deactivated position, an air gap 200 is provided between the armature and the pole member 180.
- the coil 120 is energized to activate the solenoid 10.
- the solenoid 10 When the solenoid 10 is activated the armature 170 is attracted to and slides towards the pole member 180. Movement of the armature 170 towards the pole member 180 displaces the plunger 190 downward.
- the coil 120 When the coil 120 is energized, magnetic flux is developed within the conductive elements of solenoid. The magnetic flux produces an attractive force across any air gaps (e.g. air gap 200) that occur within the circuit. This force is generally considered to be inversely proportional to the square of the air gap distance. That is, if the air gap distance is doubled, the magnetic attraction force will be reduced by approximately a factor of four.
- the working air gap 200 that exists between the armature end 172 and the pole face 182 obeys the inverse square law.
- the power of the downward stroke of the armature 170 (and the voltage required in coil 120 to produce this stroke) are a function of the air gap 200 distance.
- the air gap 200 in order to increase the stroke of the plunger 190, the air gap
- the relatively small diametral clearance (air gap) between the conductive flux member 130 and the armature 170 produces a very high side force on the armature as a result of the inverse square law.
- This side force may create unwanted friction forces that oppose sliding motion of the armature 170 in the bore 150. It is desirable to reduce the effect of this side force by minimizing the coefficient of friction between the armature 170 and the side walls of the bore 150 in which it is disposed. This is may be accomplished by selecting a liner material of plastic or brass that guides the armature 170 and prevents actual contact between the armature and the conductive flux member 130. Lubrication between the armature 170 and the conductive flux member 130 may also be used to reduce friction between the two.
- Magnetic circuits such as those in the solenoid 10. may exhibit a phenomena known as saturation.
- the conductive material of the circuit can carry only a limited flux density (Maxwells/sq.cm), visualized as so many lines of flux per unit area. Regardless of the magnetic intensity (amp-turns/cm.) exerted by the coil, a given area of the attracting armature and pole member faces may reach saturation and the flux passing through that area will be restricted beyond that value — which may result in magnetic "freeze-up" of the attracted elements.
- An object of the present invention is to reduce the likelihood of magnetic "freeze-up.”
- Solenoids may require a certain number of "amp turns” to create the necessary magnetic field around the coil to actuate the armature.
- Current engine electronic control modules are not generating the required "amp turns” or voltages necessary to actuate the current technology based solenoids. To overcome this problem, either the voltage, or the mechanical advantage of the solenoid, must be increased.
- the armature may include two members, wherein the two members are adapted to be independently displaced relative to each other towards a pole member.
- the two members of the armature may include a conductive core and at least one conductive sleeve surrounding the conductive core.
- the conductive core may be slidably disposed within the conductive sleeve, and the conductive sleeve may be slidably disposed in the conductive housing.
- the present invention may include multiple conductive sleeves, wherein an inner conductive sleeve surrounds the conductive core, and an outer conductive sleeve surrounds the inner conductive sleeve.
- the inner conductive sleeve may be recessed within and independently slidable relative to the outer conductive sleeve.
- the conductive core and the conductive sleeve may be cylindrical in shape, or the shape may vary from cylindrical to any number of shapes.
- the conductive core may include a flat or a conical end spaced from the pole member.
- the conductive core may include an internal void.
- the conductive sleeve includes a means for engaging the conductive core upon displacement of the conductive sleeve.
- the engaging means may comprise a washer composed of a non-conductive or a conductive material.
- the washer may be convex or some other type of spring mechanism.
- the electromagnetic solenoid of the present invention may possess an outer air gap between the conductive sleeve and the pole member, and an inner air gap between the conductive core and the pole member.
- the conductive core may be recessed within the conductive sleeve such that the conductive core is further from the pole member than the conductive sleeve when the solenoid is not energized.
- the outer air gap may be in the range of 0.01 and 0.05 inches, and the inner air gap may be in the range of 0.02 and 0.10 inches for certain applications, but the present invention is not intended to be limited to these ranges.
- Fig. 1 is a cross-section in elevation of an electromagnetic solenoid.
- Fig. 2 is a cross-section in elevation of a first embodiment of the cascading electromagnetic armature of the present invention.
- Fig. 3 is a cross-section in elevation of a second embodiment of the cascading electromagnetic armature of the present invention.
- Fig. 4 is a cross-section in elevation of a third alternative embodiment of the cascading electromagnetic armature of the present invention.
- Fig. 5 is a cross-section in elevation of a fourth alternative embodiment of the cascading electromagnetic armature of the present invention.
- FIG. 1 is an example of an embodiment of the present invention, in which like elements to those in Figure 1 are referred to with like reference numerals.
- the present invention may utilize a solenoid 10 with a telescoping (cascading) armature 170.
- the solenoid 10 may include a conductive housing 100. Located within the conductive housing 100, may be a two or more-piece cascading armature 170, and a pole member 180.
- the cascading armature 170 comprises a core 174 of conductive material slidably disposed within at least one conductive sleeve 176, which, in turn, is disposed in the housing 100.
- the cascading armature may contain multiple conductive sleeves in varying sizes and proportions to the core 174.
- the core 174 and sleeve 176 may be cylindrical in shape.
- the core 174 may have a conical or flat end 172, depending on the working stroke desired for the cascading armature.
- the core 174 may be a solid or hollow cylinder, slidably disposed within the sleeve 176 and arranged so that in the deactivated "resting" position the core face 172 is slightly recessed from the rim 179 of the sleeve 176.
- both the sleeve rim 179 and the core face 172 are presented to the pole member face 182 across the working air gap 200.
- the working air gap 200 is different for the core 174 and the sleeve 176 because the rim 179 of the sleeve extends beyond the core and is accordingly closer to the pole member face 182 than the core.
- FIG 3 is an example of the preferred embodiment of the present invention, in which like elements to those in Figure 1 are referred to with like reference numerals.
- the present invention may utilize a solenoid 10 with a telescoping (cascading) armature 170.
- the solenoid 10 may include a conductive housing 100, which, in turn, may include a conductive frame 110, a conductive coil 120, a conductive flux member 130, and an end cap 140, all of which define a central bore 150 in the solenoid.
- Located within the bore 150 are a two-piece cascading armature 170 and a pole member 180.
- a slidable plunger 190 is provided in a central bore through the pole member 180.
- the conductive frame 110, conductive flux member 130, and the pole member 180 may be made preferably of soft iron or fully annealed low carbon steel.
- the cascading armature 170 comprises a core 174 of conductive material slidably disposed within at least one conductive sleeve 176, which, in turn, is disposed in the bore 150.
- the cascading armature may contain multiple conductive sleeves.
- the core 174 and sleeve 176 may be cylindrical in shape.
- the core 174 may have a conical or flat end 172, depending on the working stroke desired for the cascading armature.
- Flat ended cascading armatures are generally used for short stroke applications.
- Conical ended cascading armatures, as shown in Fig. 4 may have a 90° cone for medium stroke units or a 60° cone for longer stroke devices.
- the sleeve 176 may be a thin walled cylinder having one end partially closed by a lip.
- a stop washer (ring) 178 constructed of non-conductive material.
- the lip of the sleeve 176 engages the edge of the stop washer (ring) 178.
- the stop washer (ring) 178 may be flat, or may be slightly curved to impart a "spring" action to assist in the downward movement of the cascading armature 170 upon actuation of the solenoid, as shown in Fig. 5. It is also envisioned that the stop washer (ring) 178 may be composed of either a conductive or non-conductive spring mechanism to assist in the downward movement of the cascading armature 170.
- the core 174 may be a solid cylinder, slidably disposed within the sleeve 176 and arranged so that in the deactivated "resting" position the core face 172 is slightly recessed from the rim 179 of the sleeve 176.
- both the sleeve rim 179 and the core face 172 are presented to the pole member face 182 across the working air gap 200.
- the working air gap 200 is different for the core 174 and the sleeve 176 because the rim 179 of the sleeve extends beyond the core and is accordingly closer to the pole member face 182 than the core.
- the coil 120 may comprise a copper winding that is energized with a voltage and produces a current flow in the winding.
- a magnetic field is developed as current flows through the winding.
- the magnetic field seeks a path or medium through which to flow, thus setting up a magnetic flux in the solenoid 10.
- the flux enters the cascading armature 170 through the conductive flux member 130 and causes an attractive force between the cascading armature sleeve 176/core 174 and the pole member 180.
- the flux may be concentrated in the shorter gap between the sleeve rim 179 and the pole member face 182.
- the attractive force between the sleeve 176 and the pole member 180 is enhanced by the proximity of the sleeve rim 179 to the pole member face 182. This attractive force may result in the sleeve 176 sliding towards the pole member 180 in the bore 150.
- contact between the end washer (ring) 178 and the core 174 causes the core to advance with the sleeve toward the pole member.
- the sleeve 176 and core 174 may advance together until the sleeve rim 179 contacts the pole member face 182.
- contact between the cascading armature 170 and the pole member face 182 would be undesirable because intimate contact of the cascading armature with the pole member could constitute a magnetic short circuit eliminating magnetic flux. If such a magnetic short circuit occurred, the conditions that create the attractive force would thus be satisfied and the attractive force may be greatly reduced.
- the area of the sleeve rim 179 that contacts the pole member face 182 may be sized to allow saturation to occur, limiting the flux carried by this path.
- the core 174 has advanced far enough toward the pole member 180 that the remaining flux present (attractive force) is sufficient to complete the working downward stroke of the cascading armature 170.
- the magnetic flux in the sleeve 176 may be saturated and accordingly seeks another path and begins to flow into an adjacent sleeve or core 174.
- the movement of the cascading armature 170 towards the pole member 180 is ultimately restricted by contact with the pole member and full displacement of the plunger 190.
- an upward bias provided by the plunger 190 may cause the cascading armature to return to the deactivated "resting" position.
- the cascading armature 170 may function similarly to a hydraulic or pneumatic telescoping cylinder or rod.
- the cascading armature may comprise a series of nested sleeves capable of conducting a magnetic flux, arranged so that adjacent sleeves will respond proportionally to changes in the flux magnitude.
- the alternative embodiment of the present invention may utilize a solenoid 10 with a cascading armature 170 which may consist of more than one sleeve, i.e., an inner conductive sleeve 176 and an outer conductive sleeve 173.
- the solenoid 10 may include a conductive housing 100, which, in turn, may include a conductive frame 110, a conductive coil 120, a conductive flux member 130, and an end cap 140, all of which define a central bore 150 in the solenoid.
- Located within the bore 150 are a three (or more)-piece cascading armature 170 and a pole member 180.
- a slidable plunger 190 is provided in a central bore through the pole member 180.
- the conductive frame 110, conductive flux member 130, and the pole member 180 may be made preferably of soft iron or fully annealed low carbon steel.
- the cascading armature 170 comprises a core 174 of conductive material slidably disposed within an inner conductive sleeve 176, which is slidably disposed within an outer conductive sleeve 173, which, in turn, is disposed in the bore 150.
- the cascading armature may include any number of sleeves.
- the core 174, the inner sleeve 176, and the outer sleeve 173 may be cylindrical in shape.
- the core 174 may have a conical or flat end 172, depending on the working stroke desired for the cascading armature.
- Flat ended cascading armatures are generally used for short stroke applications.
- Conical ended cascading armatures, as shown in Fig. 5, may have a 90° cone for medium stroke units or a 60° cone for longer stroke devices.
- the inner sleeve 176 and the outer sleeve 173 may be thin walled cylinders having one end partially closed by a lip. Disposed internally in the same end of the inner sleeve 176 may be a stop washer (ring) 178 constructed of non-conductive material. There may also be a stop washer (ring) 177 disposed between the inner sleeve 176 and the outer sleeve 173.
- the stop washer (ring) 178 and 177 may also be curved or composed of a spring to assist in the downward motion of the cascading armature 170 as previously discussed.
- the core 174 may be a solid cylinder, slidably disposed within the inner sleeve 176, which, in turn, is slidably disposed within outer sleeve 173 and arranged so that in the deactivated "resting" position the core face 172 is slightly recessed from the rim 179 of the inner sleeve 176, and the rim 179 of the inner sleeve 176 is slightly recessed from the rim 175 of the outer sleeve 173.
- both the inner sleeve rim 179, the outer sleeve rim 175, and the core face 172 are presented to the pole member face 182 across the working air gap 200.
- the working air gap 200 is different for the core 174 and the inner sleeve 176 because the rim 179 of the inner sleeve extends beyond the core and is accordingly closer to the pole member face 182 than the core 174.
- the working air gap 200 is different for the inner sleeve 176 and the outer sleeve 173 because the rim 175 of the outer sleeve extends beyond the inner sleeve 176 and is accordingly closer to the pole member face 182 than the inner sleeve rim 179.
- the coil 120 may comprise a copper winding that is energized with a voltage and produces a current flow in the winding.
- a magnetic field is developed as current flows through the winding.
- the magnetic field seeks a path or medium through which to flow, thus setting up a magnetic flux in the solenoid 10.
- the flux enters the cascading armature 170 through the conductive flux member 130 and causes an attractive force between the cascading armature inner sleeve 176/outer sleeve 173/core 174, and the pole member 180.
- the flux may be concentrated in the shorter gap between the outer sleeve rim 175 and the pole member face 182.
- the attractive force between the outer sleeve 173 and the pole member 180 is enhanced by the proximity of the outer sleeve rim 175 to the pole member face 182. This attractive force may result in the outer sleeve 173 sliding towards the pole member 180 in the bore 150. As the outer sleeve 173 moves toward the pole member 180.
- the area of the outer sleeve rim 175 that contacts the pole member face 182 may be sized to allow saturation to occur, limiting the flux carried by this path.
- the inner sleeve 176 has advanced far enough toward the pole member 180 that the remaining flux present (attractive force) is sufficient to cause the inner sleeve 176, and the core 174, to continue to move towards the pole face 182.
- the magnetic flux in the outer sleeve 173 may be saturated and accordingly seeks another path and begins to flow into the inner sleeve 176 and the core 174.
- the core 174 has advanced far enough toward the pole member 180 that the remaining flux present (attractive force) is sufficient to complete the working downward stroke of the cascading armature 170.
- magnetic flux in the inner sleeve 176 may be saturated and accordingly seeks another path and begins to flow into the core 174.
- the movement of the cascading armature 170 towards the pole member 180 is ultimately restricted by contact with the pole member and full displacement of the plunger 190.
- an upward bias provided by the plunger 190 may cause the cascading armature 170 to return to the resting position.
- the cascading armature of the present invention may provide a solenoid with increased mechanical advantage, and allow the solenoid to operate with less voltage.
- the cascading armature may also provide a working stroke for the armature which is longer than the initial working air gap, and thus is longer for a given solenoid voltage. Further, for the same magnetic intensity, the cascading armature may create a downward force on the solenoid plunger about
- Options include the ability to incorporate multiple tiers of cascading sleeves, or armatures composed of powder metal (e.g. P45, FH000, FH008, low carbon alloy, inconal, or magnetic ceramics) or other suitable materials. Composites with different materials on the stop washers are also envisioned. Magnetic flux may also be increased by increasing amperage or the number of coil turns. Also, due to the cascading action of the armature, the position of the cascading armature may be controlled by precisely controlling the voltage. Conventional solenoids are simple on or off devices. The cascading armature allows the solenoid to be on, off, or partially on or off.
- the cascading armature By regulating the available voltage the cascading armature can be used to operate incrementally to produce specific motion at a specific input voltage or current.
- the cascading armature allows the solenoid valve to actuate at lower voltages thus reducing the amount of current needed for operation without sacrifices to the working gap, stroke, or returning mechanism.
- a further advantage is seen in a reduction of sliding friction by virtue of having two concentric members separated by a film of lubricating oil. During the side load that results from the proximity to the flux ring, the additional oil film between the sleeve and plug creates an essentially frictionless condition during the short actuation period.
- the core and the conductive sleeves, as well as the stop washer may be composed of any of a number of materials.
- the core and the conductive sleeves can be any shape or size, depending upon the specific application.
- the core need not be completely solid, nor need it be composed of one uniform material.
- the working air gap is not limited to specific ranges or ratios, and may vary depending on the individual structure and components of the present invention. Further, it may be appropriate to make additional modifications or changes to the solenoid itself without departing from the scope of the invention.
- the solenoid housing may be constructed in any shape or size to accommodate the cascading armature.
- the coils may be modified to provide a more discrete range of voltages to permit the precise actuation of the solenoid.
Landscapes
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Electromagnets (AREA)
- Magnetically Actuated Valves (AREA)
Abstract
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2000519446A JP2001522140A (en) | 1997-11-03 | 1998-11-03 | Cascade electromagnetic armature |
EP98956490A EP1029332A4 (en) | 1997-11-03 | 1998-11-03 | Cascading electromagnetic armature |
KR1020007004826A KR20010031761A (en) | 1997-11-03 | 1998-11-03 | Cascading electromagnetic armature |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US6403597P | 1997-11-03 | 1997-11-03 | |
US60/064,035 | 1997-11-03 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1999023674A1 true WO1999023674A1 (en) | 1999-05-14 |
Family
ID=22053136
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US1998/023342 WO1999023674A1 (en) | 1997-11-03 | 1998-11-03 | Cascading electromagnetic armature |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP1029332A4 (en) |
JP (1) | JP2001522140A (en) |
KR (1) | KR20010031761A (en) |
WO (1) | WO1999023674A1 (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2001025614A1 (en) * | 1999-10-07 | 2001-04-12 | Robert Bosch Gmbh | Fuel injection valve |
KR100371430B1 (en) * | 2001-02-07 | 2003-02-12 | 안수길 | electromagnet for high speed solenoid valve |
US7078833B2 (en) * | 2002-05-31 | 2006-07-18 | Minebea Co., Ltd. | Force motor with increased proportional stroke |
WO2011113640A1 (en) * | 2010-03-15 | 2011-09-22 | Robert Bosch Gmbh | Fuel injector |
CN103221677A (en) * | 2010-11-22 | 2013-07-24 | 罗伯特·博世有限公司 | Fuel injector |
US10607758B2 (en) | 2015-12-14 | 2020-03-31 | Eto Magnetic Gmbh | Electromagnetic actuator as well as actuating system |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1743196A (en) * | 1927-06-06 | 1930-01-14 | Peter J Dugan | Solenoid construction |
US2411778A (en) * | 1942-09-22 | 1946-11-26 | Penn Electric Switch Co | Gun firing solenoid |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE447310C (en) * | 1925-08-01 | 1927-07-22 | Ferdinand Steinert Fa | Electromagnet |
US3961298A (en) * | 1975-05-07 | 1976-06-01 | The Singer Company | Dual plunger solenoid |
US4327345A (en) * | 1979-09-04 | 1982-04-27 | The Bendix Corporation | Solenoid having a multi-piece armature |
AUPN391295A0 (en) * | 1995-06-30 | 1995-07-27 | Orbital Engine Company (Australia) Proprietary Limited | Fuel injection apparatus |
-
1998
- 1998-11-03 JP JP2000519446A patent/JP2001522140A/en not_active Withdrawn
- 1998-11-03 WO PCT/US1998/023342 patent/WO1999023674A1/en not_active Application Discontinuation
- 1998-11-03 EP EP98956490A patent/EP1029332A4/en not_active Withdrawn
- 1998-11-03 KR KR1020007004826A patent/KR20010031761A/en not_active Application Discontinuation
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1743196A (en) * | 1927-06-06 | 1930-01-14 | Peter J Dugan | Solenoid construction |
US2411778A (en) * | 1942-09-22 | 1946-11-26 | Penn Electric Switch Co | Gun firing solenoid |
Non-Patent Citations (1)
Title |
---|
See also references of EP1029332A4 * |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6510841B1 (en) | 1999-10-06 | 2003-01-28 | Robert Bosch Gmbh | Fuel injection valve |
WO2001025614A1 (en) * | 1999-10-07 | 2001-04-12 | Robert Bosch Gmbh | Fuel injection valve |
KR100371430B1 (en) * | 2001-02-07 | 2003-02-12 | 안수길 | electromagnet for high speed solenoid valve |
US7078833B2 (en) * | 2002-05-31 | 2006-07-18 | Minebea Co., Ltd. | Force motor with increased proportional stroke |
WO2011113640A1 (en) * | 2010-03-15 | 2011-09-22 | Robert Bosch Gmbh | Fuel injector |
CN102792003A (en) * | 2010-03-15 | 2012-11-21 | 罗伯特·博世有限公司 | Fuel injector |
CN102792003B (en) * | 2010-03-15 | 2015-06-17 | 罗伯特·博世有限公司 | Fuel injector |
RU2555066C2 (en) * | 2010-03-15 | 2015-07-10 | Роберт Бош Гмбх | Fuel atomiser |
CN103221677A (en) * | 2010-11-22 | 2013-07-24 | 罗伯特·博世有限公司 | Fuel injector |
US10607758B2 (en) | 2015-12-14 | 2020-03-31 | Eto Magnetic Gmbh | Electromagnetic actuator as well as actuating system |
Also Published As
Publication number | Publication date |
---|---|
KR20010031761A (en) | 2001-04-16 |
JP2001522140A (en) | 2001-11-13 |
EP1029332A1 (en) | 2000-08-23 |
EP1029332A4 (en) | 2001-01-24 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4779582A (en) | Bistable electromechanical valve actuator | |
EP0640751B1 (en) | Electrically controlled timing adjustment for compression release engine brakes | |
JP4392555B2 (en) | Single-coil solenoid with a permanent magnet and a permanent magnet, its manufacturing method, non-magnetic switch for single-coil solenoid, single-coil solenoid kit | |
CA2165470C (en) | Electromagnetically actuated valve | |
US4455543A (en) | Electromagnetically operating actuator | |
EP2504606B1 (en) | Bi-stable solenoid shock absorber assembly | |
US20050046531A1 (en) | Electromagnetic valve system | |
US4686501A (en) | Electromagnetic actuator comprising at least two distinct magnetic circuits | |
KR100215958B1 (en) | Core design for electromagnetically actuated valve | |
US6166896A (en) | Method of increasing the cast-off speed of the armature in an electromagnetic actuator | |
US10927907B2 (en) | Control method of an electromagnetic brake with a controllable armature disc movement | |
US6230674B1 (en) | Electromagnetically driven valve for an internal combustion engine | |
US20040113731A1 (en) | Electromagnetic valve system | |
US5422617A (en) | Multiple coil, multiple armature solenoid | |
US5903070A (en) | Electromagnetic actuator having a slender structure | |
US20140291092A1 (en) | Shock absorber system and method | |
WO1999023674A1 (en) | Cascading electromagnetic armature | |
US5010312A (en) | Solenoid actuators | |
EP1288489A3 (en) | Linear control valve for controlling a fuel injector and engine compression release brake actuator and engine using same | |
JP2006503228A (en) | Solenoid valve system | |
GB2089478A (en) | Solenoid valve | |
DE19905492C1 (en) | Electromagnetic control of gas exchange valves in combustion engine, producing braking pulse against movement of armature in at least one phase of operating cycle | |
SU1177579A1 (en) | Air distributor | |
US6578536B1 (en) | Actuator assembly for electrohydraulic operation of cylinder valves | |
DE10137640A1 (en) | Electromagnetic actuator device has all interacting pole faces of armature and electromagnet arranged coaxially with respect to each other as cylindrical surfaces with air gap radius difference |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AK | Designated states |
Kind code of ref document: A1 Designated state(s): BR JP KR MX |
|
AL | Designated countries for regional patents |
Kind code of ref document: A1 Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LU MC NL PT SE |
|
121 | Ep: the epo has been informed by wipo that ep was designated in this application | ||
DFPE | Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101) | ||
WWE | Wipo information: entry into national phase |
Ref document number: 1020007004826 Country of ref document: KR Ref document number: PA/A/2000/004292 Country of ref document: MX |
|
ENP | Entry into the national phase |
Ref document number: 2000 519446 Country of ref document: JP Kind code of ref document: A |
|
WWE | Wipo information: entry into national phase |
Ref document number: 1998956490 Country of ref document: EP |
|
WWP | Wipo information: published in national office |
Ref document number: 1998956490 Country of ref document: EP |
|
WWW | Wipo information: withdrawn in national office |
Ref document number: 1998956490 Country of ref document: EP |
|
WWP | Wipo information: published in national office |
Ref document number: 1020007004826 Country of ref document: KR |
|
WWW | Wipo information: withdrawn in national office |
Ref document number: 1020007004826 Country of ref document: KR |