WO2003033933A1 - Verfahren zur herstellung einer rohrfeder sowie aktoreinheit mit einer solchen rohrfeder - Google Patents
Verfahren zur herstellung einer rohrfeder sowie aktoreinheit mit einer solchen rohrfeder Download PDFInfo
- Publication number
- WO2003033933A1 WO2003033933A1 PCT/DE2002/003718 DE0203718W WO03033933A1 WO 2003033933 A1 WO2003033933 A1 WO 2003033933A1 DE 0203718 W DE0203718 W DE 0203718W WO 03033933 A1 WO03033933 A1 WO 03033933A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- hollow body
- recesses
- tube
- spring
- actuator unit
- Prior art date
Links
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 9
- 238000000034 method Methods 0.000 claims abstract description 26
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 15
- 239000010959 steel Substances 0.000 claims abstract description 15
- 239000000446 fuel Substances 0.000 claims abstract description 6
- 238000005520 cutting process Methods 0.000 claims description 15
- 239000000463 material Substances 0.000 claims description 9
- 229910000639 Spring steel Inorganic materials 0.000 claims description 5
- 238000010894 electron beam technology Methods 0.000 claims description 2
- 239000000945 filler Substances 0.000 claims description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 2
- 238000003698 laser cutting Methods 0.000 abstract description 4
- 229910052751 metal Inorganic materials 0.000 description 7
- 239000002184 metal Substances 0.000 description 7
- 238000002347 injection Methods 0.000 description 6
- 239000007924 injection Substances 0.000 description 6
- 238000013461 design Methods 0.000 description 5
- 238000004080 punching Methods 0.000 description 4
- 238000003466 welding Methods 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 229910000952 Be alloy Inorganic materials 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 210000000988 bone and bone Anatomy 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000036316 preload Effects 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F1/00—Springs
- F16F1/02—Springs made of steel or other material having low internal friction; Wound, torsion, leaf, cup, ring or the like springs, the material of the spring not being relevant
- F16F1/025—Springs made of steel or other material having low internal friction; Wound, torsion, leaf, cup, ring or the like springs, the material of the spring not being relevant characterised by having a particular shape
- F16F1/028—Springs made of steel or other material having low internal friction; Wound, torsion, leaf, cup, ring or the like springs, the material of the spring not being relevant characterised by having a particular shape cylindrical, with radial openings
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10N—ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10N30/00—Piezoelectric or electrostrictive devices
- H10N30/80—Constructional details
- H10N30/88—Mounts; Supports; Enclosures; Casings
- H10N30/886—Additional mechanical prestressing means, e.g. springs
-
- 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
- F02M2200/00—Details of fuel-injection apparatus, not otherwise provided for
- F02M2200/21—Fuel-injection apparatus with piezoelectric or magnetostrictive elements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F2226/00—Manufacturing; Treatments
-
- Y—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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49405—Valve or choke making
-
- Y—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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/496—Multiperforated metal article making
-
- Y—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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49609—Spring making
Definitions
- the invention relates to a method for producing a tubular spring, in particular for an actuator unit of a fuel injector, and to such an actuator unit with a tubular spring.
- piezo actuator elements as switching and actuating elements.
- piezostacks which consist of piezo units stacked on top of one another, are elastically prestressed for reasons of durability.
- the pre-stressing elements used for this must exert very high pre-stressing forces with a small construction volume. They should also have a relatively low stiffness and a simple and robust design. Durability under high dynamic loads is also required.
- a generic Bourdon tube for biasing a piezoelectric actuator of a fuel injector is also known from DE 198 35 628 AI.
- This Bourdon tube consists of a thin-walled hollow cylinder into which a large number of recesses in the form of bones are made. These recesses bring about a desired longitudinal elasticity of the Bourdon tube.
- This known Bourdon tube requires a relatively complex production, since the recesses are made in a stamping process.
- a flat steel sheet must be brought into a cylindrical shape after the punching process and welded to its butt edge.
- An object of the invention is to provide a method for producing a pretensioning element for an actuator element of an actuator unit, which has a high elasticity.
- a thin-walled metal tube is provided with a plurality of regularly arranged, elongated recesses by means of jet cutting.
- the recesses which are elongated, ensure that the hollow body also has sufficient strength, even with the biases usually applied to the piezoelectric actuator from approx. 800 N to 1000 N, and at the same time is sufficiently elastic to carry out the longitudinal movements generated by the piezoelectric actuator is.
- jet cutting it is possible to cut very narrow and small recesses in the cylindrical hollow body. bring how they could not be introduced in this form by means of a punching process. This means that significantly more recesses can be accommodated in the same area, which leads to a significant reduction in the spring rate of the beam-cut version of the Bourdon tube.
- typical dimensions of punched recesses are predefined within relatively narrow limits due to the required minimum dimensions of the punch and the associated punching time of the punch.
- the number of recesses per unit area is also limited in the case of punched recesses, which leads to a relatively high spring rate.
- the hollow body can preferably have a cylindrical contour.
- a thin-walled, seamless drawn steel tube is particularly suitable as the material for the hollow body.
- Laser beam cutting, water jet cutting or electron beam cutting, for example, is suitable as the beam cutting method. All of these jet cutting processes can be carried out with high precision and lead to very precise and dimensionally accurate workpieces.
- a first embodiment of the method according to the invention provides that by using a suitable filler body in the interior of the hollow cylinder during jet cutting, a defined shape of the jet exit edge is achieved and damage to the opposite side is prevented.
- each recess is oriented essentially perpendicular to the cylinder central axis of the tube spring. That way a desired spring stiffness is impressed on the tubular spring in the direction of its longitudinal axis.
- the recesses are arranged in rows, the recesses of adjacent rows being arranged laterally offset from one another. This design has the advantage of an ideal suspension behavior of the Bourdon tube, since the alternating webs and recesses can lead to a possible impression of the recesses, the webs in between being able to maintain their shape.
- a minimum distance between adjacent recesses in two rows is 0.3 to 4 times the wall thickness of the cylindrical hollow body of the tubular spring.
- An ideal spring constant can be selected depending on the dimensions of the recesses and the wall thickness of the Bourdon tube.
- the design of the Bourdon tube according to the invention offers the possibility of choosing between a relatively large number of possible materials, since the stresses can be reduced while the spring rate remains the same. For example, materials can be selected which have low strength but which will follow later
- Welding processes represent the best possible pairing of materials. Furthermore, materials can also be selected that are optimally suited for the beam cutting process or the laser cutting process, i.e. those with a relatively low sulfur content of less than 0.25%.
- the seamless drawn metal tube used for the Bourdon tube preferably has a thickness of less than 1.0 mm.
- the strength can optionally also be chosen to be larger, in order in this way to achieve the desired spring stiffness even when steel of lower strength is used.
- the seamlessly drawn metal tube used for the tubular spring is preferably a spring steel, since such a relatively inexpensive elastic property also has very small dimensions.
- the recesses can each have a dumbbell-shaped contour with a constricted central area, which in turn can be used to influence the desired spring stiffness in a targeted manner.
- the following advantages of the method according to the invention result.
- a jet cutting process By using a jet cutting process, a high accuracy of the recesses in the Bourdon tube is achieved.
- no additional processing steps are required.
- a high surface quality can be achieved in the recesses, which would not be achievable by means of a punching process.
- An actuator unit has a thin-walled cylindrical hollow body which is arranged around a piezoelectric actuator element, the hollow body being elastic and prestressing the actuator element and the hollow body being a metal tube provided with a plurality of elongate recesses, in particular a seamlessly drawn one
- An actuator unit with such a cylindrical Guatemalal hollow body as a Bourdon tube can be provided with very precisely selected properties of the Bourdon tube.
- FIG. 1 shows an actuator unit in a schematic cross-sectional illustration
- FIG. 2 shows a tubular spring in a schematic side view, which is produced by means of the method according to the invention
- Figure 3 is a detailed view of a first embodiment of the Bourdon tube according to Figure 2 and
- Figure 4 is a detailed view of an alternative embodiment of the Bourdon tube.
- FIG. 1 shows an actuator unit 1, consisting of several stacked, piezoelectric individual elements.
- the piezoelectric actuator unit 1 is supplied with electrical voltage by means of contact pins 4.
- the contact pins 4 are each arranged along the actuator unit 1 and are in electrically conductive connection with the actuator element 2.
- a voltage between the contact pins 4 By applying a voltage between the contact pins 4, a longitudinal expansion of the piezoelectric actuator element 2 is generated, which can be used, for example, to set an injection valve of an internal combustion engine.
- the piezoelectric actuator element 2 with the contact pins 4 is arranged in a cylindrical hollow body designed as a tubular spring 12.
- the end faces of the piezoelectric actuator element 2 each abut a cover plate 6 or base plate 8, the upper cover plate 6 having passages 10 through which the contact pins 4 extend.
- the Ab- Cover plate 6 and the base plate 8 are each positively and / or non-positively, preferably by welding, connected to the Bourdon tube 12.
- the connection between the tubular spring 12 and the two plates 6, 8 can also be made with the help of a flanging, the flanged upper and lower edge regions of the hollow body engaging in the cover 6 and base plate 8, respectively.
- the piezoelectric actuator element 2 is biased by the two plates 6, 8, which are held in position by the tubular spring 12, with a defined force of preferably 800 N to 1000 N.
- the hollow body receiving the piezoelectric actuator element 2 is preferably made of spring steel, since spring steel is characterized by a high strength characteristic.
- spring steel is characterized by a high strength characteristic.
- other materials for example materials with a low modulus of elasticity, such as copper-beryllium alloys, can also be used.
- FIG. 2 shows the tubular spring 12 in side view.
- the tube spring 12 is a cylindrical hollow body which is made from a metal tube.
- a plurality of recesses 14 are made, which are produced by means of laser cutting.
- the elongated recesses are each oriented essentially perpendicular to the central axis 16 of the tubular spring 12.
- the recesses 14 are each arranged in rows, the recesses 14 of adjacent rows being arranged laterally offset from one another.
- the minimum distance between adjacent recesses 14 of two adjacent rows can be 0.3 to 4 times the wall thickness of the Bourdon tube.
- a seamlessly drawn steel tube for example made of spring steel, is particularly suitable as the metal tube.
- FIG. 3 shows a detailed view of the jacket surface 18 of the tubular spring 12 according to FIG. 2 provided with recesses 14.
- the recesses 14 are each designed like a club, so that they each have a constriction in a central area. This design has a favorable effect on the material load and thus enables the entire tubular spring 12 to have low spring stiffness.
- the recesses 14 can optionally be designed in the form of regular elongated holes or narrow rectangles, as is shown by way of example in FIG. 4. As contours for the recesses 14, almost any shape is possible, which leads to a lower spring rate in the axial direction of the Bourdon tube.
- the recesses can also be designed as elongated recesses with semicircular ends.
- the tubular spring can, for example, be made from a seamlessly drawn steel tube with a thickness of 1.0 mm or less.
- a steel tube with a thickness of more than 1.0 mm is particularly suitable if a steel of lower strength is used.
- a heat treatment can be carried out.
- any other abutting edge shapes can be formed, for example in the form of a sine wave or a zigzag line, a suitably shaped weld seam or spot welding then being used to fix the tubular spring.
- tubular spring 12 instead of fixing the tubular spring 12 by welding, it can also be fixed by the upper and lower plates 6, 8, so that the abutting edges only abut one another. This can result in an advantageous distribution of the pressure and spring forces in the hollow body.
- An embodiment of the actuator unit with an outer hollow body which is preferably designed as a tubular spring and in which the piezoelectric actuator is prestressed by means of form-fitting and / or non-positively connected upper and lower covers, enables simple transport and easy installation and removal, for example in an injection valve of an internal combustion engine, due to its compact design.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE50206834T DE50206834D1 (de) | 2001-10-09 | 2002-10-01 | Verfahren zur herstellung einer rohrfeder |
EP02801279A EP1434952B1 (de) | 2001-10-09 | 2002-10-01 | Verfahren zur herstellung einer rohrfeder |
US10/821,775 US7222424B2 (en) | 2001-10-09 | 2004-04-09 | Method for producing a tubular spring and an actuator unit comprising one such tubular spring |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10149746.6 | 2001-10-09 | ||
DE10149746A DE10149746C1 (de) | 2001-10-09 | 2001-10-09 | Verfahren zur Herstellung einer Rohrfeder sowie Aktoreinheit mit einer solchen Rohrfeder |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10/821,775 Continuation US7222424B2 (en) | 2001-10-09 | 2004-04-09 | Method for producing a tubular spring and an actuator unit comprising one such tubular spring |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2003033933A1 true WO2003033933A1 (de) | 2003-04-24 |
Family
ID=7701892
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/DE2002/003718 WO2003033933A1 (de) | 2001-10-09 | 2002-10-01 | Verfahren zur herstellung einer rohrfeder sowie aktoreinheit mit einer solchen rohrfeder |
Country Status (4)
Country | Link |
---|---|
US (1) | US7222424B2 (de) |
EP (1) | EP1434952B1 (de) |
DE (2) | DE10149746C1 (de) |
WO (1) | WO2003033933A1 (de) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2004097208A1 (de) * | 2003-05-02 | 2004-11-11 | Robert Bosch Gmbh | Aktoreinheit für ein piezogesteuertes kraftstoffeinspritzventil |
EP1508720A1 (de) * | 2003-08-19 | 2005-02-23 | Robert Bosch Gmbh | Rohrfeder für Aktor |
WO2006003038A1 (de) * | 2004-06-30 | 2006-01-12 | Robert Bosch Gmbh | Kraftstoffeinspritzventil |
WO2008014759A1 (de) * | 2006-07-28 | 2008-02-07 | Epcos Ag | Federelement sowie piezoaktor mit dem federelement |
CN100455841C (zh) * | 2007-03-30 | 2009-01-28 | 吉林大学 | 微弹簧的激光加工方法 |
EP1916439A3 (de) * | 2006-10-26 | 2009-11-04 | LuK Lamellen und Kupplungsbau Beteiligungs KG | Verfahren zum Herstellen eines Schlingenfederkupplungselements und Torsionsschwingungsdämpfer |
WO2012062438A3 (de) * | 2010-11-08 | 2012-10-04 | Starragheckert Ag | Einrichtung zur lagekorrektur von elementen einer werkzeugmaschine und kompensationselement dafür |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10340319A1 (de) * | 2003-09-02 | 2005-03-24 | Robert Bosch Gmbh | Ventileinrichtung, insbesondere Kraftstoffeinspritzventil für eine Brennkraftmaschine |
US7007894B1 (en) * | 2004-09-21 | 2006-03-07 | The Boeing Company | In-flight refueling system, damping device and method for preventing oscillations in in-flight refueling system components |
DE102004058715B4 (de) * | 2004-12-06 | 2010-08-12 | Continental Automotive Gmbh | Kraftstoffinjektor für eine Brennkraftmaschine sowie Verfahren zur Herstellung eines Kraftstoffinjektors |
DE102005046269B4 (de) * | 2005-09-27 | 2007-07-12 | Klaus Frietsch | Rohrfeder und Verfahren zu ihrer Herstellung |
US7765877B2 (en) * | 2007-11-30 | 2010-08-03 | Caterpillar Inc | System for preloading piezoelectric actuators and method |
US7950596B2 (en) * | 2008-06-27 | 2011-05-31 | Caterpillar Inc. | Distributed stiffness biasing spring for actuator system and fuel injector using same |
US7913929B2 (en) * | 2008-11-18 | 2011-03-29 | Continental Automotive Systems Us, Inc. | Modular outward opening piezo direct fuel injector |
DE102010008194A1 (de) | 2010-02-16 | 2011-08-18 | Steinbeis-Transferzentrum Mechatronik, 98693 | Adaptives Federelement |
DE102014116708A1 (de) * | 2014-07-23 | 2016-01-28 | Physik Instrumente (Pi) Gmbh & Co. Kg | Aktorvorrichtung |
WO2019140371A1 (en) | 2018-01-15 | 2019-07-18 | Cts Corporation | Pre-loaded piezoelectric stack actuator |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4826143A (en) * | 1985-10-22 | 1989-05-02 | U.S. Philips Corporation | Method of manufacturing a spring of the cylindrical type to be used at high temperature |
DE3844134A1 (de) | 1987-12-29 | 1989-07-13 | Toyota Motor Co Ltd | Stellantrieb fuer ein kraftstoff-einspritzventil |
US4919403A (en) * | 1986-10-07 | 1990-04-24 | Proprietary Technology, Inc. | Serpentine strip spring |
EP0514825A1 (de) * | 1991-05-21 | 1992-11-25 | FR- KONSTRUKTIONSELEMENTE FÜR ZAHNPROTHETIK GmbH & CO | Feder eines Riegelelementes für eine abnehmbare Zahnprothese |
WO2000008353A1 (de) * | 1998-08-06 | 2000-02-17 | Siemens Aktiengesellschaft | Piezoelektrische aktoreinheit |
WO2002052669A2 (en) * | 2000-12-22 | 2002-07-04 | Ballard Power Systems Inc. | Compression mechanism for an electrochemical fuel cell assembly |
Family Cites Families (8)
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FR1090004A (fr) * | 1953-07-22 | 1955-03-25 | Ressort | |
JPS57149085A (en) * | 1981-03-09 | 1982-09-14 | Nhk Spring Co Ltd | Formation of spring |
NL8105502A (nl) * | 1981-12-08 | 1983-07-01 | Philips Nv | Werkwijze voor het vervaardigen van een piezo-elektrische inrichting alsmede een inrichting vervaardigd volgens deze werkwijze. |
SU1031652A1 (ru) * | 1982-04-08 | 1983-07-30 | Предприятие П/Я А-1495 | Устройство дл резки труб |
US4858897A (en) * | 1987-11-16 | 1989-08-22 | Hideki Irifune | Spring |
EP1008191A1 (de) * | 1997-08-05 | 2000-06-14 | Siemens Aktiengesellschaft | Vorgespannter piezoelektrischer aktor |
DE19853103A1 (de) * | 1998-11-18 | 2000-05-25 | Bosch Gmbh Robert | Kraftstoffeinspritzsystem für Brennkraftmaschinen |
DE19901530C2 (de) * | 1999-01-16 | 2001-07-26 | Biotronik Mess & Therapieg | Vorrichtung zum Laserstrahl-Strukturieren von bioresorbierbaren, intraluminalen Gefäßwandstützen |
-
2001
- 2001-10-09 DE DE10149746A patent/DE10149746C1/de not_active Expired - Lifetime
-
2002
- 2002-10-01 WO PCT/DE2002/003718 patent/WO2003033933A1/de not_active Application Discontinuation
- 2002-10-01 DE DE50206834T patent/DE50206834D1/de not_active Expired - Lifetime
- 2002-10-01 EP EP02801279A patent/EP1434952B1/de not_active Expired - Lifetime
-
2004
- 2004-04-09 US US10/821,775 patent/US7222424B2/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4826143A (en) * | 1985-10-22 | 1989-05-02 | U.S. Philips Corporation | Method of manufacturing a spring of the cylindrical type to be used at high temperature |
US4919403A (en) * | 1986-10-07 | 1990-04-24 | Proprietary Technology, Inc. | Serpentine strip spring |
DE3844134A1 (de) | 1987-12-29 | 1989-07-13 | Toyota Motor Co Ltd | Stellantrieb fuer ein kraftstoff-einspritzventil |
EP0514825A1 (de) * | 1991-05-21 | 1992-11-25 | FR- KONSTRUKTIONSELEMENTE FÜR ZAHNPROTHETIK GmbH & CO | Feder eines Riegelelementes für eine abnehmbare Zahnprothese |
WO2000008353A1 (de) * | 1998-08-06 | 2000-02-17 | Siemens Aktiengesellschaft | Piezoelektrische aktoreinheit |
WO2002052669A2 (en) * | 2000-12-22 | 2002-07-04 | Ballard Power Systems Inc. | Compression mechanism for an electrochemical fuel cell assembly |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2004097208A1 (de) * | 2003-05-02 | 2004-11-11 | Robert Bosch Gmbh | Aktoreinheit für ein piezogesteuertes kraftstoffeinspritzventil |
US7420316B2 (en) | 2003-05-02 | 2008-09-02 | Robert Bosch Gmbh | Actuator unit for a piezo-controlled fuel injection valve |
EP1508720A1 (de) * | 2003-08-19 | 2005-02-23 | Robert Bosch Gmbh | Rohrfeder für Aktor |
WO2006003038A1 (de) * | 2004-06-30 | 2006-01-12 | Robert Bosch Gmbh | Kraftstoffeinspritzventil |
WO2008014759A1 (de) * | 2006-07-28 | 2008-02-07 | Epcos Ag | Federelement sowie piezoaktor mit dem federelement |
US7859169B2 (en) | 2006-07-28 | 2010-12-28 | Epcos Ag | Spring element for pretensioning a piezoelectric actuator and piezoelectric actuator with the spring element |
EP1916439A3 (de) * | 2006-10-26 | 2009-11-04 | LuK Lamellen und Kupplungsbau Beteiligungs KG | Verfahren zum Herstellen eines Schlingenfederkupplungselements und Torsionsschwingungsdämpfer |
CN100455841C (zh) * | 2007-03-30 | 2009-01-28 | 吉林大学 | 微弹簧的激光加工方法 |
WO2012062438A3 (de) * | 2010-11-08 | 2012-10-04 | Starragheckert Ag | Einrichtung zur lagekorrektur von elementen einer werkzeugmaschine und kompensationselement dafür |
CN103328153A (zh) * | 2010-11-08 | 2013-09-25 | 斯达拉格股份公司 | 用于机床元件的位置校正的装置和用于该装置的补偿元件 |
US9186764B2 (en) | 2010-11-08 | 2015-11-17 | Starrag Ag | Device for correcting the position of elements of a machine tool and compensation element therefor |
Also Published As
Publication number | Publication date |
---|---|
US20040195060A1 (en) | 2004-10-07 |
EP1434952B1 (de) | 2006-05-17 |
DE50206834D1 (de) | 2006-06-22 |
US7222424B2 (en) | 2007-05-29 |
EP1434952A1 (de) | 2004-07-07 |
DE10149746C1 (de) | 2003-05-28 |
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