| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 121 | METHOD FOR MANUFACTURING FRAME OF C- CLAMP, FRAME OF C-CLAMP AND C-CLAMP | PCT/FI2011050604 | 2011-06-22 | WO2011161322A2 | 2011-12-29 | KIVINIEMI JARI; MIINALA JUHA; LEHTO TIMO |
| The method comprises manufacturing a frame (10) of a C-clamp, which has a lower jaw (20), an upper jaw (30) and a mouth (26) between the lower jaw and upper jaw. The method comprises forming a lower end plate (22) and an upper end plate (32) and at least two frame plates (10a, 10b, 10c, 10d), which have a lower branch (12) and an upper branch (14). The lower branches of the frame plates are attached to the lower end plate and the upper branches to the upper end plate, so that the frame plates settle in a parallel manner at a distance (e) from each other. The joined frame plates and end plates form the frame of the C- clamp. The frame plates are formed by machining a steel plate of ultra-strength steel only with machining methods, which do not substantially heat up the material being machined. Suitable machining methods are for example chipping machining methods or water cutting. The lower branches are attached to the lower end plate and the upper branches are attached to the upper end plate by welding or with mechanical attaching means. The attaching point of the end plates is situated as far away as possible from the most stressed point in the frame plates, so a localized decrease in strength in the ultra-strength steel possibly caused by the welding does not affect the total strength of the frame in a decreasing way. The number of frame plates can be selected according to the strength requirements of the frame. There can thus be for example three, four, five, six, seven or eight frame plates. | ||||||
| 122 | RADIOPAQUE SUPER-ELASTIC INTRAVASCULAR STENT | PCT/US2009030220 | 2009-01-06 | WO2009089218A2 | 2009-07-16 | LUNDKVIST ANDRE S; WATSON DAVID A |
| The intravascular stent is formed from a composite wire includes an inner core of radiopaque metal, a polymer layer coaxially disposed about the inner core, and an outer metal layer coaxially disposed about the polymer layer. The intermediary polymer layer acts as a barrier material between the inner core and the outer sheath, so that the inner core and outer sheath may be made of dissimilar metallic layers, and the intermediary polymer layer will prevent a galvanic reaction between the inner core and the peripheral metal layer. The intravascular stent has ends flared radially outwardly to prevent radially and longitudinally inward deformation of the ends of the stent when the stent is disposed in a desired location in a patient's vasculature. | ||||||
| 123 | METHOD OF FORMING TURBINE BLADE ROOT | PCT/CA0201983 | 2002-12-27 | WO03059569A2 | 2003-07-24 | HOWLEY TODD |
| The present invention relates to a process for forming the root of a turbine blade using the EDM method. EDM machining of the root is done in a manner that any re-cast layer left behind is less than 1 micron. After EDM machining the turbine blade is subjected to MPT to check for depth or presence of surface cracks. A liquid tracer coating is then applied to the root, which allows the ability of the next process to be verified as complete. The root is then subjected to glass beeding to remove any re-cast and insure the surface finish prior to shot peening is consistent and contains no scratch marks or machine marks. The root is then subjected to shot peening to reduce residual tensile stresses by imparting to the surface small indentations or dimples and produce a compressed surface which resists further surface cracks. | ||||||
| 124 | METHOD FOR CONNECTING A FIBER COMPOSITE COMPONENT TO A STRUCTURAL COMPONENT OF AN AIR AND SPACECRAFT, AND A CORRESPONDING ARRANGEMENT | PCT/EP2010068802 | 2010-12-03 | WO2011069899A3 | 2011-08-11 | PACCHIONE MARCO; FURFARI DOMENICO |
| The invention relates to a method for connecting a fiber composite component (2) to a structural component (3) of an air and spacecraft, wherein a metal foil (4) is provided between the fiber composite component (2) and the structural component (3) as a transverse reinforcement element. Said foil is designed having at least one anchoring segment (7) protruding from the surface (9) facing the fiber composite component (2), and inserted between the fiber composite component (2) and the structural component (3). A corresponding arrangement is produced according to said method. | ||||||
| 125 | MACHINE TOOL, PARTICULARLY FOR MILLING A TURBOCHARGER COMPRESSOR IMPELLER | PCT/EP2009001229 | 2009-02-20 | WO2009106268A3 | 2009-11-26 | PRUST DIRK; DEUFEL KARL |
| The invention relates to a machine tool for the machining, particularly for the machining by turning and milling, of work pieces (25) having a centric bore (251), having a tool holder (19, 22) for holding a tool (23), a work piece support (13) for supporting the work piece (25), a work piece mount (30) for fixing the work piece (25), and a drive means (33) for turning the work piece (25) about a centric rotational axis (35). In order to be able to machine work pieces (25) intended for operation at a very high rotational speeds with high precision such that balancing after machining can preferably be completely eliminated, the invention provides that the work piece support (13) comprises a mandrel (36) for attaching the work piece (25) such that a section of the mandrel (36) projects into the bore (251) on a first side (252) of the work piece (25), and that the work piece support (30) has a counter holder (30) that can be moved in the direction of the bore axis (255) of the centric bore (251) for applying a pressing force onto the work piece (25) acting in the direction of the bore axis (255) on a second side (250) positioned opposite the first side (252). | ||||||
| 126 | RADIOPAQUE SUPER-ELASTIC INTRAVASCULAR STENT | PCT/US2009030217 | 2009-01-06 | WO2009089216A3 | 2009-10-29 | LUNDKVIST ANDRE S; WATSON DAVID A |
| The intravascular stent is formed from a composite wire includes an inner core (12) of radiopaque metal, a polymer layer (16) coaxially disposed about the inner core, and an outer metal layer (18) coaxially disposed about the polymer layer. The intermediary polymer layer acts as a barrier material between the inner core and the outer sheath, so that the inner core and outer sheath may e made of dissimilar metallic layers, and the intermediary polymer layer will prevent a galvanic reaction between the inner core and the peripheral metal layer. The intravascular stent (20) has ends (22,24) flared radially outwardly to prevent radially and longitudinally inward deformation of the ends of the stent when the stent is disposed in a desired location in a patient's vasculature. | ||||||
| 127 | METHOD FOR MANUFACTURING PRODUCT MEMBER, AND PRODUCT MEMBER | EP16835004.9 | 2016-07-29 | EP3336206A1 | 2018-06-20 | IWASAKI, Tatsuya; WATARI, Koji |
Provided are a product member having excellent wear resistance, bending fatigue strength, and machinability, whereby wear of a cutting tool during a manufacturing process can be suppressed, and a method for manufacturing the same. The present invention includes: a step for subjecting a rough member to induction hardening and annealing, and obtaining a hardened material, in which the frequency during high-frequency heating is set to 10 kHz to 300 kHz, the heating time during high-frequency heating is set to 1 second to 60 seconds, the annealing temperature is set to 160°C to 200°C, and the annealing time is set to 60 minutes to 180 minutes; and a step for subjecting the hardened material to cutting, and obtaining a product member, in which the rake angle of a cutting tool is set to more than -30° to -5° or less, a nose radius of the tool is set to 0.4 mm to 1.2 mm, a feed rate is set to more than 0.1 mm/rev to 0.4 mm/rev, the cutting speed is set to 50 m/minute to 150 m/minute, and the cut depth is set to 0.05 mm to 0.2 mm. |
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| 128 | PUNCHING DEVICE, PUNCH AND METHOD | EP16382429.5 | 2016-09-14 | EP3296047A1 | 2018-03-21 | HERRERO, Alberto José; PARDAVILA, Mikel |
Punching device (1) for punching a workpiece (12), the punching device (1) comprising a punching part (2) and a broaching part (3). The punching part (2) comprises a punching cutting edge (21) that limits a punching cutting area (22), the punching part (2) being intended to pierce the workpiece (12). The broaching part (3) is intended to tear the workpiece (12) later than the punching part (2), and comprises at least a broaching tooth (4, 5, 6, 7, 8) comprising a cutting edge (41, 51, 61, 71, 81) that limits a cutting area (42, 52, 62, 72, 82) which is greater than the punching cutting area (22).
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| 129 | PROCEDE DE FABRICATION PAR SOUDAGE DIFFUSION D'UNE PIECE MONOBLOC POUR UNE TURBOMACHINE | EP12728667.2 | 2012-05-11 | EP2709783B1 | 2017-11-15 | GODON, Thierry; DAMBRINE, Bruno, Jacques, Gérard |
| 130 | BREMSSCHEIBE UND VERFAHREN ZUR BEHANDLUNG DER OBERFLÄCHE EINER BREMSSCHEIBE | EP11779422.2 | 2011-11-08 | EP2659158B1 | 2017-09-20 | SCHOEPF, Martin; SCHAEFER, Bernd |
| 131 | VERFAHREN ZUM ANBINDEN EINES FASERVERBUNDBAUTEILS AN EIN STRUKTURBAUTEIL EINES LUFT- UND RAUMFAHRZEUGES UND EINE ENTSPRECHENDE ANORDNUNG | EP10784813.7 | 2010-12-03 | EP2509772B1 | 2017-06-28 | PACCHIONE, Marco; FURFARI, Domenico |
| 132 | VERFAHREN ZUR HERSTELLUNG EINES FRACHTTORS | EP10775717.1 | 2010-10-22 | EP2490854B1 | 2017-05-10 | HECKL, Matthias; HÖNLE, Christian; HESTERMANN, Fritz; STALLA, Reinhold |
| 133 | Verfahren und Vorrichtung zur Fertigbearbeitung von Werkstücken | EP12184802.2 | 2012-09-18 | EP2570229B1 | 2016-08-03 | Dr. Schreiber, Leo; Weber, Matthias |
| 134 | PLATE-SHAPED WORKPIECE FORMING METHOD AND FORMED WORKPIECE | EP12764717 | 2012-03-06 | EP2692457A4 | 2014-09-10 | SUGAI ATSUSHI; MATSUNAGA YU; OGURA DAISUKE; MORIMOTO SHOICHI; ARIMA MINORU; KANEDA YUICHI; EGAMI AKIHIKO |
| A tip-bend forming method for machining pockets while a curved, plate-shaped workpiece is in a flattened state, without depending on novel machining equipment, wherein the curve radius of the plate-shaped workpiece after the pockets have been machined is prevented from becoming smaller than a completed curve radius due to spring-in. A plate-shaped workpiece (2) forming method for post-machining pockets (3) into the curved inner surface of the workpiece (2) while the plate-shaped workpiece (2), which has been curved by a curve-forming machine (10), is in a flattened state, the forming method having: a curve-forming step (A) for estimating in advance the amount that spring-in will cause the curve radius of the plate-shaped workpiece (2) to shrink after machining of the pockets (3) compared to before the machining thereof, setting a net curve radius (Ro) obtained by adding a curve-radius shrinkage amount (R 1 ) caused by spring-in to the completed curve radius (R) of the plate-shaped workpiece (2), and forming the curve in the plate-shaped workpiece (2) so as to achieve the net curve radius (R 0 ); and a pocket-machining step for flattening the curved, plate-shaped workpiece (2), and post-machining pockets (3) therein. | ||||||
| 135 | Method of manufacturing mirror shells of a nested shells grazing incidence mirror | EP12008518.8 | 2012-12-20 | EP2746850A1 | 2014-06-25 | Metzmacher, Christof Dr.; Schürmann, Max Christian Dr. |
The present invention relates to a method of manufacturing mirror shells (11) of a nested shells grazing incidence mirror, in particular for EUV radiation and/or X-rays. In the method a blank (1) of a bulk material is provided and machined to form a mirror body (2) of the shell (11). Mechanical structures (3, 4) are integrated and/or attached to the mirror body (2) during and/or after the machining step. The mechanical structures (3, 4) are required for mounting and/or operating the mirror shells (11). After these steps the optical surface (7) is formed on the mirror body (2) by diamond turning. The proposed method allows the manufacturing of mirror shells of a nested shells grazing incidence mirror at low costs with high optical quality which may also be refurbished one or several times.
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| 136 | BREMSSCHEIBE UND VERFAHREN ZUR BEHANDLUNG DER OBERFLÄCHE EINER BREMSSCHEIBE | EP11779422.2 | 2011-11-08 | EP2659158A1 | 2013-11-06 | SCHOEPF, Martin; SCHAEFER, Bernd |
| The invention relates to a brake disc and to a method for treating a surface of a brake disc (1), wherein, in order to increase the adhesive power of a coating to the surface, said surface is roughened by introducing at least one depression (5) in the surface, the width of said depression widening with increasing depth of the depression. By means of said undercut, a positive connection is created between the brake disc and the coating. | ||||||
| 137 | WERKZEUGMASCHINE, INSBESONDERE ZUM TURBOLADER-VERDICHTERRADFRÄSEN | EP09715207.8 | 2009-02-20 | EP2254717B3 | 2013-11-06 | PRUST, Dirk; DEUFEL, Karl |
| 138 | VERFAHREN ZUR HERSTELLUNG EINER VENTILATIONSBOHRUNG IN EINEM LAGERSTUHL EINES KURBELGEHÄUSES EINER HUBKOLBEN-BRENNKRAFTMASCHINE | EP11749742.0 | 2011-08-26 | EP2622197A1 | 2013-08-07 | TÄNZER, Lars; KRÖNINGER, Hans-Rainer |
| The invention relates to a method for producing a ventilation bore (1) in a thrust bearing (2) of a crankcase (3) of a reciprocating internal combustion engine by milling, wherein the milling cutter (4) is an angled head milling cutter, which is introduced into the crankcase (3) in the direction of a cylinder longitudinal axis (Z) and is moved in the direction of a crankcase longitudinal axis (K) until the thrust bearing (2) is perforated and subsequently the angled head milling cutter is moved back in the direction of the crankcase longitudinal axis (K) and removed from the crankcase (3) by moving the angled head milling cutter in the direction of the cylinder longitudinal axis (Z). Internal stresses in the crankcase are avoided by the production according to the invention of the ventilation bore, as a result of which the strength of the crankcase is advantageously increased. | ||||||
| 139 | PROCÈDE ET MACHINE OUTIL POUR L'AJUSTAGE DU CONTOUR D'UN PIED D'AUBE DE TURBINE | EP11773103.4 | 2011-09-15 | EP2616214A1 | 2013-07-24 | DUPOUY, Olivier; DEFROCOURT, Christian; MARQUOIN, Thomas; PAUL, Pascal |
| The present invention relates to a method for adjusting a predetermined contour of a turbine blade root (4) comprising a main salient edge defined by a determined interior angle. According to the invention, the following successive steps are performed: A/ the main edge of the contour is chamfered in order to obtain two auxiliary salient edges the associated interior angles of which are respectively greater than the interior angle of the main edge; and B/ the auxiliary edges obtained are blunted in order to fine-tune the contour of the blade root (4). | ||||||
| 140 | Verfahren und Vorrichtung zur Fertigbearbeitung von Werkstücken | EP12184802.2 | 2012-09-18 | EP2570229A3 | 2013-03-27 | Dr. Schreiber, Leo; Weber, Matthias |
Zur Verkürzung der Prozesskette beim materialabnehmenden Bearbeiten, insbesondere einer Kurbelwelle (1), nach der Grobbearbeitung und insbesondere nach dem Härten, wird erfindungsgemäß vor allem die Kombination aus Umfangsdrehfräsen als erstem Schritt und nachfolgendem Trockenschleifen als zweitem Schritt vorgeschlagen.
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