US20030006583A1 - Gliding edge profile - Google Patents
Gliding edge profile Download PDFInfo
- Publication number
- US20030006583A1 US20030006583A1 US10/147,428 US14742802A US2003006583A1 US 20030006583 A1 US20030006583 A1 US 20030006583A1 US 14742802 A US14742802 A US 14742802A US 2003006583 A1 US2003006583 A1 US 2003006583A1
- Authority
- US
- United States
- Prior art keywords
- gliding
- edge profile
- gliding edge
- component parts
- profile
- 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.)
- Abandoned
Links
- 238000003466 welding Methods 0.000 claims abstract description 30
- 239000000463 material Substances 0.000 claims abstract description 12
- 238000010894 electron beam technology Methods 0.000 claims abstract description 3
- 238000004873 anchoring Methods 0.000 claims description 27
- 239000011651 chromium Substances 0.000 claims description 20
- 229910052750 molybdenum Inorganic materials 0.000 claims description 20
- 229910052804 chromium Inorganic materials 0.000 claims description 19
- 229910052799 carbon Inorganic materials 0.000 claims description 17
- 229910052721 tungsten Inorganic materials 0.000 claims description 16
- 229910001220 stainless steel Inorganic materials 0.000 claims description 15
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 14
- 239000011733 molybdenum Substances 0.000 claims description 14
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 13
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 13
- 239000010937 tungsten Substances 0.000 claims description 13
- 229910052720 vanadium Inorganic materials 0.000 claims description 13
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 11
- 229910052710 silicon Inorganic materials 0.000 claims description 10
- 239000010703 silicon Substances 0.000 claims description 10
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims description 10
- 238000000034 method Methods 0.000 claims description 9
- 239000011572 manganese Substances 0.000 claims description 8
- 230000008569 process Effects 0.000 claims description 8
- 229910052748 manganese Inorganic materials 0.000 claims description 7
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 6
- 229910000831 Steel Inorganic materials 0.000 claims description 6
- 239000010959 steel Substances 0.000 claims description 6
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 4
- 229910052742 iron Inorganic materials 0.000 claims description 3
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 claims description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims 4
- 230000003245 working effect Effects 0.000 claims 1
- 238000005452 bending Methods 0.000 description 5
- 238000010438 heat treatment Methods 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 5
- 238000010791 quenching Methods 0.000 description 4
- 238000005260 corrosion Methods 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 3
- 230000000171 quenching effect Effects 0.000 description 3
- 238000005496 tempering Methods 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 229910000734 martensite Inorganic materials 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000010962 carbon steel Substances 0.000 description 1
- 150000001805 chlorine compounds Chemical class 0.000 description 1
- 238000010622 cold drawing Methods 0.000 description 1
- 238000005097 cold rolling Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000011065 in-situ storage Methods 0.000 description 1
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002823 nitrates Chemical class 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Images
Classifications
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63C—SKATES; SKIS; ROLLER SKATES; DESIGN OR LAYOUT OF COURTS, RINKS OR THE LIKE
- A63C5/00—Skis or snowboards
- A63C5/04—Structure of the surface thereof
- A63C5/048—Structure of the surface thereof of the edges
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/22—Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/24—Ferrous alloys, e.g. steel alloys containing chromium with vanadium
Definitions
- the present invention relates to a gliding edge profile for winter sports equipment, such as, for example, skis, snowboards and sledges.
- Profiles of this type are normally made of steel and exhibit a generally L-shaped cross section with a relatively greater leg and a relatively smaller leg.
- the leg of greater cross section has the gliding edge and terminates flush with the bottom of a ski, whereas the leg with smaller cross section provides an anchor of the gliding profile between the runner base and a runner base underlayer. Accordingly, the anchoring leg and the gliding edge leg are exposed to different stress conditions.
- the gliding edge leg is subjected to particular stress that requires a high degree of wear resistance, hardness and surface quality. Another important factor to consider here is maintenance-free construction because the service life decreases when the edges are sharpened as is typically done to remove rust or to re-establish good guide properties.
- the gliding edge leg Despite a high wear resistance, it should be possible to easily grind the gliding edge leg to a level of the runner base surface to realize a completely flat running surface.
- the other leg of the edge profile, serving as anchoring profile, is subjected to much less stress because it is disposed inside the ski and therefore does neither come into contact with the atmosphere nor with snow or ice or with dispersed grit and partially snow-free ground.
- chromium steels are especially useful as material for gliding edges. Although chromium steels show high corrosion resistance and wear resistance as well as high hardness, their relatively low ductility is disadvantageous. In order to permit production of gliding edge profiles through rolling or drawing, quenchable and temperable steels are typically used which receive their wear resistance and hardness through a final heat treatment.
- German Patent Document DE 40 00 744 describes a process for the heat treatment of gliding edge legs in situ, whereby the zone about the gliding edge is heated locally by means of a laser beam to a hardness temperature and is subsequently immediately locally quenched to transform into a martensite structure.
- This process requires a complex apparatus and still cannot ensure reproducible properties of the gliding edge.
- particular measures are necessary, in addition to local quenching, to carry off heat which is generated during welding.
- This process is capable to produce a gliding edge with high hardness and wear resistance in the area of the actual gliding edge as well as comparably high toughness, especially of the anchoring profile. Still, as a consequence of the required cooling action during the heat treatment, inner tension is encountered in the edge-near region to lead to a so-called sickle distortion, i.e., a highly disadvantageous flexure of the gliding edge profile.
- German Patent Document DE 42 18 099 A1 limits the hardness gradient across the cross section and length of the gliding edge profile to less than 2 HRC.
- the process described therein employs thus a two-step heat treatment which involves a quenching and tempering of the entire gliding edge profile to provide a martensitic structure, and a subsequent partial pearlitization at a temperature as constant as possible across the length of the profile. Any sickle distortion remaining after the partial pearlitization is eliminated through a subsequent deformation by bending with constant degree of bending stretching over the length of the profile. This process is extremely complicated and still is unable to provide the gliding edge profile with the necessary corrosion resistance to eliminate the need for frequent re-grinding and sharpening.
- German Patent Document DE 198 08 276 which describes the use of a gliding edge material of chromium steel alloy.
- the hardness and wear resistance as well as vibration behavior and corrosion resistance depends in the quenched and tempered state, in particular toward chlorides and nitrates, on the presence of carbon, nitrogen, molybdenum and chromium.
- a gliding edge profile for winter sports equipment includes two component parts connected at an angle to one another along their longitudinal edges.
- the present invention resolves prior art problems by providing two component parts which can be made of different materials and are interconnected to form, for example, a L-shaped configuration, whereby one component part is the gliding edge leg and the other component part represents the anchoring leg.
- the gliding edge leg of rust-free material and wear-resistant material, preferably chromium steel
- the anchoring leg may be made of a simple carbon steel.
- the gliding edge leg may be a chromium steel with
- the balance being iron.
- chromium steel which contains at least 0.1% of tungsten, 0.4% of manganese and 0.4% of silicon.
- a currently particularly suitable chromium steel includes 0.3 to 1.0% or also at most 0.8% carbon, 5.0 to 16.5% or also 13.0% chromium, 1.0 to 2.0% molybdenum, 0.4 to 2.0% vanadium, 0.6 to 1.1% % silicon, as well as, optionally, 1.2 to 2.5% tungsten.
- a particular high wear resistance is achieved when the content of carbon, chromium and molybdenum, and, optionally, also the content of molybdenum, vanadium and tungsten, satisfies the following condition:
- Joining of the component parts or profile legs can be realized through laser beam welding, electron-beam welding or plasma jet welding. In this way, heat is introduced in a narrow locally restricted area so that the heat impact zone is small. Tempering may follow the welding process to eliminate structural changes and also welding tension accompanying the welding operation in the heat impact zone.
- the component parts may be properly guided by a profile guide for correct positioning during welding operation.
- the component parts are welded together by a welding seam at a maximum width of 0.5 mm.
- welding heat is small enough to realize a rapid cooling already in the area of the profile guide so that a distortion of the finished glide edge profile as a result of heat and undesired structural changes in the area of the gliding edge are prevented.
- a gliding edge profile may finally be subjected also to a common quenching and tempering treatment.
- Another option involves the production of the gliding edge leg from an already hardened component part, for example, a square wire so that there is only a need to quench and temper the complete gliding edge profile after the welding operation.
- the welding seam may have gaps to improve the bending capability of the gliding edge profile. Such gaps or breaches can be realized by simply cutting the welding current. The bending capability can be further enhanced, when forming the anchoring leg with openings which may or may not be open toward the welding edge or welding seam.
- FIG. 1 is a cross section of a first embodiment of a gliding edge profile according to the present invention
- FIG. 2 is a cross section of a second embodiment of a gliding edge profile according to the present invention.
- FIG. 3 is a cross section of a third embodiment of a gliding edge profile according to the present invention.
- FIG. 4 is a fragmentary perspective illustration of a fourth embodiment of a gliding edge profile according to the present invention.
- FIG. 5 is a fragmentary perspective illustration of a fifth embodiment of a gliding edge profile according to the present invention.
- FIG. 1 shows a cross section of a first embodiment of a gliding edge profile according to the present invention, including an anchoring leg 1 for attachment of the gliding edge profile in the body of a ski (not shown), and a gliding edge leg 2 of rectangular cross section and forming a gliding edge 3 for the ski.
- the anchoring leg 1 and the gliding edge leg 2 are connected together by a welding seam 4 .
- FIG. 2 shows a gliding edge profile in which the gliding edge leg 2 has an inner flank 5 which is inclined inwardly toward the anchoring leg 1
- FIG. 3 shows a gliding edge profile in which the gliding edge leg 2 has an outer flank 6 which is inclined outwardly away from the anchoring leg 1 and forms with the gliding edge 3 a slight angle.
- FIG. 4 shows another embodiment of a gliding edge profile in which the anchoring leg 1 is formed with openings 8 (only one opening 8 is shown here by way of example) and openings 11 (only one opening 11 is shown here by way of example) to improve attachment of the edge profile to the body of the ski.
- the openings 8 have a closed border 9 whereas the openings 11 are open toward the free leg edge 10 of the anchoring leg 1 .
- FIG. 5 shows an embodiment of a gliding edge profile in which the anchoring leg 1 is formed in addition to the openings 8 with openings 12 which are open toward the welding seam 4 and the gliding edge leg 2 , as indicated by reference numeral 15 .
- the anchoring leg 1 is formed with any combination of the openings 8 , 11 , 12 .
- the welding seam 5 is breached in addition to gap 15 by gaps 14 which divide the welding seam 5 into several weld sections 13 and are aligned with the gap 15 of opening 12 of the anchoring leg 1 .
- the openings 8 , 11 , 12 in the anchoring leg 1 and the gaps 14 in the welding seam 4 provide the gliding edge profile with a high bending capability so that the ski exhibits a high elasticity.
- the gliding edge leg 2 may be a chromium steel of a following composition, by weight percent: 0.1 to 1.1% of carbon, 4.0 to 18% of chromium, 0.1 to 4.0% of molybdenum and/or 0.1 to 2.4% of vanadium and/or up to 3.0% of tungsten, up to 2.0% of manganese, up to 2.0% of silicon, the balance being iron.
- a chromium steel which contains at least 0.1% of tungsten, 0.4% of manganese and 0.4% of silicon.
- a currently particularly suitable chromium steel includes 0.3 to 1.0% or also at most 0.8% carbon, 5.0 to 16.5% or also 13.0% chromium, 1.0 to 2.0% molybdenum, 0.4 to 2.0% vanadium, 0.6 to 1.1% % silicon, as well as, optionally, 1.2 to 2.5% tungsten.
- a particular high wear resistance is achieved when the content of carbon, chromium and molybdenum, and, optionally, also the content of molybdenum, vanadium and tungsten satisfies the following condition:
- chromium steel alloys K1 to K6 which, apart from the chromium steel allow disclosed in German Pat. Document DE 198 08 276 A1, are suitable as material for the gliding edge leg, wherein designations F 1 to F 5 indicate materials for the anchoring leg: Chemical Composition [weight %] Al- C Si Mn Cr Mo Ni V W loy (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%) (%)
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Heat Treatment Of Articles (AREA)
- Laser Beam Processing (AREA)
- Steam Or Hot-Water Central Heating Systems (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE10123674A DE10123674B4 (de) | 2001-05-16 | 2001-05-16 | Gleitkantenprofil |
| DE10123674.3 | 2001-05-16 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20030006583A1 true US20030006583A1 (en) | 2003-01-09 |
Family
ID=7684904
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US10/147,428 Abandoned US20030006583A1 (en) | 2001-05-16 | 2002-05-16 | Gliding edge profile |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US20030006583A1 (de) |
| AT (1) | AT501171B1 (de) |
| DE (2) | DE10123674B4 (de) |
| FR (1) | FR2824745B1 (de) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7004493B2 (en) * | 2001-07-06 | 2006-02-28 | C.D. Walzholz-Brockhaus Gmbh | Ski edge profile |
| WO2022109658A1 (en) * | 2020-11-27 | 2022-06-02 | Tang, Yuankui | A new wear resistant steel with high hardness and good toughness which keeps hardened after hard facing and tungsten carbide tile brazing |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102004020293B4 (de) * | 2004-04-26 | 2006-02-09 | Danfoss A/S | Wärmetauscher |
| EP2413047B2 (de) † | 2010-07-30 | 2021-11-17 | Grundfos Management A/S | Brauchwassererwärmungseinheit |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2126152A (en) * | 1935-06-26 | 1938-08-09 | Chauncey G Suits | Ski |
| US2743113A (en) * | 1952-07-11 | 1956-04-24 | Nelson S Griggs | Flexible running edge for ski |
| US3095207A (en) * | 1956-09-21 | 1963-06-25 | Head Howard | Ski |
| US3297332A (en) * | 1964-01-15 | 1967-01-10 | Jet Stream Ind | Skis |
| US4191599A (en) * | 1978-09-13 | 1980-03-04 | Ford Motor Company | Method of heat treating high carbon alloy steel parts to develop surface compressive residual stresses |
| US5301965A (en) * | 1985-01-07 | 1994-04-12 | Richard Floreani | Snow ski |
| US6062585A (en) * | 1993-04-27 | 2000-05-16 | Hess; Eugen | Ski construction |
Family Cites Families (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH218662A (de) * | 1941-04-22 | 1941-12-31 | Inglin & Knuesel | Ski mit Schutzkanten. |
| CH369481A (de) * | 1956-01-11 | 1963-05-31 | Birmingham Small Arms Co Ltd | Verfahren zur Erhöhung der Kriechfestigkeit von Chromstahl |
| DE1238676B (de) * | 1962-05-31 | 1967-04-13 | Gen Electric | Verwendung einer Chromstahllegierung fuer Schmiedestuecke |
| DE1578902A1 (de) * | 1966-05-26 | 1970-10-15 | Simon Fa Karl | Seitenschiene fuer Skier |
| AT307951B (de) * | 1971-02-18 | 1973-06-12 | Deutsch Friedrich | Verfahren zur Herstellung eines Stahlbeschlagteiles für Schier, insbesondere einer Stahlkante und nach diesem Verfahren hergestellter Stahlbeschlagteil |
| CH569493A5 (de) * | 1972-06-08 | 1975-11-28 | Bildner Heinz | |
| JPS5243414B2 (de) * | 1973-02-20 | 1977-10-31 | ||
| DE2427195A1 (de) * | 1974-06-05 | 1976-01-02 | Fritzmeier Kg Georg | Stahlkante fuer ski |
| FR2342459A1 (fr) * | 1976-02-27 | 1977-09-23 | Sofeas | Procede de protection, par profile metallique, des bords et aretes d'objets sensibles aux chocs et a l'usure |
| US4294613A (en) * | 1979-07-03 | 1981-10-13 | Henrik Giflo | Acid resistant, high-strength steel suitable for polishing |
| US4987282A (en) * | 1985-06-12 | 1991-01-22 | K-2 Corporation | Snow ski with treated metal edge |
| DE3620091A1 (de) * | 1986-06-14 | 1987-12-23 | Feldmuehle Ag | Ski |
| FR2627996B1 (fr) * | 1988-03-02 | 1990-12-21 | Seb Sa | Ski a carres ameliorees |
| DE4000744C2 (de) * | 1990-01-12 | 1996-07-11 | Trumpf Gmbh & Co | Verfahren für Stahlkanten von Wintersportgeräten |
| DE4011384A1 (de) * | 1990-04-07 | 1991-10-10 | Karl Schimanek | Ski mit zusaetzlichem seitenkantenprofil |
| DD298827A5 (de) * | 1990-04-25 | 1992-03-12 | Zi Fuer Festkoerperphysik Und Werkstofforschung,De | Werkstoff fuer gleitelemente von wintersportgeraeten |
| DE4218099A1 (de) * | 1991-08-28 | 1993-03-04 | Waelzholz C D Prod Gmbh | Verfahren fuer die herstellung einer skikante |
| EP0530395A1 (de) * | 1991-09-04 | 1993-03-10 | Karl Schimanek | Ski mit zusätzlichem Seitenkantenprofil |
| DE4240380A1 (de) * | 1992-12-01 | 1994-06-09 | Wirnsberger Peter | Ski mit Doppelkante |
| US5580078A (en) * | 1993-11-12 | 1996-12-03 | Vance; Mark D. | Double-edged snowboard |
| FR2729866B1 (fr) * | 1995-01-30 | 1997-04-11 | Rossignol Sa | Perfectionnement aux skis a coque pourvus de chants de support de la coque |
| JPH1157108A (ja) * | 1997-08-27 | 1999-03-02 | Kaname Fukao | スキー用エッジ |
| DE19808276C2 (de) * | 1998-02-27 | 2003-12-24 | Stahlwerk Ergste Westig Gmbh | Stahllegierung für Gleitelemente |
-
2001
- 2001-05-16 DE DE10123674A patent/DE10123674B4/de not_active Expired - Fee Related
-
2002
- 2002-04-03 DE DE10214735A patent/DE10214735A1/de not_active Withdrawn
- 2002-05-15 FR FR0205989A patent/FR2824745B1/fr not_active Expired - Fee Related
- 2002-05-15 AT AT0074302A patent/AT501171B1/de not_active IP Right Cessation
- 2002-05-16 US US10/147,428 patent/US20030006583A1/en not_active Abandoned
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2126152A (en) * | 1935-06-26 | 1938-08-09 | Chauncey G Suits | Ski |
| US2743113A (en) * | 1952-07-11 | 1956-04-24 | Nelson S Griggs | Flexible running edge for ski |
| US3095207A (en) * | 1956-09-21 | 1963-06-25 | Head Howard | Ski |
| US3297332A (en) * | 1964-01-15 | 1967-01-10 | Jet Stream Ind | Skis |
| US4191599A (en) * | 1978-09-13 | 1980-03-04 | Ford Motor Company | Method of heat treating high carbon alloy steel parts to develop surface compressive residual stresses |
| US5301965A (en) * | 1985-01-07 | 1994-04-12 | Richard Floreani | Snow ski |
| US6062585A (en) * | 1993-04-27 | 2000-05-16 | Hess; Eugen | Ski construction |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7004493B2 (en) * | 2001-07-06 | 2006-02-28 | C.D. Walzholz-Brockhaus Gmbh | Ski edge profile |
| WO2022109658A1 (en) * | 2020-11-27 | 2022-06-02 | Tang, Yuankui | A new wear resistant steel with high hardness and good toughness which keeps hardened after hard facing and tungsten carbide tile brazing |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2824745B1 (fr) | 2004-12-17 |
| DE10123674A1 (de) | 2002-12-05 |
| AT501171A1 (de) | 2006-07-15 |
| AT501171B1 (de) | 2007-01-15 |
| DE10123674B4 (de) | 2005-11-10 |
| DE10214735A1 (de) | 2003-12-18 |
| FR2824745A1 (fr) | 2002-11-22 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US5417777A (en) | Alloy for backing steel of a bimetallic band saw blade | |
| EP3653736B1 (de) | Warmgewalztes stahlband und herstellungsverfahren | |
| EP2397571A1 (de) | Stahl für einen sehr starken fahrzeugstabilisator mit ausgezeichneter korrosionsbeständigkeit und niedertremperatur-zähigkeit und verfahren zur herstellung davon, sowie stabilisator | |
| US20200332402A1 (en) | Weldable component of structural steel and method of manufacture | |
| US4058650A (en) | Back material of metal band saw high in fatigue strength | |
| JP3864536B2 (ja) | 耐遅れ破壊特性に優れる高強度鋼およびその製造方法 | |
| US6235237B1 (en) | Steel alloy for gliding elements | |
| JPH09263876A (ja) | 遅れ破壊特性の優れた高強度機械構造用鋼およびその製造方法 | |
| CA2165775A1 (en) | Rails with a low carbon martensite head | |
| US20030006583A1 (en) | Gliding edge profile | |
| EP3821040B1 (de) | Gleisteil aus hypereutektoidem stahl | |
| JPS6048582B2 (ja) | 熱処理硬さの高いステンレス剃刃用鋼 | |
| JP3454869B2 (ja) | 高炭素鋼板の連続焼鈍による球状化焼鈍方法 | |
| JP2926195B2 (ja) | 伸線加工性に優れた高炭素鋼線の製造方法 | |
| JP3117916B2 (ja) | 耐摩耗性に優れたパーライト系レールの製造法 | |
| JPS637351A (ja) | メタルバンドソ−の胴材 | |
| AU2008307112A1 (en) | Intermediate piece for connecting manganese steel molded bodies with carbon steel and method for connecting manganese high-carbon steel cast parts to control rails | |
| JPH10168518A (ja) | 板厚テーパ高張力鋼板の製造方法 | |
| EP0957182A2 (de) | Martensitischer, hitzebeständiger Stahl | |
| JPH08260093A (ja) | 溶接部の疲労強度に優れたメタルバンドソー胴材およびメタルバンドソー | |
| JPH04354852A (ja) | 高速度鋼工具用高硬度シャンク材または胴材 | |
| JP2548067B2 (ja) | 高靭性低合金鋼 | |
| JPS61117252A (ja) | 刃物用ステンレス鋼 | |
| EP0733128B1 (de) | Stahllegierung, stahlband aus dieser legierung und verwendung des stahlbandes | |
| JPH0726150B2 (ja) | 溶接性・脆性破壊伝播停止特性の優れた調質高張力鋼板の製造方法 |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: STAHLWERK ERGSTE WESTIG GMBH, GERMANY Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:ROZSNOKI, LASZLO;REEL/FRAME:013135/0939 Effective date: 20020603 |
|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |
|
| AS | Assignment |
Owner name: HSBC UK BANK PLC, UNITED KINGDOM Free format text: SECURITY INTEREST;ASSIGNOR:VOXSMART LIMITED;REEL/FRAME:068886/0008 Effective date: 20241011 |