EP0258240B1 - Sicherheitsfechtklinge - Google Patents
Sicherheitsfechtklinge Download PDFInfo
- Publication number
- EP0258240B1 EP0258240B1 EP86902847A EP86902847A EP0258240B1 EP 0258240 B1 EP0258240 B1 EP 0258240B1 EP 86902847 A EP86902847 A EP 86902847A EP 86902847 A EP86902847 A EP 86902847A EP 0258240 B1 EP0258240 B1 EP 0258240B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- blade
- longitudinal
- rupture
- section
- region
- 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.)
- Expired
Links
- 239000011888 foil Substances 0.000 claims abstract description 14
- 229910052751 metal Inorganic materials 0.000 claims abstract description 8
- 239000002184 metal Substances 0.000 claims abstract description 8
- 239000004020 conductor Substances 0.000 claims description 12
- 239000000463 material Substances 0.000 claims description 7
- 208000029152 Small face Diseases 0.000 claims description 3
- 239000012634 fragment Substances 0.000 claims description 3
- 229910000831 Steel Inorganic materials 0.000 description 5
- 239000010959 steel Substances 0.000 description 5
- 239000000956 alloy Substances 0.000 description 3
- 229910045601 alloy Inorganic materials 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41B—WEAPONS FOR PROJECTING MISSILES WITHOUT USE OF EXPLOSIVE OR COMBUSTIBLE PROPELLANT CHARGE; WEAPONS NOT OTHERWISE PROVIDED FOR
- F41B13/00—Thrusting-weapons; Cutting-weapons carried as side-arms
- F41B13/02—Sabres; Cutlasses; Swords; Epees
Definitions
- fencing blades that is, foils, swords and sabers, are made of treated steel, alloyed or not.
- the object of the present invention is to remedy this drawback by providing a safety blade indicating the moment from which the blade risks breaking and must be discarded.
- the blade according to the invention comprises, at least over part of its length and from its free end, a longitudinal zone, of reduced cross section, of concentration of stresses urging the blade and suitable, when the fatigue of the material constituting the blade risks causing its transverse sectioning, to yield longitudinally by dividing the blade into two longitudinal fragments indicating this state of fatigue of the metal.
- the metal constituting the blade reaches a state of fatigue capable of causing the transverse rupture of the latter, the stresses urging it in a fight cause the rupture of the stress concentration zone, at least over part of the length of the blade.
- the longitudinal slit thus formed modifies the physical characteristics of the blade and provides, on impact, a different sound.
- the longitudinal rupture zone is constituted by an axial core which, delimited by two deep longitudinal grooves opening out from the small faces of the blade, and giving it a “H” section, has a thickness ranging from increasing, in proportion to the increase in section of the blade, from the end of the latter to the end of this rupture zone.
- the blade is lighter and all the stresses affecting it on the surface, during a fight, are distributed over the core and over the length thereof.
- the longitudinal breaking zone is formed in the rib of the back, between the outer face of this rib and the bottom of a longitudinal groove opening into the concavity of the “V” section, and has an increasing thickness, in proportion to the increase in section of the blade, from the end of the latter to the end of this rupture zone.
- FIG. 1 to 6 denotes a foil blade whose tip is extended by a threaded end 3 and whose heel is extended by a threaded rod 4 for attachment to a handle.
- this blade has a generally rectangular cross section.
- this blade has two deep longitudinal grooves 6 emerging from its small faces and giving it a cross section in "H", that is to say formed by two wings 2a connected by a core 2b. More precisely, the two parallel bottoms 6a of the grooves 6 delimit between them, in the rupture zone 7, a stress concentration zone corresponding to the core 2b of the “H” section. Each of the bottoms 6a is connected to the corresponding lateral faces 6b by rounded fillets 8. As illustrated by FIGS.
- the grooves have a depth p1-p2 which increases, substantially proportional to the increase in the dimensions T1-D1, T2-D2 of the cross section of the blade, so that the core 2b have, in zone 7, a thickness e1-e2 also increasing in proportion to the increase in section to offer constant resistance over this length.
- the grooves have a constant depth p, and give the core 2b a thickness E which goes up to the heel.
- These grooves thus define a longitudinal area 7 which, by concentrating stresses, not only precludes the transverse rupture dan- g ereuse of the blade, but this turns out in the longitudinal direction and informs the user of the need to discard his blade.
- the grooves 6 are provided with sloping side faces 6b converging inwardly and giving them, in cross section, the shape of a trapezoid whose smallest base constitutes the opening 6c emerging from the blade.
- the opening 6c has a height h which is less than the diameter of the envelope 11a of the conductor 11 intended to be disposed in the groove 6 for transmitting the keys with the opponent's plastron in a fight with the electric foil.
- the positioning of the conductor in the corresponding groove 6 is carried out by exerting a pressure on the conductor, in the direction of the bottom of the groove, so that its envelope 11 a is deformed elastically during its passage through the opening 6c.
- the natural elasticity of the envelope 11 a restores the latter to its original dimension.
- the casing 11a cooperates with the sloping faces 6b of the groove and ensures that the conductor is held in this groove without the need for glue.
- the conductor 11 is perfectly held in the groove and cannot come out of it, even when the blade is subjected to significant bending. During these flexions, the conductor and its envelope can slide inside the groove 6 without this disturbing its retention in this groove, or the very function of the conductor.
- the sword shown in Figures 7 to 13 and generally designated by 10, has, in known manner, a cross section in "V" delimiting an outer rib 12 going from the tip 13 to the heel 14.
- the tip 13 is provided with a threaded end piece 15, while the heel 14 is extended by a threaded rod 16.
- this sword also comprises, over a part of its length and for example over half of its length, as represented by the distance "I starting from the end of the sword, a longitudinal zone 17 of concentration of stresses and longitudinal failure.
- This zone is formed in the rib of the back, between the outer face 12 constituting this rib and the bottom 18a of a groove 18 opening into the concavity of the “V” cross section of the sword.
- the depth p1 -p2 of the groove 18 increases, as shown in FIGS. 12 and 13, from the tip 13 of the blade and in proportion to the variation of the dimensions T1 and D1 of the cross section of this blade.
- the longitudinal rupture zone 17 has a thickness e1 -e2 which increases from the tip of the blade to the end of the longitudinal zone 7.
- the groove 18 has a decreasing depth until its bottom 18a touches the bottom 20 of the concavity of the profile of the blade, as shown in FIG. 10.
- the area of this outcrop is located at a distance L from the end of the blade, of value greater than the distance I.
- the thickness of the longitudinal break zone 17 of the sword can also be controlled by machining the face 12 with or without groove 18.
- the thickness e1-e2 of the stress concentration zone 7 of the foil 2 is less than the thickness z of each of the wings 1 Oa-2a which it connects, so as to constitute a zone of rupture.
- the groove 6-18 making it possible to control the geometrical characteristics of the zone of concentration of stresses, can be carried out in all the materials constituting the blades. However, its realization is simpler, less expensive and faster in blades made of alloy with structural hardening temporarily put in softened position, that is to say when the material is in a state of high plasticity and low hardness, after completion of the grooves 6 and of the other machining operations, the blade is hardened by temperature rise.
- the core of the foil 2 is crossed, in its part corresponding to the longitudinal rupture zone 7, by slots.
- These circular lights, as shown at 21 in Figure 14, or oblong, as shown at 22 in Figure 15, are distributed in a step, regular or not. They delimit bridges of material respectively 23-24 which increase the concentration of the stresses and constitute witnesses of rupture.
- the oblong slots 22, inclined between 30 and 60 ° relative to the longitudinal axis of the foil, are separated by a small step so that the anterior end of each lumen is in front or at least at the posterior end of the perforation which precedes it. They can also, in an embodiment not shown, be staggered on either side of the longitudinal axis of the blade while being parallel to this axis.
- each light is less than 1 mm and of the order of a few tenths of a millimeter.
- perforations 21 or 22 can also be made in the longitudinal breaking zone 17 of the sword, with or without the groove 18.
- the longitudinal rupture zone extended over half the length of the blade, but it is obvious that this dimension is given only by way of example and that it may as well be between one third and two thirds of the length, or even more, depending on the characteristics of the material constituting the blade, material which may be steel, or a forged alloy, but also a composite material.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Control Devices (AREA)
- Fuses (AREA)
- Control And Other Processes For Unpacking Of Materials (AREA)
- Knives (AREA)
- Endoscopes (AREA)
- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
- Dental Tools And Instruments Or Auxiliary Dental Instruments (AREA)
- Emergency Lowering Means (AREA)
- Food-Manufacturing Devices (AREA)
Claims (11)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT86902847T ATE45031T1 (de) | 1985-05-10 | 1986-05-07 | Sicherheitsfechtklinge. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8507459 | 1985-05-10 | ||
FR8507459A FR2581744B1 (fr) | 1985-05-10 | 1985-05-10 | Lame d'escrime de securite |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0258240A1 EP0258240A1 (de) | 1988-03-09 |
EP0258240B1 true EP0258240B1 (de) | 1989-07-26 |
Family
ID=9319354
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP86902847A Expired EP0258240B1 (de) | 1985-05-10 | 1986-05-07 | Sicherheitsfechtklinge |
Country Status (8)
Country | Link |
---|---|
US (1) | US4817942A (de) |
EP (1) | EP0258240B1 (de) |
AT (1) | ATE45031T1 (de) |
DE (1) | DE3664682D1 (de) |
FR (1) | FR2581744B1 (de) |
HU (1) | HUT46142A (de) |
SU (1) | SU1600617A3 (de) |
WO (1) | WO1986006824A1 (de) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2614409B1 (fr) * | 1987-04-23 | 1989-07-21 | Begon Jean | Lame d'epee |
GB2264065B (en) * | 1992-02-13 | 1995-04-26 | Leon Paul Equip Co Ltd | Fencing blade |
DE4303871A1 (de) * | 1992-02-13 | 1993-08-19 | Leon Paul Equipment Co Ltd | |
US6099608A (en) | 1998-07-30 | 2000-08-08 | 3M Innovative Properties Company | Rotating filtration cartridge and blower for HVAC applications |
US6521011B1 (en) | 1999-07-15 | 2003-02-18 | 3M Innovative Properties Company | Self-supporting pleated filter and method of making same |
US6437372B1 (en) | 2000-01-07 | 2002-08-20 | Agere Systems Guardian Corp. | Diffusion barrier spikes for III-V structures |
US6348086B1 (en) * | 2000-02-16 | 2002-02-19 | 3M Innovative Properties Company | Combination blower wheel and filter cartridge system for HVAC applications |
US6497619B2 (en) * | 2000-06-01 | 2002-12-24 | David D. Dowdy | Scoring apparatus for simulated combat |
US6565484B1 (en) | 2002-01-23 | 2003-05-20 | William C. Adams | Fencing sword |
RU2006124262A (ru) * | 2003-12-09 | 2008-01-20 | Адриан Блэр ГАРДИНЕР (NZ) | Игра |
US7228633B2 (en) * | 2004-03-01 | 2007-06-12 | Ryan Peter M | Saber |
US20050204714A1 (en) * | 2004-03-22 | 2005-09-22 | 3M Innovative Properties Company | Self-supporting pleated filter and method of making same |
US7156891B2 (en) * | 2004-09-10 | 2007-01-02 | Filtration Group Incorporated | Forced air system air filter |
US20180094899A1 (en) * | 2016-10-05 | 2018-04-05 | Ronald J. Thornton | Fencing Sport Safety Blade |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DD34206A (de) * | ||||
FR393476A (fr) * | 1908-08-19 | 1908-12-23 | Gilbert Bougnol | Genre d'épée-fleuret incassable |
FR439666A (fr) * | 1912-02-02 | 1912-06-20 | Gilbert Bougnol | Perfectionnements apportés à la construction des armes d'escrime, épées, fleurets et sabres |
US2338007A (en) * | 1940-04-27 | 1943-12-28 | James E Krilow | Cake and fruit knife |
FR1363602A (fr) * | 1963-07-05 | 1964-06-12 | Lame de fleuret | |
GB1473751A (en) * | 1976-01-30 | 1977-05-18 | Equipment P Co Ltd | Blades for fencing swords |
DE3239051C2 (de) * | 1982-10-22 | 1986-08-07 | Uhlmann Sportgeräte GmbH & Co KG, 7958 Laupheim | Fechtklinge |
-
1985
- 1985-05-10 FR FR8507459A patent/FR2581744B1/fr not_active Expired
-
1986
- 1986-05-07 HU HU863113A patent/HUT46142A/hu unknown
- 1986-05-07 EP EP86902847A patent/EP0258240B1/de not_active Expired
- 1986-05-07 US US07/010,978 patent/US4817942A/en not_active Expired - Fee Related
- 1986-05-07 AT AT86902847T patent/ATE45031T1/de not_active IP Right Cessation
- 1986-05-07 DE DE8686902847T patent/DE3664682D1/de not_active Expired
- 1986-05-07 WO PCT/FR1986/000160 patent/WO1986006824A1/fr active IP Right Grant
-
1987
- 1987-11-09 SU SU874203742A patent/SU1600617A3/ru active
Also Published As
Publication number | Publication date |
---|---|
FR2581744A1 (fr) | 1986-11-14 |
SU1600617A3 (ru) | 1990-10-15 |
EP0258240A1 (de) | 1988-03-09 |
ATE45031T1 (de) | 1989-08-15 |
HUT46142A (en) | 1988-09-28 |
DE3664682D1 (en) | 1989-08-31 |
US4817942A (en) | 1989-04-04 |
FR2581744B1 (fr) | 1987-07-24 |
WO1986006824A1 (fr) | 1986-11-20 |
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