EP0182947B1 - Linear fiber armature for electromagnetic launchers - Google Patents
Linear fiber armature for electromagnetic launchers Download PDFInfo
- Publication number
- EP0182947B1 EP0182947B1 EP19840308277 EP84308277A EP0182947B1 EP 0182947 B1 EP0182947 B1 EP 0182947B1 EP 19840308277 EP19840308277 EP 19840308277 EP 84308277 A EP84308277 A EP 84308277A EP 0182947 B1 EP0182947 B1 EP 0182947B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- conductive fibers
- sleeve
- armature
- support structure
- axis
- 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
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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
- F41B6/00—Electromagnetic launchers ; Plasma-actuated launchers
- F41B6/006—Rail launchers
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R41/00—Non-rotary current collectors for maintaining contact between moving and stationary parts of an electric circuit
Definitions
- This invention relates to armatures for conducting very large currents between parallel rails of electromagnetic launchers and more particularly to such armatures employing multiple conducting fibers to conduct current between the launcher rails.
- sliding conductive armature serves to conduct current between the rails and is subjected to an electromagnetic force which propels the armature and an associated projectile toward the muzzle end of the rails. Because of the high currents involved in the electromagnetic propulsion of projectiles, sliding conductive armatures must be designed to minimize electrical contact resistance, to have sufficient contact force to maintain a low contact voltage drop in order to prevent rail damage caused by arcing, to have sufficient compliance to accommodate both its own wear and changes in the distance between the launcher rails, and to minimize damage resulting from resistive heating. Atypical armature may be seen in U.S.
- Patent 4,457,205 (preamble of claim 1) which includes two embodiments, one illustrating a bundle of conducting fibers held together by means of a retaining band and another embodiment which utilizes a stack of chevron-shaped plates having conductive fibers along the edges thereof for contacting the rails of a parallel rail electromagnetic launcher.
- an armature for conducting large D.C. currents, between a pair of electrically conductive rails, comprises in accordance with claim 1 an insulating support structure, a plurality of conductive fibers, a cylindrical sleeve having an opening in which said conductive fibers are positioned said conductive fibers being compacted to a maximum packing density to form a solid mass within said sleeve, and means for mounting said sleeve on said support structure, said conductive fibers being spirally disposed with respect to the axis of said sleeve.
- a plurality of cantilevered conductive fibers of this structure are angled and spiralled for low contact load.
- Maximum packing density of the fibers within the sleeve produces a uniform current distribution which eliminates excessive current density concentrations and prevents gross armature melting.
- a high current brush constructed in accordance with this invention comprises: a plurality of conductive fibers; a cylindrical sleeve having an opening through which said conductive fibers pass; and wherein said conductive fibers are compacted to a maximum density to form a solid mass within said sleeve.
- FIG. 1 shows a top view of an armature assembly.
- a brush assembly comprising a plurality of conductive fibers 10 pass through an opening in sleeve 12, is attached to an insulating support structure 14 by a brush holder mounting means 16.
- the insulating support structure 14 is sized to slide between a pair of parallel launching rails in an electromagnetic launcher and serves to position the brush assembly between the rails.
- an opening 18 is shown within insulating support structure 14 for receiving a projectile.
- the insulating support structure 14 may itself be the projectile, may lie adjacent to a projectile, or may be associated with a projectile in some other manner.
- the sleeve 12 of the brush assembly passes through an opening in mounting means 16 and is held in place by a set screw 20.
- FIG 2 is a side view of the armature assembly of Figure 1.
- This embodiment uses two fiber brush assemblies each of which contains ten bundles of 0.1524 mm copper fibers such as those used to form flexible commercial welding type cable. Each bundle contains 1,100 wire fibers. These bundles were inserted into openings of cylindrical annealed copper sleeves 12. The copper sleeves were then rotary swaged until conductive fibers 10 reached a maximum packing density within each sleeve and thereby formed a single solidified connection. The sleeves 12 were inserted into an aluminum mounting block 16 and secured by way of set screws 20. A bolt 22 serves as means for attaching mounting block 16 to insulating support structure 14.
- FIG 3 is a top view of the brush assembly of the armature assembly of Figure 1.
- Each end of sleeve 12 is beveled at an angle 24 of 10° to form a . narrow side 26 and a wide side 28.
- the narrow side 26 of sleeve 12 is mounted closest to the insulating support structure 14.
- Multiple conductive fibers 10 pass through an opening in sleeve 12 and are spiralled with respect to the axis of sleeve 12.
- the conductive fibers 10 have been bent as a whole to an angle 30 of 40° at the trailing edge and an angle 32 of 10° at the forward edge.
- the ends of conductive fibers 10 are cut along two planes which lie perpendicular to the axis of sleeve 12. To improve electrical contact between conductive fibers 10 and the projectile launching rails of the launcher, the ends of conductive fiber 10 are polished to a flat surface.
- Armature assemblies in accordance with this invention have been constructed and tested in an electromagnetic launcher.
- One of these armature assemblies having a brush assembly comprising 7,700 copper fibers, each having a diameter of 0.1524 mm, was used to accelerate a 317 gram projectile to a speed of 4.2 kilometers per second with a pulsed current of 2.1 million amperes.
- the projectile and armature assembly left the barrel intact and went through the center of a 6.35 mm thick steel witness plate before being destructively caught in a catch tank.
- Rail damage was minimal, with two smooth dime-shaped holes about 2 millimeters deep having been produced approximately 15 centimeters from the breech of the launcher. The remainder of the rails and insulation showed no damage although all interior surfaces were coated with a thin layer of soot.
- the spiralled fibers provide self support and limit deflection while in the presence of high electromagnetic fields. Spiralling allows compliance to variations along the contact rails as the armature travels to maintain good electrical contact, thereby reducing the destructive effects of arcing. Through the use of flexible conductive fibers, low contact forces are required to make good electrical contact, thereby resulting in low friction losses.
- the brush assembly of the armature assembly of this invention has been as an efficient linear sliding contact during a pulsed application, it can also be used as a continuous operating brush on a slip ring surface. Because the conductive fibers have been solidified within the sleeve of the brush assembly, soldering or joining heavy electrical conductors to the brush is possible and can readily be made when required.
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Plasma & Fusion (AREA)
- General Engineering & Computer Science (AREA)
- Elimination Of Static Electricity (AREA)
- Motor Or Generator Current Collectors (AREA)
- Linear Motors (AREA)
Description
- This invention relates to armatures for conducting very large currents between parallel rails of electromagnetic launchers and more particularly to such armatures employing multiple conducting fibers to conduct current between the launcher rails.
- In the electromagnetic propulsion of projectiles, a very large DC current is injected into the breach end of a pair of parallel conductive rails. A sliding conductive armature serves to conduct current between the rails and is subjected to an electromagnetic force which propels the armature and an associated projectile toward the muzzle end of the rails. Because of the high currents involved in the electromagnetic propulsion of projectiles, sliding conductive armatures must be designed to minimize electrical contact resistance, to have sufficient contact force to maintain a low contact voltage drop in order to prevent rail damage caused by arcing, to have sufficient compliance to accommodate both its own wear and changes in the distance between the launcher rails, and to minimize damage resulting from resistive heating. Atypical armature may be seen in U.S. Patent 4,457,205 (preamble of claim 1) which includes two embodiments, one illustrating a bundle of conducting fibers held together by means of a retaining band and another embodiment which utilizes a stack of chevron-shaped plates having conductive fibers along the edges thereof for contacting the rails of a parallel rail electromagnetic launcher.
- According to the present invention, an armature, for conducting large D.C. currents, between a pair of electrically conductive rails, comprises in accordance with claim 1 an insulating support structure, a plurality of conductive fibers, a cylindrical sleeve having an opening in which said conductive fibers are positioned said conductive fibers being compacted to a maximum packing density to form a solid mass within said sleeve, and means for mounting said sleeve on said support structure, said conductive fibers being spirally disposed with respect to the axis of said sleeve.
- Conveniently, a plurality of cantilevered conductive fibers of this structure are angled and spiralled for low contact load. Maximum packing density of the fibers within the sleeve produces a uniform current distribution which eliminates excessive current density concentrations and prevents gross armature melting.
- This invention also encompasses a fiber brush assembly which is suitable for making sliding contact with a slip ring conductor. A high current brush constructed in accordance with this invention comprises: a plurality of conductive fibers; a cylindrical sleeve having an opening through which said conductive fibers pass; and wherein said conductive fibers are compacted to a maximum density to form a solid mass within said sleeve.
- The invention will now be described, by way of example, with reference to the accompanying drawings in which:
- Figure 1 is a top view of an armature assembly in accordance with one embodiment of this invention;
- Figure 2 is a side view of the armature assembly of Figure 1; and
- Figure 3 is a top view of an armature brush assembly for use in the armature assembly of Figure 1.
- Figure 1 shows a top view of an armature assembly. A brush assembly comprising a plurality of
conductive fibers 10 pass through an opening insleeve 12, is attached to aninsulating support structure 14 by a brush holder mounting means 16. Theinsulating support structure 14 is sized to slide between a pair of parallel launching rails in an electromagnetic launcher and serves to position the brush assembly between the rails. In this embodiment, anopening 18 is shown withininsulating support structure 14 for receiving a projectile. However, theinsulating support structure 14 may itself be the projectile, may lie adjacent to a projectile, or may be associated with a projectile in some other manner. Thesleeve 12 of the brush assembly passes through an opening in mounting means 16 and is held in place by aset screw 20. - Figure 2 is a side view of the armature assembly of Figure 1. This embodiment uses two fiber brush assemblies each of which contains ten bundles of 0.1524 mm copper fibers such as those used to form flexible commercial welding type cable. Each bundle contains 1,100 wire fibers. These bundles were inserted into openings of cylindrical annealed
copper sleeves 12. The copper sleeves were then rotary swaged untilconductive fibers 10 reached a maximum packing density within each sleeve and thereby formed a single solidified connection. Thesleeves 12 were inserted into analuminum mounting block 16 and secured by way of setscrews 20. Abolt 22 serves as means for attachingmounting block 16 to insulatingsupport structure 14. - Figure 3 is a top view of the brush assembly of the armature assembly of Figure 1. Each end of
sleeve 12 is beveled at anangle 24 of 10° to form a .narrow side 26 and awide side 28. When the brush assembly is mounted onto the armature assembly, thenarrow side 26 ofsleeve 12 is mounted closest to theinsulating support structure 14. Multipleconductive fibers 10 pass through an opening insleeve 12 and are spiralled with respect to the axis ofsleeve 12. Theconductive fibers 10 have been bent as a whole to anangle 30 of 40° at the trailing edge and anangle 32 of 10° at the forward edge. In addition, the ends ofconductive fibers 10 are cut along two planes which lie perpendicular to the axis ofsleeve 12. To improve electrical contact betweenconductive fibers 10 and the projectile launching rails of the launcher, the ends ofconductive fiber 10 are polished to a flat surface. - Armature assemblies in accordance with this invention have been constructed and tested in an electromagnetic launcher. One of these armature assemblies having a brush assembly comprising 7,700 copper fibers, each having a diameter of 0.1524 mm, was used to accelerate a 317 gram projectile to a speed of 4.2 kilometers per second with a pulsed current of 2.1 million amperes. Despite being subjected to a peak acceleration of 236,000 g's., the projectile and armature assembly left the barrel intact and went through the center of a 6.35 mm thick steel witness plate before being destructively caught in a catch tank. Rail damage was minimal, with two smooth dime-shaped holes about 2 millimeters deep having been produced approximately 15 centimeters from the breech of the launcher. The remainder of the rails and insulation showed no damage although all interior surfaces were coated with a thin layer of soot.
- Localized armature melting was eliminated through the use of a plurality of electrical contacts, each having sufficient compliance in a direction normal to the projectile launching rails to minimize resistive heating. Thermal transfer through the solidified center segment of the conductive fibers and through the aluminum brush holder improved heat dissipation. Low contact resistance at extreme current densities was achieved through the use of spiralled conductive fibers which provided an adequate normal force on each of the fibers. This spiral design compensates for variations in rail spacing and permits adequate mechanical compliance for the polished conductive fiber tips to remain in contact with the rail surface. It also provides for continued contact with the conductive rails when the fibers erode as they travel through the barrel. The brush assembly of this invention can be assembled without the need for soldering or metal joining procedures. The spiralled fibers provide self support and limit deflection while in the presence of high electromagnetic fields. Spiralling allows compliance to variations along the contact rails as the armature travels to maintain good electrical contact, thereby reducing the destructive effects of arcing. Through the use of flexible conductive fibers, low contact forces are required to make good electrical contact, thereby resulting in low friction losses.
- For example, although the brush assembly of the armature assembly of this invention has been as an efficient linear sliding contact during a pulsed application, it can also be used as a continuous operating brush on a slip ring surface. Because the conductive fibers have been solidified within the sleeve of the brush assembly, soldering or joining heavy electrical conductors to the brush is possible and can readily be made when required.
Claims (13)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP19840308277 EP0182947B1 (en) | 1984-11-29 | 1984-11-29 | Linear fiber armature for electromagnetic launchers |
DE8484308277T DE3478341D1 (en) | 1984-11-29 | 1984-11-29 | Linear fiber armature for electromagnetic launchers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP19840308277 EP0182947B1 (en) | 1984-11-29 | 1984-11-29 | Linear fiber armature for electromagnetic launchers |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0182947A1 EP0182947A1 (en) | 1986-06-04 |
EP0182947B1 true EP0182947B1 (en) | 1989-05-24 |
Family
ID=8192826
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19840308277 Expired EP0182947B1 (en) | 1984-11-29 | 1984-11-29 | Linear fiber armature for electromagnetic launchers |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP0182947B1 (en) |
DE (1) | DE3478341D1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4422394B4 (en) * | 1994-06-27 | 2004-03-25 | Deutsch-Französisches Forschungsinstitut Saint-Louis, Saint-Louis | Acceleration device for accelerating a missile |
FR2879032B1 (en) * | 2004-12-02 | 2008-02-29 | Saint Louis Inst | MOBILE ELECTRIC CONTACT DEVICE WITH CONDUCTOR RESERVE |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1093895B (en) * | 1958-09-24 | 1960-12-01 | Nelken Kg Dr Ewald | Brush contact for rigid and movable devices of clamping contacts and pantographs |
US3917995A (en) * | 1974-08-26 | 1975-11-04 | Henry H Clinton | Movable brush assembly for making electrical contact with the outer surface of an electrical cable |
US4398113A (en) * | 1980-12-15 | 1983-08-09 | Litton Systems, Inc. | Fiber brush slip ring assembly |
US4457205A (en) * | 1981-12-09 | 1984-07-03 | Westinghouse Electric Corp. | Multiple fiber armatures for electromagnetic launchers |
-
1984
- 1984-11-29 DE DE8484308277T patent/DE3478341D1/en not_active Expired
- 1984-11-29 EP EP19840308277 patent/EP0182947B1/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
EP0182947A1 (en) | 1986-06-04 |
DE3478341D1 (en) | 1989-06-29 |
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