EP0182947B1 - Linear fiber armature for electromagnetic launchers - Google Patents

Linear fiber armature for electromagnetic launchers Download PDF

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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
Application number
EP19840308277
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German (de)
French (fr)
Other versions
EP0182947A1 (en
Inventor
Joseph Scuro
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
CBS Corp
Original Assignee
Westinghouse Electric Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Priority to EP19840308277 priority Critical patent/EP0182947B1/en
Priority to DE8484308277T priority patent/DE3478341D1/en
Publication of EP0182947A1 publication Critical patent/EP0182947A1/en
Application granted granted Critical
Publication of EP0182947B1 publication Critical patent/EP0182947B1/en
Expired legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41BWEAPONS FOR PROJECTING MISSILES WITHOUT USE OF EXPLOSIVE OR COMBUSTIBLE PROPELLANT CHARGE; WEAPONS NOT OTHERWISE PROVIDED FOR
    • F41B6/00Electromagnetic launchers ; Plasma-actuated launchers
    • F41B6/006Rail launchers
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R41/00Non-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 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. In this embodiment, an opening 18 is shown within insulating support structure 14 for receiving a projectile. However, 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.
  • 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 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.
  • 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 an angle 24 of 10° to form a . narrow side 26 and a wide side 28. When the brush assembly is mounted onto the armature assembly, 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. In addition, 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. 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)

1. An armature for conducting large DC currents between a pair of electrically conductive rails while being driven along the rails under the influence of electromagnetic forces generated by the application of said very large DC currents, said armature comprising an insulating support structure (14), a plurality of conductive fibers (10), and characterized by a cylindrical sleeve (12) having an opening in which said conductive fibers are positioned, said conductive fibers (10) being compacted to form a solid mass within said sleeve (12), means (16) for mounting said sleeve on said support structure (14), said conductive fibers (10) being spirally disposed with respect to the axis of said sleeve (12).
2. An armature as claimed in claim 1, characterized by each end of said sleeve (12) being beveled at an angle of 10° such that said sleeve (12) has a narrow side and a wide side with the narrow side being closer to said support structure (14).
3. An armature as claimed in claim 1 or 2, characterized by said conductive fibers (10) being bent at an angle between 10° and 40° with respect to the axis of said sleeve (12), with said conductive fibers (10) which are closest to said support structure (14) being bent at an angle of 10° and said conductive fibers (10) which are farthest from said support structure (14) being bent at an angle of 40°.
4. An armature as claimed in any of claims 1 to 3, characterized by said means for mounting said sleeve on said support structure comprises a mounting block (16) having an aperture for receiving said sleeve.
5. An armature as claimed in claim 4 characterized by said mounting block (16) being substantially of aluminum.
6. An armature as claimed in any one of claims 1 to 5, characterized by one end of each of said conductive fibers (10) being cut along a first plane perpendicular to the axis of said sleeve (12) and the other end of each of said conductive fibers (10) is cut along a second plane perpendicular to the axis of said sleeve (12).
7. An armature as claimed in any one of claims 1 to 6, characterized by said plurality of conductive fibers (10) comprises approximately 7,700 conductive fibers.
8. An armature as claimed in claim 7, characterized by said conductive fibers being copper strands.
9. An armature as claimed in any one of claims 1 to 8, characterized by said sleeve (12) comprises an annealed copper cylinder having been swaged to compact said conductive fibers (10) to form said solid mass.
10. An armature as claimed in any one of claims 1 to 9, characterized by said conductive fibers (10) being polished on each end in a plane perpendicular to the axis of said sleeve (12).
11. A high current brush for an armature as claimed in any one of claims 1 to 10, in which the brush comprises a plurality of conductive fibers (10), characterized by a cylindrical sleeve (12) having an opening through which said conductive fibers (10) pass, and said conductive fibers (10) are compacted to form a solid mass within said sleeve (12), said conductive fibers (10) being spirally disposed with respect to the axis of said sleeve (12).
12. A high current brush as claimed in claim 11, characterized by one end of each of said conductive fibers (10) being cut along a plane perpendicular to the axis of said sleeve (12).
13. A high current brush as claimed in any one of claims 11 to 12, characterized by said conductive fibers (10) being copper strands each having a diameter of 0.1524 mm.
EP19840308277 1984-11-29 1984-11-29 Linear fiber armature for electromagnetic launchers Expired EP0182947B1 (en)

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

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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

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DE (1) DE3478341D1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
EP0182947A1 (en) 1986-06-04
DE3478341D1 (en) 1989-06-29

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