EP0243399A1 - Präzisionseinklemmungsverfahren und dadurch hergestellte wendelstruktur. - Google Patents

Präzisionseinklemmungsverfahren und dadurch hergestellte wendelstruktur.

Info

Publication number
EP0243399A1
EP0243399A1 EP19860906073 EP86906073A EP0243399A1 EP 0243399 A1 EP0243399 A1 EP 0243399A1 EP 19860906073 EP19860906073 EP 19860906073 EP 86906073 A EP86906073 A EP 86906073A EP 0243399 A1 EP0243399 A1 EP 0243399A1
Authority
EP
European Patent Office
Prior art keywords
barrel
rods
wave structure
slow
support rods
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.)
Granted
Application number
EP19860906073
Other languages
English (en)
French (fr)
Other versions
EP0243399B1 (de
Inventor
George M Lee
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.)
Raytheon Co
Original Assignee
Hughes Aircraft Co
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 Hughes Aircraft Co filed Critical Hughes Aircraft Co
Publication of EP0243399A1 publication Critical patent/EP0243399A1/de
Application granted granted Critical
Publication of EP0243399B1 publication Critical patent/EP0243399B1/de
Expired legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J23/00Details of transit-time tubes of the types covered by group H01J25/00
    • H01J23/16Circuit elements, having distributed capacitance and inductance, structurally associated with the tube and interacting with the discharge
    • H01J23/24Slow-wave structures, e.g. delay systems
    • H01J23/26Helical slow-wave structures; Adjustment therefor

Definitions

  • This invention is directed to a precision coining method particularly useful in coining the slow-wave structure of a traveling-wave tube and to the resulting coined helix assembly.
  • a stream of electrons in an electron beam is caused to interact with a propagating electromagnetic wave in a manner which amplifies the electromagnetic wave energy.
  • the electromagnetic wave is propagated along a slow- wave structure, such as an electrically conductive helix wound around the path of the electron beam.
  • the slow-wave structure provides a path of propagation for the magnetic wave which is considerably longer than the axial length of the structure so that the traveling wave may be made to effectively propagate at nearly the velocity of the stream of electrons in the electron beam.
  • Slow-wave structures of the helix type are usually supported within an encasing barrel by means of a plurality of (usually three) equally circumferentially spaced electrically insulating rods positioned around v the helix and within the barrel.
  • One prior method of mounting the helix with its slow-wave structure and support rods within the barrel has been to triangulate the barrel. Initially the barrel is circular in section and it is thereupon distorted by applying forces to three points around its circumference to alter its section from circular toward triangular. When distorted in that manner, the helical slow-wave structure with its support rods is inserted into the distorted barrel.
  • the metallic barrel has an initial inside diameter which is smaller than the circumscribing circle around the support rods so that, if assembled with those dimensions, there would be an interference fit.
  • the barrel is heated and it is made of a material, such as copper, which expands upon heating.
  • an inside diameter is reached which is sufficiently large to receive the helix with its support rods, the helix and its support rods are inserted therein.
  • the barrel reduces in size to embrace the helix with its support rods in an interference fit.
  • FIGURE 1 is an isometric view of the helical slow- wave structure with its attached support rods going into the barrel.
  • FIGURE 2 shows the assembly between dies, with closure of the dies about to malleably coin the barrel around the helical slow-wave structure and its support rods for an interference fit.
  • FIGURE 3 is an end view of the assembly after coining, showing the finished assembly and its inter ⁇ ference fit.
  • the slow-wave structure 10 is shown in FIGURES 1, 2 and 3.
  • the slow-wave structure is made of a rectangular metal ribbon, usually tungsten, wound into a helix to define an interior passage through which the electron beam passes.
  • the passage for the electron beam is of circular section.
  • the external surface of the helix 10 is also of circular section.
  • the helix is straight. In order to maintain the helix of the slow-wave structure 10 in position, it is supported by three support rods 12, 14 and 16.
  • the support rods are made of dielectric material, and beryllium oxide ceramic material is preferred.
  • the support rods are in the forms of right circular solid cylinders.
  • the support rods lie around slow-wave structure 10.to be spaced at equal angles.
  • the support rods 12, 14, and 16 are spaced 120 degrees apart around the axis through the center of the slow-wave structure.
  • the support rods are attached to the slow- wave structure by means of dielectric glue.
  • the glue is illustrated in FIGURE 2 where glue spot 18 is specifi ⁇ cally identified as attaching support rod 12 to slow- wave structure 10.
  • Barrel 20 is a metallic tube in the form of a right circular cylindrical tube. It is made of malleable metal, such as oxygen-free high conductivity copper.
  • the barrel 20 has an initial outside diameter of 0.1078 inch and an initial inside diameter of its inner cylindrical surface 22 of 0.0700 inch.
  • the circumscribing circle around ' the support rods 12, 14 and 16 provides a diametrical clearance within the barrel of 0.0007 inch so that the circum ⁇ scribing circle is 0.0693 inch. While both the subassembly and the barrel are at room temperature, the subassembly is inserted into the barrel. This step is shown in FIGURE 1.
  • FIGURE 2 shows upper and lower dies 24 and 26 which respectively have upper and lower cavities 28 and 30 facing each other.
  • the cavities 28 and 30 form a right circular cylinder when the dies are closed together, with the parting line lying on the axis of the cylinder.
  • the diameter of the cavity, when closed, is 0.1070 inch.
  • FIGURE 3 is a view of the completed assembly.
  • the completed assembly of FIGURE 3 is flushed with " hot acetone to remove the methyl methacrylate glue. Thereupon, the assembly is placed into the traveling-wave tube.
  • the large contact area between the support rods and the barrel is necessary for proper heat transfer out away from the slow-wave structure.
  • the stressed helix provides force on the rods to maintain the helical slow-wave structure in place, upon its proper axis.
  • the plastically deformed copper barrel provides precision placement of the slow-wave structure and proper compression of the support rods onto the helix of the slow-wave structure so that the compressed helix maintains the return force over temperature cycling.
  • the process is fast and accurate so that increased yield is achieved.
  • the small sizes are now producible with accuracy.
  • the compression of the barrel and the slow-wave structure with its supporting rods therein is controlled by employing dies having the desired cavity diameter, in accordance with the size of the parts. An adequate length can be readily achieved.
  • the sizes given are to provide a specific example of the process and article. Other sizes and shapes can be produced by employing different starting parts and dies. Such are within the scope of this invention.

Landscapes

  • Microwave Tubes (AREA)
  • Manufacture Of Electron Tubes, Discharge Lamp Vessels, Lead-In Wires, And The Like (AREA)
  • Forging (AREA)
EP19860906073 1985-10-21 1986-09-15 Präzisionseinklemmungsverfahren und dadurch hergestellte wendelstruktur Expired EP0243399B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US78988285A 1985-10-21 1985-10-21
US789882 1985-10-21

Publications (2)

Publication Number Publication Date
EP0243399A1 true EP0243399A1 (de) 1987-11-04
EP0243399B1 EP0243399B1 (de) 1989-10-18

Family

ID=25148964

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19860906073 Expired EP0243399B1 (de) 1985-10-21 1986-09-15 Präzisionseinklemmungsverfahren und dadurch hergestellte wendelstruktur

Country Status (4)

Country Link
EP (1) EP0243399B1 (de)
JP (1) JPS63501182A (de)
DE (1) DE3666522D1 (de)
WO (1) WO1987002507A1 (de)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4712293A (en) * 1986-11-28 1987-12-15 Hughes Aircraft Company Method for securing a slow-wave structure in enveloping structure with crimped spacers
CN102501032B (zh) * 2011-12-02 2014-01-08 安徽华东光电技术研究所 一种行波管电子枪系统定位弹片的制作工艺

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3271615A (en) * 1961-08-23 1966-09-06 Westinghouse Electric Corp Traveling wave electron discharge device having means exerting a radial force upon the envelope
US3132410A (en) * 1962-03-08 1964-05-12 Cohen Aaron Methods of constructing a traveling wave tube
US3208126A (en) * 1962-05-14 1965-09-28 Sperry Rand Corp Method for making traveling wave tubes
GB984607A (en) * 1962-07-19 1965-02-24 Ferranti Ltd Improvements relating to travelling-wave tubes
US3808677A (en) * 1972-10-10 1974-05-07 Varian Associates Method of fabricating a traveling wave tube

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO8702507A1 *

Also Published As

Publication number Publication date
WO1987002507A1 (en) 1987-04-23
JPH0437535B2 (de) 1992-06-19
EP0243399B1 (de) 1989-10-18
DE3666522D1 (en) 1989-11-23
JPS63501182A (ja) 1988-04-28

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