US3466494A - Traveling wave tube with delay line supports having a lossy layer and an insulation layer - Google Patents
Traveling wave tube with delay line supports having a lossy layer and an insulation layer Download PDFInfo
- Publication number
- US3466494A US3466494A US725848A US3466494DA US3466494A US 3466494 A US3466494 A US 3466494A US 725848 A US725848 A US 725848A US 3466494D A US3466494D A US 3466494DA US 3466494 A US3466494 A US 3466494A
- Authority
- US
- United States
- Prior art keywords
- layer
- attenuation
- delay line
- traveling wave
- 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.)
- Expired - Lifetime
Links
- 238000009413 insulation Methods 0.000 title description 12
- 239000010410 layer Substances 0.000 description 70
- 238000013016 damping Methods 0.000 description 9
- 239000000463 material Substances 0.000 description 8
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 6
- 238000000034 method Methods 0.000 description 6
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 6
- 229910002804 graphite Inorganic materials 0.000 description 4
- 239000010439 graphite Substances 0.000 description 4
- 235000012239 silicon dioxide Nutrition 0.000 description 4
- 230000007704 transition Effects 0.000 description 4
- 238000010894 electron beam technology Methods 0.000 description 3
- 230000003628 erosive effect Effects 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000036961 partial effect Effects 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 239000010453 quartz Substances 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 2
- 239000012774 insulation material Substances 0.000 description 2
- 238000010849 ion bombardment Methods 0.000 description 2
- 150000002500 ions Chemical class 0.000 description 2
- 238000005507 spraying Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 239000000725 suspension Substances 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- VXAUWWUXCIMFIM-UHFFFAOYSA-M aluminum;oxygen(2-);hydroxide Chemical compound [OH-].[O-2].[Al+3] VXAUWWUXCIMFIM-UHFFFAOYSA-M 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000011229 interlayer Substances 0.000 description 1
- 239000000395 magnesium oxide Substances 0.000 description 1
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 1
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 description 1
- 230000000873 masking effect Effects 0.000 description 1
- XZWYZXLIPXDOLR-UHFFFAOYSA-N metformin Chemical compound CN(C)C(=N)NC(N)=N XZWYZXLIPXDOLR-UHFFFAOYSA-N 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- 239000011253 protective coating Substances 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000011241 protective layer Substances 0.000 description 1
- 150000003377 silicon compounds Chemical class 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- LIVNPJMFVYWSIS-UHFFFAOYSA-N silicon monoxide Chemical compound [Si-]#[O+] LIVNPJMFVYWSIS-UHFFFAOYSA-N 0.000 description 1
- 229910052814 silicon oxide Inorganic materials 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J23/00—Details of transit-time tubes of the types covered by group H01J25/00
- H01J23/16—Circuit elements, having distributed capacitance and inductance, structurally associated with the tube and interacting with the discharge
- H01J23/24—Slow-wave structures, e.g. delay systems
- H01J23/30—Damping arrangements associated with slow-wave structures, e.g. for suppression of unwanted oscillations
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J23/00—Details of transit-time tubes of the types covered by group H01J25/00
- H01J23/16—Circuit elements, having distributed capacitance and inductance, structurally associated with the tube and interacting with the discharge
- H01J23/24—Slow-wave structures, e.g. delay systems
- H01J23/26—Helical slow-wave structures; Adjustment therefor
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49002—Electrical device making
- Y10T29/49016—Antenna or wave energy "plumbing" making
Description
Sept. 9, 1969 w. EICHIN ETAL 3,466,494
TRAVELING WAVE TUBE WITH DELAY LINE SUPPORTS HAVING A LOSSY LAYER AND AN INSULATION LAYER Filed May 1. 1968 2 Sheets-Sheet 1 Fig.1 5" ,5
I #a ur BWMLM-ATTORNEYS INVENTORSI &466.494
W. EICHIN ETAL TRAVELING WAVE TUBE WITH DELAY LINE SUPPORTS HAVING A LOSSY LAYER AND AN INSULATION LAYER 2 Sheets-Sheet 2 Filed May 1, 1968 Fig.5
'1 w, INVENTORS l VfR/VE& E/cJ/A/ V I i w -M #sa/war %472 BY wm' mwonuas United States Parent O U.S. Cl. 315-3.5 15 Claims ABSTRACT OF THE DISCLOSURE A traveling wave tube comprsing a spiral delay' line supported by longitudinal supporting rods which are coated with an attenuation layer. An insulaton layer is formed over the attenuation layer at least except at the points of contact between the spiral delay line and the supporting rods so as to prevent the dropping of the operating attenuation due to erosion during use.
BACKGROUND OF THE INVENTION Field of the invention The invention relates in general to traveling wave tubes and particularly to support means for a delay line of the spiral type.
Description of the prior art In prior traveling wave tubes with spital delay lines supported by rods along the periphery it has been known to cover the rods with an attenuation layer with an insulaton layer..
However, in such structures due to the presence of the insulating interlayer between the spiral delay line and the damping layer, the conductance of the high frequency transition is not suicient to provide attenuation (damping) of feedback or self-excitation of 75 db. or more, which is necessary for the operation of high efficiency traveling wave tubes using a spiral or helical delay line.
Recent traveling wave tubes with a helical line supported between insulating bars have had only a damping layer with no insulating layer, and the helx (spiral) is normally allowed to lie directly against the damping (attenuation) layer. Such damping layers are usually composed of a material containing mostly carbon or graphite and the use of such layers allows high values of Operating attenuating (more than 75 db.) to be obtained. With such structures well defined high-frequency transitions between the helical line and the damping layer can be obtained. However, the Operating attenuation must not drop below a certain value during the life of the tube. The tube life is normally determined by the cathode of the tube. It has -been shown that attenuation layers with a protective coating give more constant Operating characteristcs than those without, so for that reason the protective layer should not be dspensed with.
SUMMARY OF THE INVENTION The present invention overcomes the shortcomings of the prior art by providing a traveling wave tube with a helical delay line which is supported .between -dielectrc holding or support bars which are coated with a damping layer, in such a way that the electrioal properties of the damping (attenuation) layer remain largely preserved in the operation of the tube and which are coated by an insulaton layer at points excepts where the support bars engage the helical delay line.
We have discovered that the undesired dropping of the Operating attenuation in prior traveling wave tubes has 3,466,494 Patented Sept. 9, 1969 'ice been caused by eroson of the attenuation layer, which is caused by the impact of ions which come from the residual gas content of the tube. We have verified this phenomenon with experiments using an electron-microscope. The insulaton layer of the present invention protects the attenuation layer from ion impact and because of the conductive contact between the delay line and attenuation layer an Operating attenuation of over db. is obtained.
Many other advantages, features and additional objects of the present invention will become manifest to those versed in the art upon making reference to the detailed description and the accompanying sheets of drawings in which preferred structural embodiments incorporating the principles of the present invention are shown by way of illustrative example.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a partial cross-sectional view of a supporting rod and helx.
FIG. 2 is a side view of a supporting rod showing the points of a contact of the helx.
FIG. 3 is a partial cross-sectional view of a modification of a support rod and helx.
FIG. 4 is an end View of three supporting rods and illustrates a manner of applying the protective insulation layers according to this invention.
FIG. 5 is a' side view of a support bar of FIG. 4; and
FIG. 6 is a schematic view of a traveling wave tube.
DESCRIPTION OF THE PREFERRED EMBODIMENTS FIG. 6 illustrates schematically a traveling wave tube having san electron source 10 which passes electron beam through the helx 1. The helx 1 is supported between parallel spaced supporting rods 2, 2' and 2". The vacuum envelope and the catcher of the tube as well as the input and output couplings are not illustrated since such structures are well known to those skilled in the art. For a detail description of a traveling wave tube reference may be made to Patent No. 2,626,371.
The supporting rods 2, 2' and 2" may be made of quartz for example and are formed by grinding quartz to a tolerance of 2 microns for example. Each of the rods 2, 2' and 2" are coated with an attenuation layer, 3, 3' and 3". A single bar is shown in FIGS. 1 and 2, for example, and the attenuation layer 3 is formed by a suitable carburization process or by painting or spraying on a graphite solution in which graphite is in suspension.
After the attenuation layer 3 has been formed on the rods insulating layers 4, 4' and 4" are formed on the rods 2, 2' and 2". The insulating layer 4 may comprise .for example silicon dioxide and may be attached by a vaporizing-on process, for example.
At points 5 on the rods 2, 2' and 2" at which the helx 1 engages the rods 2, 2' and 2" the insulating layers 4, 4' and 4" is left oli. 'In other words at the points 5 illustrated in FIG. 2 for example the attenuation layer 3 is formed on the rods 2, 2' and 2" but the insulaton layer 4 s not formedat those points. This may be accomplished for example by masking the points 5 as the insulaton layer is applied by vaporizing-on or other suitable process.
FIG. 1 for example is a partial view of a rod 2 illustrating the attenuation layer 3 which covers the entire surface of the rod 2 and shows the insulating layer 4 overlaying the attenuation layer 3 at all points except where the helx 1 engages the rod. These points are indicated by the numeral 5 in FIG. l, for example.
FIG. 2 is a side view of a rod 2 illustrating the points 5.
FIG. 3 illustrates a modification of the invention wherein a rod 2 is formed with depressions 6 between adjacent coils of the helix 1 and the coils of the helix 1 engage the rod 2 at extensions 11 formed in the rods 2. The' depression 6 may be milled for example into the rods 2 and the attenuation layer 3 is applied over the entire surface of the rods. An insulating layer 4 may then be formed over the entire surface of the rod including the attenuation layer and then the projections 11 may be ground or otherwise milled down so as to remove the insulation layer on the projections 11. However, the attenuation layer is left on the projections 11 so that the turns of the helix 1 engage the attenuation layer.
FIGS. 4 and 5 illustrate a particular manner in which rods 2, 2' and 2" may be formed. The rods 2, 2' and 2" are coated with a suitable attenuation layer 3 over their entire surfaces. Then the rods are spaced together as shown in FIG. 4 and the three rods are coated with a suitable insulating layer 4 as for example SiO For example, the three rods may be placed into a chamber in which a silicon compound is decomposed into a gaseous form by thermal chemical action in the presence of oxygen so that Si will be formed. The rods act as masks to cover the areas 7 at which they engage each other and the surfaces of the rods 2, 2' and 2" will be coated with an insulation layer except at lines along their longitudinal lengths as shown in FIGS. 4 and 5. As shown in FIG. a narrow strip 7 will be formed on the rods 2 which does not have a coating of insulation layer 4. Because of the close galvanic contact between the helical delay line 1 and the attenuation layer 3 in the assembled traveling wave tube even the complete erosion of the small area 7 between the turns of the helix 1 will not appreciably reduce the operating attenuation of the traveling wave tube. The places of contact, themselves, are protected from impact by the helix 1 which at those places engages the bar directly. The current, then, which at first tends to run preferentially along these exposed zones in the attenuation layer 3, is thus deflected by the erosion of the attenuation layer 3, into the adjacent zones of the attenuation layer which are protected by the insulation.
The insulating layer may be tormed of various materials as, for example, aluminum dioxide, magnesium oxide and particularly SiO All of these substances are capable of being installed in a vacuum and particularly resistant to ion bombardment. The structure according to the invention to avoid undesirable reflections requires that the attenuation layer should provide a smooth transition from the damped to the undampcd part of the delay line since reflections occur at discontinuities and the smooth transition will therefore, substantially eliminate reflections. To improve the impedance matching characteristics of the helical line 1 the thickness and length of the damping or attenuation layer 3 may -be gradually decreased towards both ends of the helix as shown in FIG. 6 so as to suitably match the impedance. Thus in the end areas it is very important that the insulation layer covers the attenuation layer to protect it from ion bombardment which would remove the impedance layer and result in a discontinuity.
It will be understood that variations and modifications may be efiected without departing from the spirit and scope of the novel concepts of this invention.
What we claim is:
1. A travelng wave tube with an electron beam comprisng:
a delay line through which the electron beam passes,
support means in engagement with the delay line,
the support means covered with a first layer of attenuation material, and
the support means covered with a second layer of insulation material which overlaps the first layer of attenuation material at least except at the points of contact between the delay line and the support means.
2. Apparatus according to claim 1 wherein the delay line comprises a helix formed from electrical conducting material.
3. Apparatus according to claim 2 wherein the support means comprises at least one longitudinal member which engages the helix at a number of points.
4. Apparatus according to claim 3 wherein the support means comprises a plurality of rods of quartz.
5. Apparatus according to claim 4 wherein the rods are formed with projections at the points at which they engage the helix.
6. Apparatus according to claim 4 wherein the first layer of attenuation material has relatively low electrical impedance.
7. Apparatus according to claim 6 wherein the first layer is formed of carbon.
8. Apparatus according to claim 6 wherein the first layer is in the form of a graphite suspension.
9. Apparatus according to claim 6 wherein the thickness of the first layer of attenuation material is thicker at the mid portion of the helix than it is at either end of the helix.
10. Apparatus according to claim 6 wherein the second layer of insulation material comprises a refractory oxide.
11. Apparatus according to claim 9 wherein the second layer comprises silicon oxide.
12. Apparatus according to claim 9 wherein the helix makes good electrical contact with the first attenuation layer on the rods.
, 13. The method of formng longitudinal members for supporting a helix of a traveling wave tube comprising:
spraying a layer of attenuation material on the longitudinal members and forming an insulation layer on the longitudinal members except at the points where they engage the helix.
, 14. The method of claim 13 wherein the longitudinal members are covered completely with the layer of attenuation material and are then stacked so that they engage at lines along their longitudinal lengths and are then covered with the insulation layer except at the lines where they engage.
15. The method of claim 13 wherein the insulation layer is formed on the longitudinal members with a mask formed to cover the longitudinal members except where they engage the helix.
References Cited UNITED STATES PATENTS 2,903,657 11/1954 Eichin 315-393 HERMAN KARL SAALBACH, Primary Examiner F. PRINCE BUTLER, Assistant Examiner U.S. CI. X.R.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US72584868A | 1968-05-01 | 1968-05-01 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3466494A true US3466494A (en) | 1969-09-09 |
Family
ID=24916203
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US725848A Expired - Lifetime US3466494A (en) | 1968-05-01 | 1968-05-01 | Traveling wave tube with delay line supports having a lossy layer and an insulation layer |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3466494A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3832593A (en) * | 1972-06-28 | 1974-08-27 | Siemens Ag | Selectively damped travelling wave tube |
| FR2646732A1 (en) * | 1989-05-04 | 1990-11-09 | Raytheon Co | HIGH FREQUENCY AMPLIFIER HAVING SLOW WAVE STRUCTURE |
| EP0534762A1 (en) * | 1991-09-27 | 1993-03-31 | Nec Corporation | Dielectric support rod for a traveling-wave tube |
| US5274304A (en) * | 1991-04-01 | 1993-12-28 | Nec Corporation | Helix type traveling wave tube structure with supporting rods covered with boron nitride or artificial diamond |
| US5495144A (en) * | 1993-02-03 | 1996-02-27 | Nec Corporation | Helical slow-wave circuit assembly with reduced RF losses |
| US20120067462A1 (en) * | 2009-06-01 | 2012-03-22 | Toyo Tanso Co., Ltd. | Method for carburizing tantalum member, and tantalum member |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2903657A (en) * | 1953-12-10 | 1959-09-08 | Siemens Ag | Wave conductor, particularly for travelling wave tubes |
-
1968
- 1968-05-01 US US725848A patent/US3466494A/en not_active Expired - Lifetime
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2903657A (en) * | 1953-12-10 | 1959-09-08 | Siemens Ag | Wave conductor, particularly for travelling wave tubes |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3832593A (en) * | 1972-06-28 | 1974-08-27 | Siemens Ag | Selectively damped travelling wave tube |
| FR2646732A1 (en) * | 1989-05-04 | 1990-11-09 | Raytheon Co | HIGH FREQUENCY AMPLIFIER HAVING SLOW WAVE STRUCTURE |
| US5038076A (en) * | 1989-05-04 | 1991-08-06 | Raytheon Company | Slow wave delay line structure having support rods coated by a dielectric material to prevent rod charging |
| US5274304A (en) * | 1991-04-01 | 1993-12-28 | Nec Corporation | Helix type traveling wave tube structure with supporting rods covered with boron nitride or artificial diamond |
| EP0534762A1 (en) * | 1991-09-27 | 1993-03-31 | Nec Corporation | Dielectric support rod for a traveling-wave tube |
| US5495144A (en) * | 1993-02-03 | 1996-02-27 | Nec Corporation | Helical slow-wave circuit assembly with reduced RF losses |
| US20120067462A1 (en) * | 2009-06-01 | 2012-03-22 | Toyo Tanso Co., Ltd. | Method for carburizing tantalum member, and tantalum member |
| US8986466B2 (en) * | 2009-06-01 | 2015-03-24 | Toyo Tanso Co., Ltd. | Method for carburizing tantalum member, and tantalum member |
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