JPH0327324Y2 - - Google Patents

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Publication number
JPH0327324Y2
JPH0327324Y2 JP5407984U JP5407984U JPH0327324Y2 JP H0327324 Y2 JPH0327324 Y2 JP H0327324Y2 JP 5407984 U JP5407984 U JP 5407984U JP 5407984 U JP5407984 U JP 5407984U JP H0327324 Y2 JPH0327324 Y2 JP H0327324Y2
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JP
Japan
Prior art keywords
collector
vacuum envelope
radiation
collector electrode
metal
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
JP5407984U
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Japanese (ja)
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JPS60164755U (en
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Priority to JP5407984U priority Critical patent/JPS60164755U/en
Publication of JPS60164755U publication Critical patent/JPS60164755U/en
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Description

【考案の詳細な説明】 (1) 考案の属する分野の説明 本考案は、衛星に搭載される高出力進行波管に
主として用いられる輻射冷却形多段コレクタの改
良に関するものである。
[Detailed description of the invention] (1) Description of the field to which the invention pertains The present invention relates to the improvement of a radiation-cooled multistage collector mainly used in high-power traveling wave tubes mounted on satellites.

(2) 従来の技術の説明 衛星に搭載される高出力の進行波管ではコレク
タにおいて消費される電力をできるだけ少なくし
て能率の向上を図るため、コレクタ電極を複数個
に分割してそれぞれ異なつた電圧を印加すること
により、高周波との相互作用を終えて速度分布を
もつようになつた電子をそれぞれの速度に応じて
弁別して、できるだけ熱損失が発生しないように
捕捉する多段コレクタが一般に用いられる。また
コレクタで発生する熱が多いので衛星本体の温度
上昇を防ぐため、コレクタを衛星外壁の外に突き
出した状態で進行波管を衛星に据えつけてコレク
タで発生する熱を直接に宇宙空間に輻射によつて
放散する輻射冷却形コレクタが用いられる。この
ような衛星搭載用の進行波管に用いられる輻射冷
却形多段コレクタは小形、軽量、および振動、温
度などの環境条件に対する非常に高い信頼性が要
求される。
(2) Description of conventional technology In high-power traveling wave tubes mounted on satellites, the collector electrode is divided into multiple parts, each with a different A multi-stage collector is generally used that, by applying a voltage, discriminates electrons that have a velocity distribution after interaction with high frequencies according to their respective velocities and captures them while minimizing heat loss. . In addition, since a lot of heat is generated in the collector, in order to prevent the temperature of the satellite body from rising, a traveling wave tube is installed on the satellite with the collector protruding outside the satellite outer wall, and the heat generated in the collector is radiated directly into space. A radiation-cooled collector is used which dissipates the radiation by . Radiation-cooled multistage collectors used in traveling wave tubes mounted on satellites are required to be small, lightweight, and highly reliable against environmental conditions such as vibration and temperature.

第1図は従来の輻射冷却形多段コレクタの1例
を中心軸を通る平面で切つた断面図で表わしたも
のである。ボデイ1(一部だけ図示)にコレクタ
を支持する支持板2がろう付され、この支持板2
にステンレス製ベローズ3および円筒形の薄肉金
属製の真空外囲器4がろう付され、この真空外囲
器4と皿形の薄肉金属製の真空外囲器5がそれぞ
れのつば部においてアーク溶接されてコレクタの
真空外囲器が形成されている。また支持板2には
ステンレス製支柱6を介して支持板7がろう付さ
れている。この支持板7の外周は、ベローズ3と
真空外囲器4との接続部にろう付されている。薄
い金属板で所要の形状に作られた第1ないし第4
の各コレクタ電極、それぞれ8,9,10,11
は支持板7の円周上数カ所に立てられたネジ14
を支柱として円筒状の磁器製絶縁管12を間には
さんで所要の間隔で保持されている。ネジ14の
先端は支持板13を通した後、ナツト15により
締めつけられている。支持板13は真空外囲器4
および5の接続部に接続されている。第4コレク
タ電極11の中央部は磁器製絶縁板16を介して
真空外囲器5の底面中央部に接続されている。
FIG. 1 is a cross-sectional view of an example of a conventional radiation-cooled multi-stage collector taken along a plane passing through the central axis. A support plate 2 that supports the collector is brazed to the body 1 (only a portion is shown), and this support plate 2
A stainless steel bellows 3 and a cylindrical thin-walled metal vacuum envelope 4 are brazed to the top, and the vacuum envelope 4 and the dish-shaped thin-walled metal vacuum envelope 5 are arc welded at their respective ribs. to form the vacuum envelope of the collector. Further, a support plate 7 is brazed to the support plate 2 via stainless steel columns 6. The outer periphery of this support plate 7 is brazed to the connection portion between the bellows 3 and the vacuum envelope 4. The first to fourth parts are made of thin metal plates into the required shape.
collector electrodes, respectively 8, 9, 10, 11
are screws 14 set at several locations on the circumference of the support plate 7.
They are held at required intervals with cylindrical porcelain insulating tubes 12 being sandwiched between them as supports. The tip of the screw 14 is tightened with a nut 15 after passing through the support plate 13. The support plate 13 is the vacuum envelope 4
and 5. A central portion of the fourth collector electrode 11 is connected to a central portion of the bottom surface of the vacuum envelope 5 via a ceramic insulating plate 16 .

このような構成において第1コレクタないし第
4コレクタ電極には、第1コレクタ電極から順に
低い電圧が給電線(図示せず)によつて印加され
る。したがつて高周波との相互作用により速度分
布を生じた電子ビームは速度の遅い電子から順に
第1、第2、第3、第4コレクタ電極へと入射し
入射するときの速度に応じた熱損失が発生する。
各コレクタ電極で発生した熱の内、大部分は磁器
製絶縁管12或は支持板7,13、更には磁器製
絶縁板16を熱伝導経路として伝導により真空外
囲器に伝達され、真空外囲器表面からは輻射によ
り宇宙空間へ放熱される。ボデイ側への熱伝導は
ステンレス製の支柱6およびベローズ3により十
分抑えられている。
In such a configuration, lower voltages are applied to the first to fourth collector electrodes in order from the first collector electrode through a power supply line (not shown). Therefore, the electron beam, which has a velocity distribution due to the interaction with the high frequency, enters the first, second, third, and fourth collector electrodes in order from the slowest electrons, and heat loss occurs depending on the velocity when the electrons enter. occurs.
Most of the heat generated in each collector electrode is transferred to the vacuum envelope by conduction through the porcelain insulating tube 12 or the support plates 7 and 13, and further through the porcelain insulating plate 16 as a heat conduction path, and is transferred to the vacuum envelope. Heat is radiated from the surface of the envelope into space by radiation. Heat conduction to the body side is sufficiently suppressed by the stainless steel columns 6 and bellows 3.

このように従来の輻射冷却形多段コレクタにお
いては各コレクタ電極で発生した熱はほとんど熱
伝導で真空外囲器に伝達される為、コレクタ電極
と磁器製絶縁管の接続をネジとナツトを用いて機
械的に締め付けて行なう従来構造では、構成部材
の熱膨張の違いのために、接続部の接触状態が悪
くなると、熱放散が悪くなり、したがつてコレク
タ電極温度の上昇を招き、その結果、高温部から
のガス放出による管内真空度の劣化、ひいてはそ
れによる動作不良を生じる恐れがある。また接続
部の熱抵抗を小さくしようとして接続部の接触面
積を大きくすると、コレクタが大形になり重量も
増えることになる。さらに衛星搭載用進行波管に
要求される厳しい振動条件に耐える為には、各コ
レクタ電極をネジとナツトにより機械的に締め付
けて固定する構造の強度をコレクタの使用温度範
囲にわたつて各構成部材の熱膨張の違いを考慮に
入れて維持しなければならず、そのため構造が複
雑になる欠点があつた。
In this way, in conventional radiation-cooled multi-stage collectors, most of the heat generated at each collector electrode is transferred to the vacuum envelope by thermal conduction, so the connection between the collector electrode and the porcelain insulating tube is done using screws and nuts. In the conventional mechanically tightened structure, due to the difference in thermal expansion of the components, if the contact condition of the connection becomes poor, heat dissipation will be poor, resulting in an increase in the collector electrode temperature, and as a result, There is a risk that the degree of vacuum inside the tube will deteriorate due to gas discharge from the high temperature section, and this may lead to malfunction. Furthermore, if the contact area of the connecting portion is increased in an attempt to reduce the thermal resistance of the connecting portion, the collector will become larger and its weight will also increase. Furthermore, in order to withstand the severe vibration conditions required for traveling wave tubes onboard satellites, the strength of the structure in which each collector electrode is mechanically tightened and fixed using screws and nuts must be maintained over the operating temperature range of the collector. This has to be maintained by taking into account the difference in thermal expansion between the two, which has the disadvantage of complicating the structure.

(3) 考案の目的 本考案の目的は、このような従来の欠点をとり
除いた輻射冷却形多段コレクタを提供するもの
で、外周部に径方向のスリツトを入れたコレクタ
電極と、真空外囲器内面にろう付した断面が馬蹄
形の金属製支持体を磁器製絶縁体を介してろう付
により接続固定している為、熱抵抗の小さい耐振
性のある簡単な構造の輻射冷却形多段コレクタが
得られる。以下、図面に基づいて本考案の実施例
の説明を行なう。
(3) Purpose of the invention The purpose of the invention is to provide a radiation-cooled multi-stage collector that eliminates these conventional drawbacks. A metal support with a horseshoe-shaped cross section is brazed to the inner surface of the container and is connected and fixed by brazing through a porcelain insulator, resulting in a radiation-cooled multi-stage collector with a simple structure that has low thermal resistance and vibration resistance. can get. Embodiments of the present invention will be described below based on the drawings.

(4) 考案の構成および作用の説明 第2図aは本考案を適用した輻射冷却形多段コ
レクタを中心軸を通る平面で切つた断面図を第2
図bは本考案の主要な部分を示す斜視図を表わし
ている。ボデイ1(一部だけ図示)にコレクタを
支持する支持板2がろう付され、この支持板2に
ステンレス製ベローズ3および円筒形の薄肉金属
製の真空外囲器4がろう付され、この真空外囲器
4と皿形の薄肉金属製の真空外囲器5がそれぞれ
のつば部においてアーク溶接されてコレクタの真
空外囲器が形成されている。支持板2にはステン
レス製支柱6を介して支持板7がろう付されてい
る。この支持板7の外周はベローズ3と真空外囲
器4との接続部にろう付されている。薄い金属板
で所要の形状に作られた第1ないし第4の各コレ
クタ電極17,18,19,20には外周部に径
方向のスリツト23が軸対称に複数入れられてい
る。スリツトの幅およびスリツトの深さはコレク
タ電極に印加した電圧によつて得られる電界を大
きく乱さないように配慮して決められる。一方、
円筒形の薄肉金属製の真空外囲器4の内面には、
各コレクタ電極17〜20の外周にそつて、断面
が馬蹄形をした金属製支持体21が複数個ろう付
されている。そして、各コレクタ電極17〜20
はこれら金属製支持体21と、間に磁器製絶縁体
22をはさんでろう付により固定されている。な
お、第4コレクタ電極20の中央部は従来形と同
様磁器製絶縁板16を介して真空外囲器5の底面
中央部に接続されている。
(4) Explanation of the structure and operation of the invention Figure 2a is a cross-sectional view of a radiation-cooled multi-stage collector to which the invention is applied, taken along a plane passing through the central axis.
Figure b shows a perspective view showing the main parts of the invention. A support plate 2 that supports the collector is brazed to the body 1 (only a portion is shown), a stainless steel bellows 3 and a cylindrical thin-walled metal vacuum envelope 4 are brazed to the support plate 2, and the vacuum An envelope 4 and a dish-shaped vacuum envelope 5 made of thin metal are arc welded at their respective flanges to form the vacuum envelope of the collector. A support plate 7 is brazed to the support plate 2 via stainless steel columns 6. The outer periphery of this support plate 7 is brazed to the connection portion between the bellows 3 and the vacuum envelope 4. Each of the first to fourth collector electrodes 17, 18, 19, 20 made of a thin metal plate into a desired shape has a plurality of radial slits 23 axially symmetrically formed in the outer periphery thereof. The width of the slit and the depth of the slit are determined so as not to greatly disturb the electric field obtained by the voltage applied to the collector electrode. on the other hand,
On the inner surface of the cylindrical thin-walled metal vacuum envelope 4,
A plurality of metal supports 21 each having a horseshoe-shaped cross section are brazed along the outer periphery of each of the collector electrodes 17 to 20. And each collector electrode 17 to 20
is fixed to these metal supports 21 by brazing with a porcelain insulator 22 interposed therebetween. Note that the central portion of the fourth collector electrode 20 is connected to the central portion of the bottom surface of the vacuum envelope 5 via a ceramic insulating plate 16, as in the conventional type.

このような構成において第1ないし第4コレク
タ電極17〜20で発生した熱の内、一部は輻射
によつて高温のコレクタ電極から低温のコレクタ
電極に、或は各コレクタ電極から真空外囲器4,
5に伝達されるものの、ほとんどの熱は伝導によ
り、磁器製絶縁体22を通り、金属製支持体21
に伝達され、更に真空外囲器4,5に伝達され
る。構成部材の熱膨張の違いによる機械ストレス
については各コレクタ電極に設けたスリツト23
および断面が馬蹄形の金属製支持体21により軽
減される。
In such a configuration, part of the heat generated in the first to fourth collector electrodes 17 to 20 is transferred from the high temperature collector electrode to the low temperature collector electrode or from each collector electrode to the vacuum envelope by radiation. 4,
5, most of the heat passes through the porcelain insulator 22 by conduction and is transferred to the metal support 21.
and further transmitted to the vacuum envelopes 4 and 5. Mechanical stress due to differences in thermal expansion of constituent members can be reduced by using slits 23 provided in each collector electrode.
and is reduced by a metal support 21 having a horseshoe-shaped cross section.

(5) 効果の説明 以上説明したように本考案による輻射冷却形多
段コレクタを用いれば、外周部に径方向に複数の
スリツトが入つたコレクタ電極を真空外囲器内面
にろう付された断面が馬蹄形の金属製支持体に、
磁器製絶縁石を介してろう付で固定している為、
コレクタ電極と真空外囲器の間の熱抵抗を小さく
することができ、各コレクタ電極で発生した熱を
低い温度差で真空外囲器に伝達できる。その結
果、コレクタ電極温度の上昇によるガス放出など
の不具合の発生が避けられる。また、進行波管の
動作状態の変化に応じてコレクタの発生熱量が変
化した場合でも、コレクタの構成部材には機械的
ストレスはほとんどない為、常に安定した熱放散
特性が得られる。さらには、構成が簡単である
為、コレクタを小形軽量にすることができ、耐振
性上有利となる。
(5) Explanation of Effects As explained above, if the radiation-cooled multi-stage collector of the present invention is used, the cross-section of the collector electrode, which has multiple radial slits in the outer circumference, is brazed to the inner surface of the vacuum envelope. On a horseshoe-shaped metal support,
Because it is fixed by brazing through a porcelain insulating stone,
The thermal resistance between the collector electrode and the vacuum envelope can be reduced, and the heat generated at each collector electrode can be transferred to the vacuum envelope with a small temperature difference. As a result, problems such as gas release due to an increase in collector electrode temperature can be avoided. Furthermore, even if the amount of heat generated by the collector changes in response to changes in the operating state of the traveling wave tube, there is almost no mechanical stress on the components of the collector, so stable heat dissipation characteristics can always be obtained. Furthermore, since the configuration is simple, the collector can be made small and lightweight, which is advantageous in terms of vibration resistance.

なお上記実施例はコレクタ電極が4段の場合で
あつたがコレクタ電極数が異なる場合にも適用で
きるのはもちろんである。
In the above embodiment, the collector electrodes are arranged in four stages, but it is of course applicable to cases where the number of collector electrodes is different.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は、従来の輻射冷却形多段コレクタの断
面図、第2図aは本考案による輻射冷却形多段コ
レクタを示す断面図、第2図bは本考案の主要な
部分を示す斜視図である。 1……ボデイ、2,7,13……支持板、3…
…ベローズ、4,5……真空外囲器、8,9,1
0,11,17,18,19,20……第1,
2,3,4コレクタ電極、12……磁器製絶縁
管、16……磁器製絶縁板、22……磁器製絶縁
体、14……ネジ、15……ナツト、21……金
属製支持体、23……スリツト。
FIG. 1 is a sectional view of a conventional radiation-cooled multistage collector, FIG. 2a is a sectional view of a radiation-cooled multistage collector according to the present invention, and FIG. 2b is a perspective view showing the main parts of the present invention. be. 1...Body, 2, 7, 13...Support plate, 3...
...Bellows, 4,5...Vacuum envelope, 8,9,1
0, 11, 17, 18, 19, 20...1st,
2, 3, 4 collector electrodes, 12... Porcelain insulating tube, 16... Porcelain insulating plate, 22... Porcelain insulator, 14... Screw, 15... Nut, 21... Metal support, 23...Slit.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 円筒状の金属製真空外囲器の中に軸方向に、複
数のコレクタ電極が所要の間隔に配設され、前記
コレクタ電極で発生した熱が前記金属製真空外囲
器から外部に輻射で放熱される輻射冷却形多段コ
レクタにおいて、各コレクタ電極の外周部に径方
向に複数のスリツトを設け、前記金属製真空外囲
器の内面には断面が馬蹄形の金属製支持体を複数
個ろう付し、前記コレクタ電極と前記金属製支持
体とを磁器製絶縁体を介してろう付により固定し
たことを特徴とする輻射冷却形多段コレクタ。
A plurality of collector electrodes are arranged at required intervals in the axial direction in a cylindrical metal vacuum envelope, and the heat generated at the collector electrodes is radiated from the metal vacuum envelope to the outside. In the radiation-cooled multi-stage collector, a plurality of slits are provided in the radial direction on the outer periphery of each collector electrode, and a plurality of metal supports each having a horseshoe-shaped cross section are brazed to the inner surface of the metal vacuum envelope. A radiation-cooled multi-stage collector, characterized in that the collector electrode and the metal support are fixed by brazing via a ceramic insulator.
JP5407984U 1984-04-12 1984-04-12 Radiation-cooled multi-stage collector Granted JPS60164755U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5407984U JPS60164755U (en) 1984-04-12 1984-04-12 Radiation-cooled multi-stage collector

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5407984U JPS60164755U (en) 1984-04-12 1984-04-12 Radiation-cooled multi-stage collector

Publications (2)

Publication Number Publication Date
JPS60164755U JPS60164755U (en) 1985-11-01
JPH0327324Y2 true JPH0327324Y2 (en) 1991-06-13

Family

ID=30575522

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5407984U Granted JPS60164755U (en) 1984-04-12 1984-04-12 Radiation-cooled multi-stage collector

Country Status (1)

Country Link
JP (1) JPS60164755U (en)

Also Published As

Publication number Publication date
JPS60164755U (en) 1985-11-01

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