JPH04106841A - Travelling-wave tube for mounting on satelite - Google Patents

Travelling-wave tube for mounting on satelite

Info

Publication number
JPH04106841A
JPH04106841A JP22292590A JP22292590A JPH04106841A JP H04106841 A JPH04106841 A JP H04106841A JP 22292590 A JP22292590 A JP 22292590A JP 22292590 A JP22292590 A JP 22292590A JP H04106841 A JPH04106841 A JP H04106841A
Authority
JP
Japan
Prior art keywords
collector
slow
case
case cover
supporting plates
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
JP22292590A
Other languages
Japanese (ja)
Other versions
JP2679379B2 (en
Inventor
Toru Mitsui
徹 三井
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.)
NEC Corp
Original Assignee
NEC 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 NEC Corp filed Critical NEC Corp
Priority to JP2222925A priority Critical patent/JP2679379B2/en
Publication of JPH04106841A publication Critical patent/JPH04106841A/en
Application granted granted Critical
Publication of JP2679379B2 publication Critical patent/JP2679379B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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  • Microwave Tubes (AREA)

Abstract

PURPOSE:To make it possible to set the optimum size electrically, thermally, and mechanically in compact size with light weight by using trapezoid supporting plates as a case cover too. CONSTITUTION:A travelling-wave tube is composed of a slow-wave structure l in which microwave is amplified by reciprocal action with electrons, a radiation cooling collector 7 which captures the reciprocally acted electrons and discharges the generated heat to the space by radiation, a case substrate 8 which discharges the heat of the slow-wave structure l by transmission, a disk- like holding plate 9 to hold the collector 7, a case cover 10 to shield electromagnetic waves from the slow-wave structure 1, and trapezoid supporting plates 11 to support the holding plate 9 and the case substrate 8, and the trapezoid supporting plate 11 composes a part of the case cover. By making the structure in this way, two trapezoid supporting plates 11 are fixed in the positions close the slow-wave structure l. As a result, the size of the collector 7 is made the optimum thermally and electrically and further the disk-like supporting plate 9, trapezoid supporting plates 11, and the case substrate 8 are made small.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、進行波管に関し、特に輻射冷却コレクタを有
する衛星搭載用進行波管に関する。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a traveling wave tube, and more particularly to a traveling wave tube for use in a satellite having a radiation-cooled collector.

〔従来の技術〕[Conventional technology]

従来の輻射冷却コレクタを有する衛星搭載用進行波管は
、電子を射ヨする電子銃(図示せず)。
A conventional traveling wave tube onboard a satellite having a radiation-cooled collector is an electron gun (not shown) that shoots electrons.

マイクロ波を電子と相互作用させ増幅する遅波回路、相
互作用した電子を捕獲するコレクタおよびこれらを収納
し強固に支持・固定するケースより構成される。一般的
に衛星搭載用高出力進行波管のコレクタは、熱の冷却を
考慮して輻射冷却タイプが採用される。従来のコレクタ
の例を第2図(a)、(b)に示す。この輻射冷却コレ
クタ2は、円板状保持板3に固定され、さらに十分な耐
振強度を確保するなめ台形状支持板4によりケース基板
5に支持されている。又、衛星内に設置される進行波管
は、他の電子機器に悪影響を与えないために遅波回路1
から発生する電磁波をシールドしなければならない。ケ
ースカバー6は、このシールド効果があり、ケース基板
5及び保持板3に導電性接着剤により密着して固定され
る。
It consists of a slow-wave circuit that amplifies microwaves by interacting with electrons, a collector that captures the interacted electrons, and a case that houses and firmly supports and fixes them. In general, collectors for high-power traveling wave tubes mounted on satellites are of the radiation-cooled type in consideration of heat cooling. Examples of conventional collectors are shown in FIGS. 2(a) and 2(b). This radiation-cooled collector 2 is fixed to a disk-shaped holding plate 3, and further supported by a case substrate 5 by a trapezoid-shaped support plate 4 that ensures sufficient vibration resistance. In addition, the traveling wave tube installed inside the satellite is equipped with a slow wave circuit 1 to prevent it from adversely affecting other electronic equipment.
must be shielded from electromagnetic waves generated by The case cover 6 has this shielding effect and is fixed to the case substrate 5 and the holding plate 3 in close contact with the conductive adhesive.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

この従来の衛星搭載用進行波管において、遅波回路は主
に電気的特性により形状及び寸法が決定され、又、コレ
クタは内部を極の温度を計算した熱的特性と、コレクタ
電極への給電端子の配置及び円板状保持板に固定するネ
ジの配置等により寸法が決められる。衛星搭載用機器は
、高信頼性と共に/J’%型軽量が要求される。コレク
タ形状を小型による場合、2枚の台形状支持板4の間隙
を縮める必要があるが、遅波回路の寸法が既に決定され
、又、構造上遅波回路と台形支持板の間にケースカバー
を入れなければらならないので、台形状支持板はケース
カバーの外側に少し間隙をあけて配置する必要があり、
小型軽量化は制約されるという問題があった。
In this conventional traveling wave tube for use in satellites, the shape and dimensions of the slow wave circuit are determined mainly by electrical characteristics, and the collector has internal thermal characteristics calculated from the pole temperature and power supply to the collector electrode. The dimensions are determined by the arrangement of the terminals and the arrangement of screws fixed to the disc-shaped holding plate. Satellite onboard equipment is required to be highly reliable and /J'% lightweight. If the collector shape is small, it is necessary to reduce the gap between the two trapezoidal support plates 4, but the dimensions of the slow-wave circuit have already been determined, and due to the structure, a case cover must be inserted between the slow-wave circuit and the trapezoidal support plate. Therefore, the trapezoidal support plate must be placed on the outside of the case cover with a slight gap.
There was a problem in that miniaturization and weight reduction were restricted.

〔課題を解決するための手段〕[Means to solve the problem]

本発明の衛星搭載用進行波管は、輻、耐冷却コレクタ、
このコレクタを保持する円板状保持板および円板状保持
板をケース基板に支持、固定する台形状支持板を有し、
しがも台形状支持板がケースカバーの一部を構成してい
ることを特徴とする。
The traveling wave tube for use in a satellite according to the present invention has radiation, cooling-resistant collector,
It has a disc-shaped holding plate that holds the collector and a trapezoidal support plate that supports and fixes the disc-shaped holding plate to the case substrate,
It is characterized in that the trapezoidal support plate forms part of the case cover.

〔実施例〕〔Example〕

次に本発明について図面を参照して説明する。 Next, the present invention will be explained with reference to the drawings.

第1図(a)は本発明の一実施例の側面図、第1図(b
)は第1図(a)のB−B断面図である。マイクロ波が
電子と相互作用して増幅される遅波回路1と、相互作用
した電子を捕獲し、発生した熱を輻射により宇宙空間に
放散する輻射冷却コレクタ7と、遅波回路1の熱を伝導
により放散するケース基板8と、コレクタを保持する円
板状保持板9と、遅波回路1からの電磁波をシールドす
るケースカバー10と、保持板9とケース基板8とを支
持し、かつ、ケースカバーを兼ねる台形状支持板11と
により構成されている。すなわち、本実施例ではケース
カバー10は台形状支持板11に接続固着され、ケース
カバー10の上部は円板状保持板9まで伸びて電磁波を
シールドしている。
FIG. 1(a) is a side view of one embodiment of the present invention, and FIG. 1(b) is a side view of one embodiment of the present invention.
) is a sectional view taken along line BB in FIG. 1(a). A slow wave circuit 1 in which microwaves interact with electrons and are amplified; a radiation cooling collector 7 that captures the interacting electrons and radiates the generated heat into space; A case substrate 8 that dissipates through conduction, a disc-shaped holding plate 9 that holds the collector, a case cover 10 that shields electromagnetic waves from the slow wave circuit 1, and supports the holding plate 9 and the case substrate 8, and It is composed of a trapezoidal support plate 11 which also serves as a case cover. That is, in this embodiment, the case cover 10 is connected and fixed to the trapezoidal support plate 11, and the upper part of the case cover 10 extends to the disk-shaped holding plate 9 to shield electromagnetic waves.

このような構造にすることにより、2枚の台形状支持板
11は遅波回路1に接近した位置に固定できる。このた
め、コレクタ7の寸法を熱的及び電気的特性により最適
寸法にでき、更に円板状保持板9台形状支持板およびケ
ース基板も小さくできる。
With this structure, the two trapezoidal support plates 11 can be fixed at positions close to the slow wave circuit 1. Therefore, the dimensions of the collector 7 can be optimized depending on the thermal and electrical characteristics, and the disk-shaped holding plate 9, the trapezoidal support plate, and the case substrate can also be made smaller.

〔発明の効果〕〔Effect of the invention〕

以上説明したように本発明は、台形状支持板がケースカ
バーを兼ねる構造としたため、台形状支持板を遅波回路
に接近した位置に固定でき、進行波管のコレクタ及びそ
の付近の寸法が構造的制約を受けず、電気的、熱的2機
械的に最適寸法に設定でき小型軽量化ができるという効
果を有する。
As explained above, since the present invention has a structure in which the trapezoidal support plate also serves as a case cover, the trapezoidal support plate can be fixed at a position close to the slow wave circuit, and the dimensions of the collector of the traveling wave tube and the vicinity thereof can be reduced. It has the advantage that it can be set to the optimum dimensions electrically, thermally, and mechanically without being subject to physical constraints, and can be made smaller and lighter.

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

第1図(a)は本発明の一実施例の側面図、第1図(b
)は第1図(a)のB−B断面図、第2図(a>は従来
例の側面図、第2図(b)は第2図(a)のA−A断面
図である。 1・・・遅波回路、2.7・・・輻射冷却コレクタ、3
.9・・・円板状保持板、4・・・台形状支持板、5゜
8・・・ケース基板、6・・・従来のケースカバー 1
0・・・本発明のケースカバー、11・・・本発明の台
形状支持板。 第1図 7 :輻阜nガψ]I、タタ
FIG. 1(a) is a side view of one embodiment of the present invention, and FIG. 1(b) is a side view of one embodiment of the present invention.
) is a sectional view taken along line BB in FIG. 1(a), FIG. 2(a) is a side view of the conventional example, and FIG. 2(b) is a sectional view taken along line AA in FIG. 2(a). 1...Slow wave circuit, 2.7...Radiation cooling collector, 3
.. 9... Disc-shaped holding plate, 4... Trapezoidal support plate, 5° 8... Case substrate, 6... Conventional case cover 1
0... Case cover of the present invention, 11... Trapezoidal support plate of the present invention. Figure 1 7: 輻阜ngaψ]I, Tata

Claims (1)

【特許請求の範囲】[Claims] 輻射冷却コレクタ、このコレクタを保持する円板状保持
板、この保持板をケース基板に支持する台形状支持板、
遅波回路、ケース基板とケースカバーを有する衛星搭載
用進行波管において、前記台形状支持板がケースカバー
の一部を構成することを特徴とする衛星搭載用進行波管
a radiation-cooled collector, a disk-shaped holding plate that holds this collector, a trapezoidal support plate that supports this holding plate on a case substrate,
1. A traveling wave tube for use in a satellite having a slow wave circuit, a case substrate, and a case cover, wherein the trapezoidal support plate constitutes a part of the case cover.
JP2222925A 1990-08-24 1990-08-24 Traveling wave tube for satellite Expired - Lifetime JP2679379B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2222925A JP2679379B2 (en) 1990-08-24 1990-08-24 Traveling wave tube for satellite

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2222925A JP2679379B2 (en) 1990-08-24 1990-08-24 Traveling wave tube for satellite

Publications (2)

Publication Number Publication Date
JPH04106841A true JPH04106841A (en) 1992-04-08
JP2679379B2 JP2679379B2 (en) 1997-11-19

Family

ID=16790013

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2222925A Expired - Lifetime JP2679379B2 (en) 1990-08-24 1990-08-24 Traveling wave tube for satellite

Country Status (1)

Country Link
JP (1) JP2679379B2 (en)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH025859U (en) * 1988-06-27 1990-01-16

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH025859U (en) * 1988-06-27 1990-01-16

Also Published As

Publication number Publication date
JP2679379B2 (en) 1997-11-19

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