JPS6212639B2 - - Google Patents

Info

Publication number
JPS6212639B2
JPS6212639B2 JP7917076A JP7917076A JPS6212639B2 JP S6212639 B2 JPS6212639 B2 JP S6212639B2 JP 7917076 A JP7917076 A JP 7917076A JP 7917076 A JP7917076 A JP 7917076A JP S6212639 B2 JPS6212639 B2 JP S6212639B2
Authority
JP
Japan
Prior art keywords
magnetron
heating chamber
transformer
fan
cooling
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
JP7917076A
Other languages
Japanese (ja)
Other versions
JPS534240A (en
Inventor
Shigeki Ueda
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.)
Panasonic Holdings Corp
Original Assignee
Matsushita Electric Industrial Co Ltd
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 Matsushita Electric Industrial Co Ltd filed Critical Matsushita Electric Industrial Co Ltd
Priority to JP7917076A priority Critical patent/JPS534240A/en
Publication of JPS534240A publication Critical patent/JPS534240A/en
Publication of JPS6212639B2 publication Critical patent/JPS6212639B2/ja
Granted legal-status Critical Current

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  • Constitution Of High-Frequency Heating (AREA)
  • Electric Ovens (AREA)

Description

【発明の詳細な説明】 本発明は冷却すべき電気部品をすべて一側室に
集め、冷却空間を限定すると共に、プロペラフア
ンを用いて効率の良い冷却を行おうとするもので
ある。
DETAILED DESCRIPTION OF THE INVENTION The present invention attempts to collect all the electrical components to be cooled in one side chamber, limit the cooling space, and perform efficient cooling using a propeller fan.

従来、高周波加熱装置、一般に電子レンジにお
ける冷却構造は、発熱量の最も大きいマグネトロ
ンを主体的に冷却するため、これを冷却フアンの
直後に配し、効率の良い吹きつけ冷却を行い、残
るトランスや操作回路は冷却フアンの吹い込み冷
却に頼るものが多かつた。すなわち、トランス等
の部品とマグネトロンと冷却フアンが直列に配さ
れてきたわけである。かかる構成の長所はマグネ
トロンの冷却が良好なことであるが、反面吹い込
み冷却は途中のロスが多く吸い込み冷却される部
品の冷却効果は前者に比べはるかに劣り、そのた
めにトランスなどではかなり太い径を有するコイ
ルを使用して温度上昇を抑えるのが常であつた。
かかる点に注目し、本発明はすべての部品を効率
の良い吹きつけ冷却できる構造を実現するもので
ある。以下図面に従つて本発明の構成を説明す
る。
Conventionally, the cooling structure of high-frequency heating devices, generally microwave ovens, mainly cools the magnetron, which generates the largest amount of heat, so it is placed immediately after the cooling fan to perform efficient blow cooling, and the remaining transformer and Many of the operating circuits relied on blow-cooling from a cooling fan. In other words, components such as transformers, magnetrons, and cooling fans have been arranged in series. The advantage of this configuration is that the magnetron can be cooled well, but on the other hand, blow cooling has a lot of loss during the process, and the cooling effect of the parts that are cooled by suction is much inferior to the former, and for this reason, transformers etc. have to have a fairly large diameter. It was customary to suppress the temperature rise by using a coil with a
Focusing on this point, the present invention realizes a structure in which all parts can be efficiently blown and cooled. The configuration of the present invention will be explained below with reference to the drawings.

第1図は本発明の一実施例を示す電子レンジの
正面斜視図、第2図は同側面内部構造、第3図は
同上面内部構造図、第4図は同裏面図である。1
はドア、2は加熱室、3は操作パネルで、本実施
例はいわゆる横型レンジである。外装4を外すと
内部は第2図および第3図に示すように、操作パ
ネルの後方、加熱室の右側面にすべての電気部品
が集中して配されている。5はマグネトロン、6
はトランス、7はコンデンサ、8はプロペラフア
ン、9はその駆動モータ、10はタイマー、11
はオーブンランプ、12はラツチスイツチ、13
はドアスイツチ、14はヒユーズボツクス、15
はダイオードである。このようにすべての電気部
品を右側面に集めると共に、加熱室上壁16を第
3図に示すように外装のそばまで延長し、この機
械室空間を仕切ることでプロペラフアン8の効果
が発揮される。この点を説明する。プロペラフア
ンの特性は大きな風量は得られるが、高い風圧は
得られないので、空気抵抗の大きな部品は冷却し
にくく、反面抵抗の小さい部品はシロツコフアン
に比べ同能力のモータで数倍の風量を送り込むこ
とができる。第2図の例ではマグネトロンの冷却
フインへは風は入りにくく抵抗の少ないプロペラ
フアンの外周方向に風が逃げてしまいやすい。そ
こで加熱室後壁17と上壁16の延長部と外装4
と底面シヤーシ18と加熱室右側壁19とで、プ
ロペラフアン8と冷却されるべき部品とを密室内
に収納することで、風がプロペラフアンの外周方
向へ逃げることを防ぎ、吸気孔20から吸気され
た外気を被冷却部品に直進させうる。本実施例で
は最も空気抵抗の大きいマグネトロンを効果的に
冷却するため、プロペラフアンとマグネトロンを
対向位置させると共に、その距離を10〜15mm程
度まで接近させ、かつその回転中心C―C軸をマ
グネトロンの冷却フインからはずし、最も風速の
大きなプロペラフアンの外周部を冷却フインと対
向させている。これにより大きな風量の得られる
大径のプロペラフアンが採用できる。さらにプロ
ペラフアンを上向きに持ち上げるように取付板2
1を構成すれば、より一層マグネトロンの冷却効
果は高まる。22はマグネトロンの排気を加熱室
内へ導くガイドで、本例ではランプ11のカバー
をも兼ねている。ガイド22はコの字形をしてお
り、垂直面はマグネトロンの排気の流れを転換
し、加熱室内へ向わせる。上方の水平面は上壁1
6に取り付けられるためのフランジである。下方
の水平面は三角形をしており、マグネトロンの排
気が電気部品を配した機械室空間に漏れないよ
う、マグネトロンの排気の通風路と機械室空間と
を遮蔽する。このガイド22の上壁16への取付
部は、第3図に示すように傾斜した上壁16のフ
ランジに押しあてられ、1本のビスで固定されて
いる。三角形に切り欠いた上壁16の一角は、ガ
イド22の回り止めにもなる。
FIG. 1 is a front perspective view of a microwave oven showing an embodiment of the present invention, FIG. 2 is a side view of the internal structure, FIG. 3 is a top view of the internal structure, and FIG. 4 is a back view of the microwave oven. 1
2 is a door, 2 is a heating chamber, and 3 is an operation panel, which is a so-called horizontal range in this embodiment. When the exterior 4 is removed, all the electrical components are concentrated on the rear of the operation panel and on the right side of the heating chamber, as shown in FIGS. 2 and 3. 5 is magnetron, 6
is a transformer, 7 is a capacitor, 8 is a propeller fan, 9 is its drive motor, 10 is a timer, 11
is an oven lamp, 12 is a latch switch, 13 is
is the door switch, 14 is the fuse box, 15 is
is a diode. In this way, all the electrical parts are gathered on the right side, and the upper wall 16 of the heating chamber is extended to the side of the exterior as shown in Fig. 3, and this machine room space is partitioned, so that the effect of the propeller fan 8 can be exerted. Ru. This point will be explained. The characteristics of a propeller fan are that it can obtain a large air volume, but it cannot obtain a high wind pressure, so parts with high air resistance are difficult to cool.On the other hand, parts with low resistance can be sent several times the air volume with a motor of the same capacity compared to a Sirotskov fan. be able to. In the example shown in Fig. 2, it is difficult for wind to enter the cooling fins of the magnetron, and the wind tends to escape toward the outer circumference of the propeller fan, where there is less resistance. Therefore, the extension of the heating chamber rear wall 17 and the upper wall 16 and the exterior 4
The bottom chassis 18 and the right side wall 19 of the heating chamber house the propeller fan 8 and the parts to be cooled in a closed chamber, thereby preventing the wind from escaping toward the outer circumference of the propeller fan and allowing air to be taken in through the intake hole 20. The cooled outside air can be directed straight to the parts to be cooled. In this embodiment, in order to effectively cool the magnetron, which has the largest air resistance, the propeller fan and magnetron are positioned facing each other, and the distance between them is brought close to each other by about 10 to 15 mm, and the rotation center C-C axis is aligned with the magnetron. It is removed from the cooling fin, and the outer periphery of the propeller fan, which has the highest wind speed, is placed opposite the cooling fin. This allows the use of a large-diameter propeller fan that provides a large amount of air. Furthermore, move the mounting plate 2 so as to lift the propeller fan upward.
1, the cooling effect of the magnetron is further enhanced. A guide 22 guides the exhaust gas from the magnetron into the heating chamber, and also serves as a cover for the lamp 11 in this example. The guide 22 is U-shaped with a vertical surface that diverts the flow of the magnetron's exhaust gas and directs it into the heating chamber. The upper horizontal plane is the upper wall 1
This is a flange for attaching to 6. The lower horizontal plane has a triangular shape and shields the magnetron exhaust ventilation path and the machine room space so that the magnetron's exhaust gas does not leak into the machine room space where electrical components are arranged. The attachment portion of the guide 22 to the upper wall 16 is pressed against the flange of the inclined upper wall 16, as shown in FIG. 3, and is fixed with one screw. One corner of the triangularly cut upper wall 16 also serves as a stop for the guide 22 to rotate.

次にトランス6その他の部品の冷却構造につい
て説明する。吸気口20より吸気された外気は当
然トランス6やコンデンサ7にも吹きつけられ
る。そして加熱室の右壁のほぼ直下に位置する立
壁23(底面シヤーシ18の一部)に設けた小孔
より機体外へ排気される。従つてこれらの部品の
冷却抵抗は極めて小さく、そのためにトランス
6、タイマー10のモータコイル、冷却フアンモ
ータ9のコイル等は従来の冷却に比べはるかに良
好で、線径の細いものが使用でき、コストダウン
をはかれる。なお、25は加熱室過昇温度防止装
置で、加熱室壁に取付けられるが、図示のように
フアンの吹出し近傍、すなわちマグネトロン近傍
の加熱室壁面に設けることで良好に冷却されるた
め、その設定温度を低くしても正常時の誤動作が
ない。したがつて、異常の検知をすみやかに行う
ことができ、他の部品が2次的に破壊されるのを
防止できる。またマグネトロンの異常過熱や加熱
室内の火災の検知以外にプロペラフアンの故障に
よる停止までも検出しうる。
Next, a cooling structure for the transformer 6 and other parts will be explained. The outside air taken in through the intake port 20 is naturally blown onto the transformer 6 and the condenser 7 as well. The air is then exhausted to the outside of the aircraft through a small hole provided in the standing wall 23 (a part of the bottom chassis 18) located almost directly below the right wall of the heating chamber. Therefore, the cooling resistance of these parts is extremely small, and therefore the transformer 6, the motor coil of the timer 10, the coil of the cooling fan motor 9, etc. are much better than conventional cooling, and can use wires with a thin diameter. Cost reduction is possible. Note that 25 is a heating chamber excessive temperature rise prevention device, which is attached to the heating chamber wall, but as shown in the figure, it is installed near the blowout of the fan, that is, on the heating chamber wall near the magnetron, to ensure good cooling. There is no malfunction during normal operation even at low temperatures. Therefore, an abnormality can be detected quickly and other parts can be prevented from being destroyed secondary. In addition to detecting abnormal overheating of the magnetron and fire in the heating chamber, it can also detect stoppages due to propeller fan failure.

なおラツチスイツチ12は2枚の絶縁シート2
6(第2図)でサンドイツチ状にはさみ込まれて
固定されているが、これは端子部の絶縁以外にス
イツチのケースの割れを防止する効果もある。2
7は絶縁チユーブでダイオード15とコンデンサ
ケースとの絶縁をはかつている。ダイオードのア
ース端子28はコンデンサ7の取付板29に固定
され、コンデンサとダイオードを一つのユニツト
として扱える構成となつている。いずれの絶縁シ
ート、チユーブともこのあたりの雰囲気が低いた
め、高温による絶縁性能の劣化が少ない。また、
30はオーブンランプ11の光を調理表示灯31
に導くライトコンダクターであるが、これはその
透光性からアクリルで構成されることがほとんど
である。アクリルは熱変形しやすい樹脂である
が、これも本発明によれば何ら問題とならない。
The latch switch 12 is made of two insulation sheets 2.
6 (Fig. 2), which is sandwiched and fixed in a sandwich-like manner, which not only insulates the terminals but also prevents the switch case from cracking. 2
7 is an insulating tube which insulates the diode 15 and the capacitor case. The ground terminal 28 of the diode is fixed to the mounting plate 29 of the capacitor 7, so that the capacitor and diode can be treated as one unit. Because the atmosphere around both insulation sheets and tubes is low, there is little deterioration of insulation performance due to high temperatures. Also,
30 is a cooking indicator light 31 that converts the light of the oven lamp 11
This is a light conductor that guides the light, but it is mostly made of acrylic because of its translucency. Although acrylic is a resin that is easily deformed by heat, this does not pose any problem according to the present invention.

次に加熱室内へ導かれた換気風の排気構造につ
いて述べる。最近コスト面での有利さから風力で
駆動するスタラーフアンが汎用されるようになつ
たが、小孔32はこのような風力駆動スタラーを
考慮して、その駆動力を増すためにマグネトロン
の排気以外に、直接プロペラフアンから加熱室内
へ風を導き入れるものである。33はスタラーを
回した後、ドアののぞき窓34に換気風を吹きつ
けるスリツトである。スリツト33より加熱室内
に入つた風は排気ガイド35より本体外へ排出さ
れる。ここで排気ガイド35は吸気孔20と接近
して設けられ、本体が傾いて壁に押しあてられて
も吸気孔20に確実な吸気ギヤツプdを確保する
(第3図)。
Next, we will discuss the exhaust structure for ventilation air guided into the heating chamber. Recently, wind-driven stirrer fans have come into widespread use due to their cost advantages.In consideration of such wind-driven stirrers, the small hole 32 is designed to be equipped with a method other than magnetron exhaust to increase the driving force. , which introduces air directly into the heating chamber from the propeller fan. 33 is a slit that blows ventilation air into the peephole 34 of the door after turning the stirrer. Air entering the heating chamber through the slit 33 is discharged to the outside of the main body through the exhaust guide 35. Here, the exhaust guide 35 is provided close to the intake hole 20 to ensure a reliable intake gap d at the intake hole 20 even if the main body is tilted and pressed against a wall (FIG. 3).

最後に第1図および第3図によりドアまわりの
説明をする。36はハンドル、37はハンドルの
操作により上下動しラツチスイツチ12を調理開
始スイツチ38の操作と共に動作させるキー、3
9はドアスイツチピン、40はそのピンの動きを
拡大するテコ、41はアーム、42はアームの動
きを制御するアームピンである。ドアスイツチ1
3およびヒユーズボツクス14についても、通常
導波管43の近傍は温度上昇が著しく、高い許容
温度を備えた高価な絶縁材料を用いなければこの
ような位置に部品を配することは困難であるが、
本発明によれば、かかる箇所についても何ら特別
な配慮をする必要なく、安価な材料で構成したド
アスイツチやヒユーズボツクスが使用できる。な
お44は電源コードである。
Finally, the door and its surroundings will be explained with reference to FIGS. 1 and 3. 36 is a handle; 37 is a key that moves up and down when the handle is operated and operates the latch switch 12 together with the operation of the cooking start switch 38;
9 is a door switch pin, 40 is a lever that magnifies the movement of the pin, 41 is an arm, and 42 is an arm pin that controls the movement of the arm. door switch 1
3 and the fuse box 14, the temperature usually rises significantly in the vicinity of the waveguide 43, and it is difficult to place components in such a position without using an expensive insulating material with a high allowable temperature. ,
According to the present invention, door switches and fuse boxes made of inexpensive materials can be used without any special consideration for such locations. Note that 44 is a power cord.

以上述べたように本発明によれば冷却すべき空
間が限定され、低圧大風量のプロペラフアンがそ
の持味を存分に発揮し、良好な冷却構造が実現で
きる。また電気部品のすべてが一側面に集中して
いるため、リード線が短くでき作業性の良い安価
な配線が可能である。また当然のことながらサー
ビス性もすこぶる良好である。
As described above, according to the present invention, the space to be cooled is limited, the propeller fan with low pressure and large air volume can fully demonstrate its characteristics, and a good cooling structure can be realized. In addition, since all the electrical parts are concentrated on one side, the lead wires can be shortened, allowing for easy and inexpensive wiring. As a matter of course, the service quality is also very good.

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

第1図は本発明の一実施例を示す高周波加熱装
置の斜視図、第2図は同側面内部を示す斜視図、
第3図は同上面図、第4図は同裏面斜視図であ
る。 5……マグネトロン、6……トランス、8……
プロペラフアン、16……加熱室上壁延長部。
FIG. 1 is a perspective view of a high-frequency heating device showing an embodiment of the present invention, FIG. 2 is a perspective view showing the inside of the same side,
FIG. 3 is a top view of the same, and FIG. 4 is a rear perspective view of the same. 5... Magnetron, 6... Transformer, 8...
Propeller fan, 16...Heating chamber upper wall extension.

Claims (1)

【特許請求の範囲】[Claims] 1 被加熱物に高周波を照射する加熱室と、高周
波を発生するマグネトロンと、このマグネトロン
に高電圧を供給するトランスと、プロペラフアン
を有する冷却フアンと、機体外かくに設けた吸気
孔および第1、第2の排気孔と、過昇温度防止装
置とより成り、前記マグネトロンおよび前記トラ
ンスを加熱室の一壁面に集中して配置し、前記フ
アンの回転軸を前記マグネトロンの冷却フインか
ら外し、プロペラフアンの外周部と冷却フインと
を対向させ、前記吸気孔より吸入した外気を前記
マグネトロンに吹きつけて冷却し、その排気を前
記加熱室内に導くと共に、前記第1の排気孔より
機体外に排出し、かつ前記トランスにも前記吸気
孔より吸入した外気を吹きつけて冷却し、その排
気を前記トランスの近傍に設けた第2の排気孔よ
り機体外に排出し、さらに前記冷却フインの吹出
し近傍の加熱室壁面に前記温度過昇防止装置を設
けた高周波加熱装置。
1. A heating chamber that irradiates high frequency waves to the object to be heated, a magnetron that generates high frequency waves, a transformer that supplies high voltage to this magnetron, a cooling fan that has a propeller fan, and an intake hole and a first , a second exhaust hole, and an excessive temperature rise prevention device, the magnetron and the transformer are arranged centrally on one wall of the heating chamber, the rotating shaft of the fan is removed from the cooling fin of the magnetron, and the propeller is The outer periphery of the fan and the cooling fin are arranged to face each other, and the outside air taken in through the intake hole is blown onto the magnetron to cool it, and the exhaust gas is guided into the heating chamber and discharged to the outside of the aircraft through the first exhaust hole. In addition, the transformer is also cooled by blowing outside air taken in through the intake hole, and the exhaust air is discharged to the outside of the aircraft through a second exhaust hole provided near the transformer. A high-frequency heating device comprising the above temperature rise prevention device on the wall surface of the heating chamber.
JP7917076A 1976-07-02 1976-07-02 High-frequency heater Granted JPS534240A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7917076A JPS534240A (en) 1976-07-02 1976-07-02 High-frequency heater

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7917076A JPS534240A (en) 1976-07-02 1976-07-02 High-frequency heater

Publications (2)

Publication Number Publication Date
JPS534240A JPS534240A (en) 1978-01-14
JPS6212639B2 true JPS6212639B2 (en) 1987-03-19

Family

ID=13682489

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7917076A Granted JPS534240A (en) 1976-07-02 1976-07-02 High-frequency heater

Country Status (1)

Country Link
JP (1) JPS534240A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6026077A (en) * 1983-07-21 1985-02-08 Nippon Hikari Fiber Kk Self-adhesive tape

Also Published As

Publication number Publication date
JPS534240A (en) 1978-01-14

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