JPH10205493A - Blower impeller and manufacture thereof - Google Patents

Blower impeller and manufacture thereof

Info

Publication number
JPH10205493A
JPH10205493A JP991497A JP991497A JPH10205493A JP H10205493 A JPH10205493 A JP H10205493A JP 991497 A JP991497 A JP 991497A JP 991497 A JP991497 A JP 991497A JP H10205493 A JPH10205493 A JP H10205493A
Authority
JP
Japan
Prior art keywords
blower impeller
impeller
hollow
blower
airfoil
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
JP991497A
Other languages
Japanese (ja)
Other versions
JP3752762B2 (en
Inventor
Hironao Numamoto
浩直 沼本
Sadami Masahara
定巳 正原
Masaharu Ota
雅春 太田
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 JP00991497A priority Critical patent/JP3752762B2/en
Publication of JPH10205493A publication Critical patent/JPH10205493A/en
Application granted granted Critical
Publication of JP3752762B2 publication Critical patent/JP3752762B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Abstract

PROBLEM TO BE SOLVED: To provide a blower impeller made of a metal to take a recycle, saving of resources, and coping with a PL method into consideration and have high performance and to provide manufacture thereof. SOLUTION: A blower impeller 2 is formed of a magnesium alloy, a hollow layer is formed at the internal part of a structure, and a hollow part is pressurized and held at a pressure higher than an atmospheric pressure. Thus, the blower impeller is light in weight and excellent in recycle properties. A manufacturing method is such that after the blower impeller is divided into constituting elements and molded, a joining portion is adhered or brazed. When a hollow part is pressurized and held, after the constituting elements of the blower impeller are joined together through bonding or brazing, a pin hole part is formed in a part thereof, and gas is injected through the pin hole. Thereafter, by closing the pin hole part, the hollow part of a blade type impeller forms a structure which is held at a pressure higher than an atmospheric pressure. This means improves workability of a work to bring the device into a hollow state and pressurize an internal part.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、低騒音化に効果の
ある厚さを有する翼型羽根を備えた送風機羽根車に関す
るものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a blower impeller provided with an airfoil blade having a thickness effective for reducing noise.

【0002】[0002]

【従来の技術】翼型羽根を備えた送風機羽根車は、昭和
30年代の空気調和機の室外機本体中に大型プロペラフ
ァンをして使用されていた時には金属製のものが使用さ
れていた。しかし、時代の流れとともにプラスチック製
に置き換わっていった。その理由は低騒音で大風量の得
られる送風機羽根車として、プラスチック製が大量生産
に適していたためである。
2. Description of the Related Art A blower impeller equipped with airfoil blades was made of metal when a large propeller fan was used in an outdoor unit of an air conditioner in the 1950s. However, with the passage of time, it was replaced by plastic. The reason is that plastic is suitable for mass production as a blower impeller that can obtain a large air volume with low noise.

【0003】[0003]

【発明が解決しようとする課題】しかしながら、近年家
電製品のリサイクル化が望まれる中ではプラスチック製
部品よりも金属製部品のほうが再資源化が容易であり、
適した材料と認知されている。したがって、昔のような
金属鋼板製に戻せばよいのであるが、近年の技術進歩に
よって高性能化した送風機羽根車を金属鋼板で同様な性
能レベルに達成するのは非常に困難であった。
However, in recent years, while recycling of home appliances is desired, metal parts are easier to recycle than plastic parts.
It is recognized as a suitable material. Therefore, it is only necessary to return to the metal steel plate as in the past, but it has been very difficult to achieve the same performance level with the metal steel plate for the fan impeller, which has been improved in performance in recent years.

【0004】また、空気調和機の室外機はPL法対応と
して放火への対策を講じる目的で難燃化も要望されてい
る。
[0004] In addition, the outdoor unit of the air conditioner is required to be flame retardant in order to take measures against arson in compliance with the PL method.

【0005】本発明は、上記従来の問題点を鑑みて、リ
サイクル、省資源化、PL法対応を考慮し、高性能な金
属製送風機羽根車とその製造方法を提供することを目的
とする。
SUMMARY OF THE INVENTION In view of the above-mentioned conventional problems, it is an object of the present invention to provide a high-performance metal blower impeller and a method of manufacturing the same in consideration of recycling, resource saving, and compliance with the PL method.

【0006】[0006]

【課題を解決するための手段】上記課題を解決するため
に本発明は、マグネシウム系合金からなる材質を使用す
ることによってリサイクル化を容易にし、送風機羽根車
の難燃化も実現できる。また、構造体内部を中空化する
ことによって省資源化が可能となる。また、翼型羽根の
中空部を大気圧以上に保持させることによって、外力に
よる変形に対して充分な反発性を有することでさらに薄
肉化が可能となる。
According to the present invention, in order to solve the above-mentioned problems, recycling is facilitated by using a material made of a magnesium-based alloy, and the fan impeller can be made flame-retardant. In addition, it is possible to save resources by hollowing the inside of the structure. In addition, by maintaining the hollow portion of the airfoil at a pressure higher than the atmospheric pressure, the airfoil has sufficient resilience against deformation due to external force, thereby enabling further reduction in thickness.

【0007】製造方法としては、送風機羽根車を構成要
素に分割して成形した後、接合することで中空化を図
る。直接中空化を行うと内部の中空状態にバラツキを生
じやすく、羽根車の回転バランスを補正することが困難
となる。構成要素に分割することは工数アップになる
が、品質の安定を考えた量産化には好ましい方法であ
る。また、中空部を加圧状態にする場合には構成要素に
分割された成形品を接合した後、一部にピンホール部を
設け、前記ピンホール部からガスを注入し、その後前記
ピンホール部を塞ぐ。接合と中空部の加圧を同時に行う
のであれば、接合部が充分な強度を有するまで固定保持
しなければならない。ピンホール部であれば加圧後の作
業が容易である。
[0007] As a manufacturing method, a blower impeller is divided into constituent elements, formed, and then joined to hollow. If hollowing is performed directly, the hollow state of the inner portion tends to vary, making it difficult to correct the rotational balance of the impeller. Dividing into components increases the number of man-hours, but is a preferable method for mass production considering stability of quality. Further, when the hollow portion is to be pressurized, after joining the molded product divided into the constituent elements, a pinhole portion is provided in a part, gas is injected from the pinhole portion, and then the pinhole portion is provided. Close up. If the joining and the pressurization of the hollow portion are performed at the same time, the joint must be fixedly held until the joint has sufficient strength. If it is a pinhole portion, the operation after pressurization is easy.

【0008】[0008]

【発明の実施の形態】上記の課題を解決するための請求
項1記載の発明は、マグネシウム系合金からなる送風機
羽根車である。そしてこの構成によれば金属合金の中で
も軽量なものが得られる。
DESCRIPTION OF THE PREFERRED EMBODIMENTS The invention according to claim 1 for solving the above-mentioned problems is a blower impeller made of a magnesium-based alloy. According to this configuration, a lightweight metal alloy can be obtained.

【0009】請求項2記載の発明は構造体内部に中空層
を有することで、さらに軽量化と低コスト化が可能であ
る。
According to the second aspect of the present invention, since the structure has the hollow layer inside, the weight and cost can be further reduced.

【0010】請求項3記載の発明は、翼型羽根の中空部
が大気圧以上に加圧保持することで、軽量化を追求して
薄肉化を進めた場合に信頼性で問題となる外力による変
形に対して充分な反発性を有することができる。
According to the third aspect of the present invention, since the hollow portion of the airfoil blade is kept at a pressure higher than the atmospheric pressure, an external force which becomes a problem in reliability when the thickness is reduced in pursuit of weight reduction is pursued. It can have sufficient resilience to deformation.

【0011】また、請求項4記載の発明は、送風機羽根
車を構成要素に分割して成形した後、接合部位を接着あ
るいはロウ付けで行う送風機羽根車の製造方法であり、
内部中空化を均一に実現し易くしたものである。
[0011] The invention according to claim 4 is a method for manufacturing a fan impeller in which a blower impeller is divided into components and molded, and a joining portion is bonded or brazed.
This makes it easy to achieve uniform hollowing inside.

【0012】また、請求項5記載の発明は、送風機羽根
車を構成要素に分割して成形した後、接合部位を接着あ
るいはロウ付けで行った後、一部にピンホール部を設
け、前記ピンホール部からガスを注入し、その後前記ピ
ンホール部を塞ぐことによって翼型羽根の中空部が大気
圧以上に保持された構造体を得る送風機羽根車の製造方
法であり、内部中空への加圧を実現し易くしたものであ
る。
Further, according to the present invention, after the blower impeller is divided into components and formed, the joint portion is bonded or brazed, and a pinhole portion is provided in a part, and the pinhole is provided. This is a method for manufacturing a blower impeller in which a gas is injected from a hole portion, and thereafter, the pinhole portion is closed to obtain a structure in which the hollow portion of the airfoil is held at a pressure higher than the atmospheric pressure. Is realized easily.

【0013】[0013]

【実施例】以下、本発明の実施例について図面を参照し
て説明する。
Embodiments of the present invention will be described below with reference to the drawings.

【0014】図1において室外機本体1の中心部に送風
機羽根車2は位置し、ファンモータ3のボルトにナット
4で固定され、熱交換機(図示せず)に対して大気を供
給して熱交換性能向上に貢献している。
In FIG. 1, a blower impeller 2 is located at the center of the outdoor unit main body 1 and is fixed to a bolt of a fan motor 3 with a nut 4 to supply air to a heat exchanger (not shown) to generate heat. It contributes to the exchange performance improvement.

【0015】(実施例1)マグネシウム系合金(90M
g−10Al)のチップ(長軸が5〜6mm程度の米粒
状)を使用してチクソモールディング法によって外寸3
50mmφの送風機羽根車を成形した。チクソモールデ
ィング法とはシリンダー内でチップを凝固点〜融点の温
度まで加熱し、液相と固相が共存した半溶融状態にして
金型に射出注入する成形方法である。実施例では550
〜580℃まで加熱した。マグネシウム系合金(90M
g−10Al)は比重が1.82程度で金属としては低
比重な材料である。また、コア部は金属化によって機械
的強度の向上が図れるので設計肉厚1mmとした。
(Example 1) Magnesium alloy (90M
g-10Al) chips (rice grains having a major axis of about 5 to 6 mm) by the thixomolding method.
A blower impeller of 50 mmφ was formed. The thixomolding method is a molding method in which a chip is heated to a temperature from a freezing point to a melting point in a cylinder to be in a semi-molten state in which a liquid phase and a solid phase coexist and injected into a mold. 550 in the embodiment
Heated to 5580 ° C. Magnesium alloy (90M
g-10Al) is a material having a specific gravity of about 1.82 and a low specific gravity as a metal. The core portion was designed to have a designed thickness of 1 mm because metallization can improve mechanical strength.

【0016】(比較例1)難燃性ポリプロピレンを使用
して外寸350mmφの送風機羽根車を成形した。比重
は1.2であり、コア部は設計肉厚2mmとした。
Comparative Example 1 A blower impeller having an outer dimension of 350 mmφ was formed using flame-retardant polypropylene. The specific gravity was 1.2, and the core portion had a designed thickness of 2 mm.

【0017】実施例1と比較例1を比べると、比重は金
属製のほうがプラスチック製に比べて重いため、形状の
変わらない翼型羽根は重くなるが、コア部は金属化によ
って機械的強度が向上分だけ薄肉化したので差はなかっ
た。したがって、全体では翼型羽根分だけ金属製のほう
が重くなった。しかし、プラスチック製には環境負荷の
大きな難燃剤が使用されており、リサイクル、環境影響
を考慮すると実施例のほうがはるかに適した部品と言え
る。
When comparing Example 1 with Comparative Example 1, the specific gravity of metal is heavier than that of plastic. There was no difference because the thickness was reduced by the improvement. Therefore, the metal was heavier by the airfoil blades as a whole. However, a flame retardant with a large environmental load is used for plastics, and it can be said that the examples are far more suitable parts in consideration of recycling and environmental impact.

【0018】(実施例2)実施例1と同じ材料を使用
し、翼型羽根が中空化できるように分割してチクソモー
ルディング法によって外寸350mmφの送風機羽根車
を成形した。その後、接合すべき箇所をシアノアクリレ
ート系の接着剤で固定した。図2に接合箇所(点線部お
よび翼端面)がわかるように送風機羽根車の斜視図を示
した。この時、翼型羽根の設計肉厚は1.5mmとし、
コア部は肉厚1mmとした。
Example 2 The same material as in Example 1 was used, and a blade impeller having an outer size of 350 mmφ was formed by thixomolding by dividing the airfoil blade so as to be hollow. Thereafter, the portion to be joined was fixed with a cyanoacrylate adhesive. FIG. 2 is a perspective view of the blower impeller so that the joints (dotted line portions and blade end surfaces) can be seen. At this time, the design thickness of the airfoil blade is 1.5 mm,
The core had a thickness of 1 mm.

【0019】実施例2と比較例1を比べると、翼型羽根
を中空化し、肉厚を1.5mmとすることで全体の重量
も実施例2のほうが軽量化された。
Comparing Example 2 with Comparative Example 1, the overall weight was reduced in Example 2 by hollowing out the airfoil blade and setting the thickness to 1.5 mm.

【0020】実施例2では、短時間で充分な接着強度の
得られるシアノアクリレート系接着剤で接合箇所を固定
したが、その他エポキシ系、酢酸ビニル系のものでもよ
い。また、ロウ付けによって固定することも可能であっ
た。
In the second embodiment, the bonding portion is fixed with a cyanoacrylate-based adhesive capable of obtaining a sufficient adhesive strength in a short time, but other epoxy-based or vinyl acetate-based adhesives may be used. It was also possible to fix by brazing.

【0021】(実施例3)実施例1と同じ材料を使用
し、翼型羽根が中空化できるように分割してチクソモー
ルディング法によって外寸350mmφの送風機羽根車
を成形した。その後、翼型羽根の接合箇所は一部をピン
ホール部(ハブ付近)として残し、その他はシアノアク
リレート系の接着剤で固定した。この時、翼型羽根の設
計肉厚は0.5mmとし、コア部は設計肉厚1mmとし
た。次に、3ヶ所のピンホール部から弾性材を介して
1.5kg/cm2 に内圧がなるように窒素ガスを注入
した後、弾性材が実用に際して外れないよう接着剤で補
強した。
(Example 3) The same material as in Example 1 was used, and an airfoil impeller having an outer dimension of 350 mmφ was formed by a thixomolding method by dividing the airfoil blade so as to be hollow. Thereafter, a part of the joint of the airfoil was left as a pinhole (near the hub), and the other was fixed with a cyanoacrylate-based adhesive. At this time, the design thickness of the airfoil blade was 0.5 mm, and the design thickness of the core portion was 1 mm. Next, nitrogen gas was injected from the three pinholes via an elastic material so that the internal pressure became 1.5 kg / cm 2 , and the elastic material was reinforced with an adhesive so as not to come off during practical use.

【0022】実施例3と比較例1を比べると、翼型羽根
を中空化し、肉厚も0.5mmとすることで全体の重量
も実施例3のほうがはるかに軽量化された。
Comparing Example 3 with Comparative Example 1, the overall weight was much lighter in Example 3 by making the airfoil blade hollow and making the wall thickness 0.5 mm.

【0023】また、実施例3では中空部の内圧が1.5
kg/cm2 になるように設定したが、内圧は翼型羽根
部の設計肉厚と相関させる必要があった。すなわち、設
計肉厚が薄くなるにしたがって内圧は高めにする。この
効果は大気圧以上であれば有効であるが、あまり高くす
ると内圧バラツキが大きく、作業性も低下してくるので
2kg/cm2 以下にすることが好ましい。注入に使用
するガスは、実施例では窒素ガスを使用したがこれに限
定されるわけではなく、その他乾燥空気、二酸化炭素等
も使用できた。
In the third embodiment, the internal pressure of the hollow portion is 1.5
The pressure was set to be kg / cm 2 , but the internal pressure had to be correlated with the design thickness of the airfoil blade portion. That is, the internal pressure is made higher as the design thickness becomes thinner. This effect is effective as long as more than the atmospheric pressure, large pressure variation when too high, it is preferable to 2 kg / cm 2 or less because workability come reduced. As the gas used for injection, nitrogen gas was used in the examples, but the gas is not limited to nitrogen gas, and dry air, carbon dioxide, and the like could also be used.

【0024】また、ガス注入用に設定するピンホール部
とは、弾性材に注射針が差し込める程度の大きさであ
り、約3mmφ以下を意味する。
The pinhole portion set for gas injection has such a size that an injection needle can be inserted into an elastic material, and means about 3 mmφ or less.

【0025】(実施例4)実施例1と同じ材料を使用
し、翼型羽根の中空部がコア部を介して連続空間となる
ように分割してチクソモールディング法によって外寸3
50mmφの送風機羽根車を成形した。その後、コア部
に配置したピンホール部だけを残して、翼型羽根の接合
箇所はシアノアクリレート系の接着剤で固定した。この
時、翼型羽根の設計肉厚は0.5mmとし、コア部は設
計肉厚1mmとした。次に、コア部のピンホール部から
弾性材を介して1.5kg/cm2 に内圧がなるように
窒素ガスを注入した後、弾性材が実用に際して外れない
よう接着剤で補強した。
(Embodiment 4) Using the same material as in Embodiment 1, the airfoil blade is divided so that the hollow portion becomes a continuous space via the core portion, and the outer dimensions of the airfoil blade are reduced by a thixomolding method.
A blower impeller of 50 mmφ was formed. Thereafter, the joint of the airfoil blade was fixed with a cyanoacrylate-based adhesive except for the pinhole portion arranged in the core portion. At this time, the design thickness of the airfoil blade was 0.5 mm, and the design thickness of the core portion was 1 mm. Next, nitrogen gas was injected from the pinhole portion of the core portion through the elastic material to an internal pressure of 1.5 kg / cm 2 so that the elastic material was reinforced with an adhesive so as not to come off in practical use.

【0026】実施例4と比較例1を比べると、翼型羽根
を中空化し、肉厚も0.5mmとすることで全体の重量
も実施例4のほうがはるかに軽量化された。さらに実施
例3と4を比較するとピンホール部を連続空間とするこ
とによって製造する上での作業性ははるかに向上した。
Comparing Example 4 with Comparative Example 1, the overall weight was much lighter in Example 4 by hollowing out the airfoil blade and making the wall thickness 0.5 mm. Further, when Examples 3 and 4 were compared, the workability in manufacturing was greatly improved by making the pinhole portion a continuous space.

【0027】実施例1〜4ではアルミニウムとの合金に
ついて示したが、本発明の目的に使用できるものはその
他、マンガン、亜鉛等があった。
In Examples 1 to 4, alloys with aluminum were shown, but manganese, zinc and the like could be used for the purpose of the present invention.

【0028】上記実施例1〜4で作成した送風機羽根車
を使用して、実用を踏まえた単体評価試験(苛酷試験と
衝撃強度試験)を行った。
Using the fan impellers prepared in Examples 1 to 4, unit evaluation tests (severe tests and impact strength tests) were conducted based on practical use.

【0029】苛酷試験は、室温にて1300rpm(使
用最高回転数の1.3倍)で運転25秒間/停止5秒間
を1サイクルとして10000サイクル繰り返した。そ
の後、クラック、変形等の異常の有無を観察した。
The severe test was repeated 10000 cycles at room temperature at 1300 rpm (1.3 times the maximum number of rotations used), one cycle of 25 seconds of operation and 5 seconds of stop. Thereafter, the presence or absence of abnormalities such as cracks and deformation was observed.

【0030】衝撃強度試験は、室温にて落錘式衝撃試験
装置に送風機羽根車を装着し、鋼球(100g)を50
cmの高さから各翼羽根に垂直落下させることを1サイ
クルとして100サイクル繰り返した。その後、送風機
羽根車を起動から1000rpmまで回転させた時に異
常音の有無を調べた。
In the impact strength test, a blower impeller was attached to a falling weight impact test apparatus at room temperature, and 50 g of steel balls (100 g) were placed.
One cycle of vertically dropping each blade from a height of cm was repeated 100 times. Thereafter, when the blower impeller was rotated to 1000 rpm from the start, the presence or absence of abnormal noise was examined.

【0031】その結果、実施例1〜4の送風機羽根車は
問題がないことを確認した。本発明は特に送風機羽根車
の材質に対して特徴を有しているが、海岸付近等の塩害
が危惧される場所に際しては耐食性強化のために表面へ
の塗膜コート等も必要となる。したがって、送風機羽根
車表面への塗膜コートしたものについても本発明の範囲
とする。
As a result, it was confirmed that the fan impellers of Examples 1 to 4 had no problem. The present invention is particularly characterized by the material of the blower impeller, but in places where there is a risk of salt damage, such as near the coast, a coating film or the like on the surface is required to enhance corrosion resistance. Therefore, a blower impeller surface coated with a coating film is also included in the scope of the present invention.

【0032】[0032]

【発明の効果】上記実施例から明らかなように、請求項
1記載の発明は、マグネシウム系合金からなる材質を使
用するもので、リサイクル化を容易にし、送風機羽根車
の難燃化も実現できる。
As is apparent from the above embodiment, the invention according to claim 1 uses a material made of a magnesium-based alloy, so that recycling can be facilitated and the blower impeller can be made flame-retardant. .

【0033】また、請求項2記載の発明は構造体内部を
中空化することによって省資源化が可能となる。
According to the second aspect of the present invention, it is possible to save resources by hollowing the inside of the structure.

【0034】また、請求項3記載の発明は翼型羽根の中
空部を大気圧以上に保持させることによって、外力によ
る変形に対して充分な反発性を有することでさらに薄肉
化が可能となる。
According to the third aspect of the present invention, by maintaining the hollow portion of the airfoil at a pressure higher than the atmospheric pressure, the airfoil has sufficient resilience against deformation due to an external force, thereby making it possible to further reduce the thickness.

【0035】また、請求項4記載の発明はコア部と翼型
羽根との中空部を連続空間とすることで大気圧以上に加
圧保持する作業性が向上する。
According to the fourth aspect of the present invention, the workability of maintaining the pressure above the atmospheric pressure is improved by making the hollow portion between the core portion and the airfoil blade a continuous space.

【0036】請求項5記載の発明は、製造方法として
は、送風機羽根車を構成要素に分割して成形して成形し
た後、接合して中空化を図ることで、直接中空化を行う
よりも品質の安定した製品が得られる。
According to a fifth aspect of the present invention, as a manufacturing method, a blower impeller is divided into constituent elements, formed and formed, and then joined to form a hollow, so that hollowing is performed more directly than hollowing is performed. Products with stable quality can be obtained.

【0037】また請求項6記載の発明は、中空部を加圧
状態にする場合には構成要素に分割された成形品を接合
した後、一部にピンホール部を設け、前記ピンホール部
からガスを注入し、その後前記ピンホール部を塞ぐこと
で、中空部加圧化の作業性が向上する。
According to a sixth aspect of the present invention, in the case where the hollow portion is pressurized, the molded product divided into the constituent elements is joined, and then a pinhole portion is provided in part, and By injecting a gas and then closing the pinhole portion, the workability of pressurizing the hollow portion is improved.

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

【図1】本発明の実施例が供される室外機本体の一部分
解斜視図
FIG. 1 is a partially exploded perspective view of an outdoor unit main body provided with an embodiment of the present invention.

【図2】本発明の実施例2によって得られた送風機羽根
車の斜視図
FIG. 2 is a perspective view of a blower impeller obtained according to a second embodiment of the present invention.

【符号の説明】[Explanation of symbols]

1 室外機本体 2 送風機羽根車 3 ファンモータ 4 ナット 1 Outdoor unit body 2 Blower impeller 3 Fan motor 4 Nut

Claims (6)

【特許請求の範囲】[Claims] 【請求項1】 マグネシウム系合金からなることを特徴
とする送風機羽根車。
1. A fan impeller comprising a magnesium-based alloy.
【請求項2】 構造体内部に中空層を有することを特徴
とする請求項1記載の送風機羽根車。
2. The blower impeller according to claim 1, further comprising a hollow layer inside the structure.
【請求項3】 翼型羽根の中空部が大気圧以上に加圧保
持されていることを特徴とする請求項1または2記載の
送風機羽根車。
3. The blower impeller according to claim 1, wherein the hollow portion of the airfoil is pressurized and held at a pressure higher than the atmospheric pressure.
【請求項4】 コア部と翼型羽根が中空部を有し、前記
中空部が連続空間で、かつ大気圧以上に加圧保持されて
いることを特徴とする請求項1または2記載の送風機羽
根車。
4. The blower according to claim 1, wherein the core portion and the airfoil blade have a hollow portion, and the hollow portion is a continuous space and is pressurized and held at a pressure higher than the atmospheric pressure. Impeller.
【請求項5】 送風機羽根車を構成要素に分割して成形
した後、接合部位を接着あるいはロウ付けで行うことを
特徴とする送風機羽根車の製造方法。
5. A method for manufacturing a blower impeller, wherein the blower impeller is divided into components and molded, and then a joining portion is bonded or brazed.
【請求項6】 送風機羽根車を構成要素に分割して成形
した後、接合部位を接着あるいはロウ付けで行った後、
一部にピンホール部を設け、前記ピンホール部からガス
を注入し、その後前記ピンホール部を塞ぐことによって
翼型羽根の中空部が大気圧以上に保持された構造体を得
ることを特徴とする送風機羽根車の製造方法。
6. After the blower impeller has been divided into components and formed, the joined portions are bonded or brazed.
A pinhole portion is provided in a part, a gas is injected from the pinhole portion, and thereafter, the hollow portion of the airfoil is obtained by closing the pinhole portion to obtain a structure in which the hollow portion is maintained at an atmospheric pressure or higher. Method of producing a blower impeller.
JP00991497A 1997-01-23 1997-01-23 Blower impeller Expired - Fee Related JP3752762B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP00991497A JP3752762B2 (en) 1997-01-23 1997-01-23 Blower impeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP00991497A JP3752762B2 (en) 1997-01-23 1997-01-23 Blower impeller

Publications (2)

Publication Number Publication Date
JPH10205493A true JPH10205493A (en) 1998-08-04
JP3752762B2 JP3752762B2 (en) 2006-03-08

Family

ID=11733382

Family Applications (1)

Application Number Title Priority Date Filing Date
JP00991497A Expired - Fee Related JP3752762B2 (en) 1997-01-23 1997-01-23 Blower impeller

Country Status (1)

Country Link
JP (1) JP3752762B2 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6468038B1 (en) 1999-03-03 2002-10-22 Mitsubishi Denki Kabushiki Kaisha Fan, method for producing the fan by molding molten metal, and device for producing the fan by molding molten metal
US7332838B2 (en) * 2004-04-09 2008-02-19 Hitachi Koki Co., Ltd. Motor-fan assembly and combustion-type power tool employing the same
JP2009210185A (en) * 2008-03-04 2009-09-17 Mitsubishi Electric Corp Air conditioner and safety management method of air conditioner

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6468038B1 (en) 1999-03-03 2002-10-22 Mitsubishi Denki Kabushiki Kaisha Fan, method for producing the fan by molding molten metal, and device for producing the fan by molding molten metal
US6595265B2 (en) 1999-03-03 2003-07-22 Mitsubishi Denki Kabushiki Kaisha Fan, method for producing the fan by molding molten metal, and device for producing the fan by molding molten metal
US7332838B2 (en) * 2004-04-09 2008-02-19 Hitachi Koki Co., Ltd. Motor-fan assembly and combustion-type power tool employing the same
JP2009210185A (en) * 2008-03-04 2009-09-17 Mitsubishi Electric Corp Air conditioner and safety management method of air conditioner

Also Published As

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