JPS5893997A - Blower - Google Patents
BlowerInfo
- Publication number
- JPS5893997A JPS5893997A JP56190755A JP19075581A JPS5893997A JP S5893997 A JPS5893997 A JP S5893997A JP 56190755 A JP56190755 A JP 56190755A JP 19075581 A JP19075581 A JP 19075581A JP S5893997 A JPS5893997 A JP S5893997A
- Authority
- JP
- Japan
- Prior art keywords
- diffuser
- inlet
- impeller
- blade
- axial width
- 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.)
- Pending
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/44—Fluid-guiding means, e.g. diffusers
- F04D29/441—Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/50—Inlet or outlet
- F05D2250/52—Outlet
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
【発明の詳細な説明】
この発明は家庭用電気掃除機の電動送風機にかかわり、
特にその流体性能の向上に関するものである。[Detailed Description of the Invention] This invention relates to an electric blower for a household vacuum cleaner.
In particular, it concerns the improvement of its fluid performance.
従来用いられている電動送風機の構成及び作用を第1図
〜第4図により説明する。第1図は電動送風機の縦断面
図であって、1は電動機を表わし。The structure and operation of a conventionally used electric blower will be explained with reference to FIGS. 1 to 4. FIG. 1 is a longitudinal sectional view of an electric blower, and 1 represents an electric motor.
その回転軸2の一端に遠心形の羽根車3がナツト4によ
り締結されている。羽根車3の外側には前面がほぼ円錐
形、 111面が円筒形のケーシング5が配置きれ、電
動機1の送風機側の端部に設けられ7m円板形のエンド
ブラケット6に嵌合して内部に空間を形成し、前記羽根
車全収納している。ケータング5内には羽根車3の後面
(反吸込側)に位置して円板状の仕切板7が配置9篤円
周方向の複数個所においてボルト8によりエンドブラケ
ット6及び電動機1に固定さ扛る。仕切板7の前面(吸
込側)かつ羽根車3の外周には、円形翼列状のディフュ
ーザg9が突設され、筐た仕切&7の後面には戻9案内
興10が突設ちれて流体通路を形成する。また仕切板7
の外周端とケーシング5の内周面との間には円環状の間
隙11が形成される。羽根車3の回転により空気は吸込
口12から吸入され、羽根車により加圧された後ディフ
ューザ翼91円猿状間隙11.及び戻り案内XIOから
成る流体通路を流れて減速しつつ動圧を静圧に変換され
、エンドブラケット6及び電動機の端部に設けられた吸
気口13より電動機の内部に流入し、電動機を冷却した
後電動機の他端又は側方に設けられた開口部(図示せず
)から流出する。第2図、第3図及び第4図はそれぞ扛
ディフューザ翼、戻シ案内翼、及び吸気口の軸方向親図
でろる。A centrifugal impeller 3 is fastened to one end of the rotating shaft 2 with a nut 4. A casing 5 having a substantially conical front surface and a cylindrical surface 111 is disposed outside the impeller 3, and is fitted into a 7 m disc-shaped end bracket 6 provided at the end of the electric motor 1 on the blower side. A space is formed in which the impeller is fully housed. A disk-shaped partition plate 7 is disposed inside the impeller 5 on the rear surface (anti-suction side) of the impeller 3, and is fixed to the end bracket 6 and the electric motor 1 with bolts 8 at multiple locations in the circumferential direction. Ru. A diffuser g9 in the form of a circular blade row is protruded from the front surface (suction side) of the partition plate 7 and the outer periphery of the impeller 3, and a return 9 guide box 10 is protruded from the rear surface of the partition &7 housing to prevent the fluid from flowing. form a passage. Also, partition plate 7
An annular gap 11 is formed between the outer peripheral end of the casing 5 and the inner peripheral surface of the casing 5 . As the impeller 3 rotates, air is sucked in through the suction port 12, and after being pressurized by the impeller, the air is passed through the diffuser blade 91 through the circular monkey-shaped gap 11. The dynamic pressure is converted into static pressure while flowing through the fluid passage consisting of the return guide XIO and the return guide XIO, and flows into the inside of the motor through the intake port 13 provided at the end bracket 6 and the end of the motor to cool the motor. It flows out from an opening (not shown) provided at the other end or side of the rear motor. FIGS. 2, 3 and 4 are axial views of the diffuser vane, return guide vane, and intake port, respectively.
上記構成の電動送風機で用いられているディフューザ翼
、戻シ案内翼等の構成は、従来用いられている大形の送
風機・圧縮機等のそれらと似ているが、電動送風機では
太き逼・形状等に特に制約がある。すなわち大形機にお
いてはディフューザの出口径と入口径との比は1.4〜
2程度に大きくとるのが普通であるが、電動送風機にお
いては1.15〜1.25程度の小さな値しかとること
ができず、$11方向の寸法も同様に極端に制限さ扛て
いる。しかるに従来の電動送風機ではこのような制約さ
れたスペース内で効率のよい流体通路を構成するという
工夫がなされておらず、従って流体性能が低く、騒音レ
ベルが高い等の欠点がめった。The configurations of the diffuser blades, return guide vanes, etc. used in the electric blower with the above configuration are similar to those of conventionally used large-sized blowers and compressors. There are particular restrictions on the shape, etc. In other words, in large machines, the ratio of the diffuser outlet diameter to the inlet diameter is 1.4 to
Normally, the value is as large as about 2, but electric blowers can only take a small value of about 1.15 to 1.25, and the dimension in the $11 direction is also extremely limited. However, conventional electric blowers have not been designed to construct an efficient fluid passage within such a restricted space, and therefore often suffer from drawbacks such as low fluid performance and high noise levels.
また通常の遠心送風機・圧縮機では1羽根車から吐出さ
れる流nが円周方向に対してなす内反は20°〜30°
の程贋の値でLEI、従ってディフューザ翼の入口角も
この値に合せて設計さnるが、電動送風機は低比速度(
圧力が高い割合に流量が少ない)であり、ディフューザ
入口における匠扛角(!−iディフューザ翼入日入口角
6°前後という小さな値である。このような低流入角に
おいては失速が生じ易く、また流れの損失が大きくて良
好なディフューザ効4I−を得ることが困難で必るが。In addition, in a normal centrifugal blower/compressor, the inversion of the flow n discharged from one impeller with respect to the circumferential direction is 20° to 30°.
The inlet angle of the diffuser blade is also designed according to this value, but the electric blower has a low specific speed (
The flow rate is small when the pressure is high), and the angle of entry at the diffuser inlet (!-i) is a small value of around 6 degrees at the inlet angle of the diffuser blade. At such a low inflow angle, stall is likely to occur, Furthermore, it is difficult to obtain a good diffuser effect due to large flow loss.
この点も従来の電動送風機では考慮されておらず。This point is also not taken into consideration with conventional electric blowers.
そのため流体性能が低いという欠点があった。Therefore, there was a drawback that fluid performance was low.
この発明は、前記欠点を除去し流体性能の高い家庭電気
掃除機用電動送風機を提供することを目的とする。SUMMARY OF THE INVENTION An object of the present invention is to provide an electric blower for a domestic vacuum cleaner that eliminates the above-mentioned drawbacks and has high fluid performance.
この発明の特徴は、ディフューザ真の入口と羽根車出口
との間に翼なし部分を設けてディフューザ翼人口の軸方
向幅を翼なし部分入口の軸方向幅よりも小式くすること
によシ、流速の半径方向成分が加速するようにし、流れ
角を増加せしめてディフューザの通路長さ比及び等価広
が9角(いずれも後述)がディフューザの性能上良好な
範囲に来るようにしたことである。The feature of this invention is that a bladeless portion is provided between the diffuser true inlet and the impeller outlet, and the axial width of the diffuser blade population is made smaller than the axial width of the bladeless portion inlet. By accelerating the radial component of the flow velocity and increasing the flow angle, the diffuser's passage length ratio and equivalent spread angle of 9 (both will be described later) are within a range that is good for the performance of the diffuser. be.
遠心型流体機械に用いられるディフューザの特性を第5
図を用いて説明する。図の横軸はディフューザ翼の長さ
くあるいは翼間通路中心線の長さ)tと、ディフューザ
翼の入口において流れ方向に直角に測った通路幅W1−
π])、sinム/Z (ここにDは回転軸中心に関す
る直径、βは興が円周方向に対してなす角、Zは翼枚数
、小学1はナイフユーザ翼入口を表わす)との比t/W
Ikfiわし、縦軸ri翼間通路を真直ぐな通路に置換
しfc場合の等価広がり角θ=2tan−’[(w2−
w+)/2z) (iだしW2−πD2sinβ、/z
、i字2はディフューザ翼出口を表わす)を表わしてい
る。−1′fにの図中で右下りの曲線群はディフューザ
の面積比A、−Wt/ Wl(= (D2sinβ2)
/ (D、 sinβl))が一定の線群を表わし、
ディフューザ効率η及びティ7ユーザの圧力上昇係数C
2、(いずれも次に定義する)が一定の曲線群は、発明
者が実験によシ求めたものである。The characteristics of diffusers used in centrifugal fluid machines are explained in the fifth section.
This will be explained using figures. The horizontal axis of the figure is the length of the diffuser blade or the length of the center line of the passage between the blades (t), and the passage width W1- measured perpendicular to the flow direction at the inlet of the diffuser blade.
π]), sin/Z (where D is the diameter with respect to the center of the rotation axis, β is the angle that the axis makes with respect to the circumferential direction, Z is the number of blades, and elementary school 1 represents the knife user blade inlet). t/W
Ikfi, the equivalent spread angle θ = 2tan-' [(w2-
w+)/2z) (i outW2-πD2sinβ,/z
, i-character 2 represents the diffuser blade outlet). The group of curves descending to the right in the figure at -1'f is the area ratio A of the diffuser, -Wt/Wl (= (D2sinβ2)
/ (D, sinβl)) represents a certain group of lines,
Diffuser efficiency η and pressure rise coefficient C of tee 7 user
2. A group of curves with constant values (both defined below) were obtained through experiments by the inventor.
(ここにPは静圧、Uは流速、ρrユ流体の密度を表わ
す)
前記のように電動送風機用にディフューザJK1t用い
る場合、興入口における流れ角が極めて小さいので、非
常に長い翼になり易く、従来の方法でディフューザを設
計すると第5図中に記号Aで示すようにt/Wl=14
〜20.θ=13°〜9°の付近の値となる。この形状
に相当するディフューザの圧力係数Cp rB o、
5〜0.55であって十分高い値ではない。なおここで
面積比A、は約4としているが、これはこの種のディフ
ューザでとられる実際上最大の面積比(剥離防止上必要
)である。(Here, P is the static pressure, U is the flow velocity, and ρr represents the density of the fluid.) As mentioned above, when using the diffuser JK1t for an electric blower, the flow angle at the inlet is extremely small, so the blades tend to be very long. , if the diffuser is designed using the conventional method, t/Wl=14 as shown by symbol A in FIG.
~20. The value is around θ=13° to 9°. Pressure coefficient Cp rBo of a diffuser corresponding to this shape,
5 to 0.55, which is not a sufficiently high value. Here, the area ratio A is approximately 4, which is actually the maximum area ratio (necessary for preventing peeling) for this type of diffuser.
この発明の実施例を第6図により説明する。図はディフ
ューザ部分の縦断面図であり、他の部分については第1
図〜第4図に示したものと同じなので、説明を省略する
。図に示すようにディフューザ翼9の入口と羽根車3の
出口との間に、xなし部分14が設けら扛、ディフュー
ザ翼入口の軸方向幅b1は興なし部分入口の軸方向幅b
oより小さくしぼらnて、流速の半径方向成分C2が加
速されるように芒れている。すなわち翼なし部分入口に
おける半径方向流速成分はC,O=Q/(πDobo)
(ここにQは風量、添字Oは興なし部分入口を表わす)
であり、7″″イフユ一ザ翼入口の半径方向流速成分は
C,l=Q/(πD+ b+ )であるから、D+ b
+ < Do boであるようにす扛ば。An embodiment of this invention will be explained with reference to FIG. The figure is a vertical cross-sectional view of the diffuser part, and other parts are
Since it is the same as that shown in FIGS. 4 to 4, the explanation will be omitted. As shown in the figure, a portion 14 without x is provided between the inlet of the diffuser blade 9 and the outlet of the impeller 3.
It is narrowed to be smaller than o so that the radial component C2 of the flow velocity is accelerated. In other words, the radial velocity component at the inlet of the part without blades is C, O=Q/(πDobo)
(Here, Q represents the air volume, and the subscript O represents the entrance without opening.)
, and the radial flow velocity component at the inlet of the 7'' filter blade is C,l=Q/(πD+ b+ ), so D+ b
+ < Do bo.
Cz>Cro となる。また流nが円周方向に対してな
す角(流れ角)αはα=(8)−’(C,/C,)(C
,は流速の円周方向成分で、Xなし部分においてはC2
はDに半比例する)であるから、ディフューザ翼入口に
おける流n角は翼なし部入口よシも増加せしめられる。Cz>Cro. The angle (flow angle) α that the flow n makes with the circumferential direction is α=(8)-'(C, /C,)(C
, is the circumferential component of the flow velocity, and in the part without X, C2
is half proportional to D), the flow n angle at the inlet of the diffuser blade is also increased at the inlet of the non-blade section.
実例でいえば2通常の場合ディフューザ入口においてα
は6°付近であるが、発明者等はこれを10°程度まで
増加させた。こlしによpディフューザ通路のt /
W+ とθは第5図に示すB点(z/Wt =i t
、θ−16°)に移動し、この結果圧力上昇係数Cp
rは約0.6に上昇した。なお面積比は4となるようb
2及びβ2を定めている。In an actual example, 2. Normally, α at the diffuser inlet
is around 6°, but the inventors increased this to around 10°. T of the diffuser passage /
W+ and θ are at point B (z/Wt = i t
, θ-16°), resulting in a pressure increase coefficient Cp
r rose to about 0.6. Note that the area ratio is 4 b
2 and β2 are determined.
翼なし部分14において流速の半径方向成分C1は増速
するが1円周方向成分、CuはDに反比例して減速する
ので、流速の絶対値c < −Vの1己>はXなし部分
において若干減少する。すなわちこの部分は面積比の小
さい(1,05〜1.1程度の)ディフューザとなって
、減速ならびに流れの安定化・整流に貢献する。The radial component C1 of the flow velocity increases in the bladeless part 14, but the circumferential component C1 slows down in inverse proportion to D, so the absolute value of the flow velocity c < -V 1> in the part without X. It will decrease slightly. In other words, this portion becomes a diffuser with a small area ratio (about 1.05 to 1.1) and contributes to deceleration and stabilization and rectification of the flow.
第6図の実施例では、ディフューザ翼9及び翼なし部分
14の前面側をそろえて、回転軸に対して垂直な一平面
上にあるようにしたが、この場合ディフューザ及びケー
シングの製作が容易であるという利点がある。しかしこ
の形に限る必賛はなく。In the embodiment shown in FIG. 6, the front sides of the diffuser blades 9 and the bladeless portion 14 are aligned so that they lie on one plane perpendicular to the rotation axis, but in this case, the diffuser and casing can be manufactured easily. There is an advantage to having one. However, there is no guarantee that it is limited to this form.
仕切板側を平面とし、ケーンング側を傾斜面とすること
(又は両側とも傾斜面とすること)も可能である。この
場合一般に遠心型羽根車から流出する流nはハブ側(仕
切板側)で速度が高いので、第6図の実施例よりも性能
的に有利である。It is also possible to have the partition plate side as a flat surface and the caning side as an inclined surface (or both sides as inclined surfaces). In this case, since the flow n flowing out from the centrifugal impeller generally has a higher speed on the hub side (partition plate side), this embodiment is more advantageous in terms of performance than the embodiment shown in FIG.
第7図は上記実施例の効果を示す実験結果で。FIG. 7 shows experimental results showing the effects of the above embodiment.
電動送風機の風量Qと圧力(静圧)Hとの関係を示す。The relationship between the air volume Q and the pressure (static pressure) H of the electric blower is shown.
図で破線で示す特性曲線は従来方式により設計したほぼ
同枚数のディフューザを用いた場合の特性で、実aはこ
の発明の場合を示す。図からこの発明のディフューザの
場合1%性曲勝は大凧側へ大幅に伸び、大部分の風量範
囲において発生(9)
圧力が従来例よシも蔦いことがわかる。The characteristic curve shown by the broken line in the figure is the characteristic when almost the same number of diffusers designed by the conventional method are used, and the curve a shows the characteristic curve according to the present invention. From the figure, it can be seen that in the case of the diffuser of the present invention, the 1% deflection greatly extends toward the large kite side, and the pressure generated in most of the air volume range (9) is even higher than in the conventional case.
以上の説明かられかるように、この発明ではディフュー
ザ翼の入口と羽根車出口との間に真なし部分を設けてデ
ィフューザ翼入口の軸方向幅を翼なし部分入口の軸方向
幅よυも小名くすることにより、流速の半径方向成分が
加速するように構成したことにより、電動送風機のディ
フューザII&を入口角の大きい範囲へ移行させ、ディ
フューザ翼間通路の長さ比1 / W 1 と等側床が
9角θとをディフューザの特性マツプ上で性能上有利な
範囲へ移して高い圧力上昇が得られるようにしたので、
製作費用の著しい増加を招くことなしに送風機の流体的
特性を大幅に改善し、高性能の電動送風機を提供するこ
とができる。As can be seen from the above description, in the present invention, a trueless portion is provided between the inlet of the diffuser blade and the impeller outlet, so that the axial width of the diffuser blade inlet is smaller than the axial width of the inlet of the bladeless portion. Namely, by configuring the radial component of the flow velocity to accelerate, the diffuser II & of the electric blower is moved to a range with a large inlet angle, and the length ratio of the passage between the diffuser blades is 1 / W 1 etc. Since the side floor moves the 9-angle θ to a range that is advantageous for performance on the diffuser characteristic map, a high pressure rise can be obtained.
The fluid characteristics of the blower can be significantly improved without significantly increasing manufacturing costs, and a high-performance electric blower can be provided.
第1図は従来の電動送風機を示す縦断面図、第2図は第
1図ディフューザの軸方向親図(II−n矢視図)、第
3図は第1図戻り案内翼の軸方向親図(I[−III矢
視図親図第4図は第1図電動機吸気口の軸方向*親図(
■−■矢視図親図第5図はデ(10)
ィフユーザの特性を示すマツプ図、第6図はこの発明に
よるディフューザの縦断面図、第7図はこの発明の効果
を示す送風機特性図である。
3・・・羽根車、7・・・仕切板、9・・・ディフュー
ザ翼。
10・・・戻シ案内翼、14・・・翼なし部分。
代理人 弁理士 薄田利幸
(11)Fig. 1 is a vertical sectional view showing a conventional electric blower, Fig. 2 is an axial main view of the diffuser shown in Fig. 1 (viewed from arrow II-n), and Fig. 3 is an axial main view of the return guide vane shown in Fig. 1. Figure (I
Figure 5 is a map diagram showing the characteristics of the D(10) fifter, Figure 6 is a longitudinal sectional view of the diffuser according to the present invention, and Figure 7 is a blower characteristic diagram showing the effects of the present invention. It is. 3... Impeller, 7... Partition plate, 9... Diffuser blade. 10... Return guide blade, 14... Wingless part. Agent Patent attorney Toshiyuki Usuda (11)
Claims (1)
面に円板状の仕切板を配置して同仕切板の前面かつ羽根
車の外周にディフューザXを。 また仕切板の後面に戻シ案内翼を突設し、仕切板の外周
端と前記ケーシングとの間に円環状の間隙を形成したも
のにおいて。 ディフューザ翼入口と羽根車出口との間に興なし部分を
設け、ディフューザ翼入口の軸方向幅は翼なし部分入口
の軸方向幅よりも小さくして流れの半径方向速度成分を
加速させるようにすると共に、ディフューザ翼の軸方向
幅を出口へかけて拡大せしめ、かつディフューザの面積
比 A r = D2b、sinβ2/D 、 b 、 s
inβ、(ここにDは回転軸中心に関する直径、bは軸
方向幅、βは翼が円周方向に対してなす角、添字1はデ
ィフューザ翼の入口、2は同じく出口)が4を著しく越
ちぬようディフューザ翼出口の軸方向幅b2及び出口角
β2を定めたことを特徴とする電動送風機。 2、特許請求の範囲1において、ディフューザの前面端
が回転軸に垂直な一平面内にあるようにしたことを特徴
とする電動送風機。[Claims] 1. A centrifugal impeller is coupled to a rotating shaft of an electric motor. A cylindrical casing is provided on the outside of the impeller, a disk-shaped partition plate is arranged on the back of the impeller, and a diffuser X is provided in front of the partition plate and on the outer periphery of the impeller. Further, a return guide vane is provided protruding from the rear surface of the partition plate, and an annular gap is formed between the outer peripheral end of the partition plate and the casing. An uncircumcised portion is provided between the diffuser blade inlet and the impeller outlet, and the axial width of the diffuser blade inlet is smaller than the axial width of the bladeless portion inlet to accelerate the radial velocity component of the flow. At the same time, the axial width of the diffuser blade is expanded toward the exit, and the area ratio of the diffuser A r = D2b, sin β2/D , b , s
inβ, (where D is the diameter with respect to the center of the rotation axis, b is the axial width, β is the angle that the blade makes with respect to the circumferential direction, the subscript 1 is the inlet of the diffuser blade, and 2 is the outlet) significantly exceeds 4. An electric blower characterized in that an axial width b2 and an exit angle β2 of a chinuyo diffuser blade outlet are determined. 2. The electric blower according to claim 1, wherein the front end of the diffuser is located within a plane perpendicular to the rotation axis.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP56190755A JPS5893997A (en) | 1981-11-30 | 1981-11-30 | Blower |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP56190755A JPS5893997A (en) | 1981-11-30 | 1981-11-30 | Blower |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5893997A true JPS5893997A (en) | 1983-06-03 |
Family
ID=16263188
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP56190755A Pending JPS5893997A (en) | 1981-11-30 | 1981-11-30 | Blower |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5893997A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6123898A (en) * | 1984-07-09 | 1986-02-01 | Matsushita Electric Ind Co Ltd | Blower for electrical cleaner |
JPS6128800A (en) * | 1984-07-20 | 1986-02-08 | Matsushita Electric Ind Co Ltd | Motor-driven blower |
FR2619812A1 (en) * | 1987-08-31 | 1989-03-03 | Zinpro Corp | FERRIC ION-CATALYSED PROCESS FOR COMPLEXING ZINC AND / OR MANGANESE WITH ALPHA-AMINO ACIDS |
US4929149A (en) * | 1985-01-08 | 1990-05-29 | Superstream, Inc. | Gas blower |
EP0375198A2 (en) * | 1988-12-05 | 1990-06-27 | Kazuo Kuroiwa | Supersonic centrifugal compressor |
JPH03140660A (en) * | 1989-10-25 | 1991-06-14 | Yanmar Diesel Engine Co Ltd | Lubricating oil supply system for marine multistage reduction reverser |
-
1981
- 1981-11-30 JP JP56190755A patent/JPS5893997A/en active Pending
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6123898A (en) * | 1984-07-09 | 1986-02-01 | Matsushita Electric Ind Co Ltd | Blower for electrical cleaner |
JPS6128800A (en) * | 1984-07-20 | 1986-02-08 | Matsushita Electric Ind Co Ltd | Motor-driven blower |
US4929149A (en) * | 1985-01-08 | 1990-05-29 | Superstream, Inc. | Gas blower |
FR2619812A1 (en) * | 1987-08-31 | 1989-03-03 | Zinpro Corp | FERRIC ION-CATALYSED PROCESS FOR COMPLEXING ZINC AND / OR MANGANESE WITH ALPHA-AMINO ACIDS |
EP0375198A2 (en) * | 1988-12-05 | 1990-06-27 | Kazuo Kuroiwa | Supersonic centrifugal compressor |
JPH03140660A (en) * | 1989-10-25 | 1991-06-14 | Yanmar Diesel Engine Co Ltd | Lubricating oil supply system for marine multistage reduction reverser |
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