JP2007506037A - Propeller blower and shell propeller - Google Patents

Propeller blower and shell propeller Download PDF

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JP2007506037A
JP2007506037A JP2006527430A JP2006527430A JP2007506037A JP 2007506037 A JP2007506037 A JP 2007506037A JP 2006527430 A JP2006527430 A JP 2006527430A JP 2006527430 A JP2006527430 A JP 2006527430A JP 2007506037 A JP2007506037 A JP 2007506037A
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wing
propeller
impeller disk
propeller blower
blower
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ブリュニク,マシアス
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Priority claimed from DE200410010457 external-priority patent/DE102004010457B3/en
Priority claimed from DE200410043618 external-priority patent/DE102004043618A1/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/30Vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/325Rotors specially for elastic fluids for axial flow pumps for axial flow fans
    • F04D29/329Details of the hub

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

本発明は、流路の内側に隣接し凸状の翼1を備える羽根車円盤2を用いて吸引される空気の軸方向への排出のためのプロペラ送風機に関する。翼1は、延ばされ拡大したシェルブレードとして具象化される。端部領域20は、貫入領域において羽根車円盤2に接続されている。他端21は、外部へ半径方向に延び、流れ方向において軸方向成分と共に半径距離が増加してある。
【選択図】図1
The present invention relates to a propeller blower for discharging air sucked in an axial direction using an impeller disk 2 having a convex blade 1 adjacent to the inside of a flow path. The wing 1 is embodied as an extended and enlarged shell blade. The end region 20 is connected to the impeller disk 2 in the penetration region. The other end 21 extends radially outward and has a radial distance that increases with the axial component in the flow direction.
[Selection] Figure 1

Description

本発明は、内部の流れを定めると共に羽根車円盤として形成され、回転軸を中心に回転駆動されるハブを用いて、気体又は液体の媒体の流出を実質的に軸方向に方向付けるためのプロペラ送風機に関し、上記ハブは、流れ方向における翼流入端と翼流出端との間の翼領域で湾曲した翼を備える。   A propeller for directing the outflow of a gaseous or liquid medium in a substantially axial direction using a hub that defines an internal flow and is formed as an impeller disk and is driven to rotate about a rotational axis. With respect to the blower, the hub includes a blade that is curved in a blade region between a blade inflow end and a blade outflow end in the flow direction.

既知のこの種の送風機(100 20878C2:独国特許明細書)は、外側におけるガイド面によって与えられる。これに関し、厳密に制限された吸い込み領域のみが軸方向へ実行できる。   A known blower of this kind (100 20878C2: German patent specification) is provided by a guide surface on the outside. In this regard, only a strictly limited suction area can be performed in the axial direction.

本発明の課題は、例えばキッチンにおいて上昇する湯気がフードを用いることなく広範囲に亘って引き込まれるように、吸い込まれる媒体が半球状に流入して軸方法に流出するような種類のプロペラ送風機を設計することである。   The object of the present invention is to design a propeller blower of a kind in which the sucked medium flows in a hemisphere and flows out into the shaft method so that steam rising in the kitchen is drawn over a wide range without using a hood, for example It is to be.

各搬送翼が、縦方向に延びる牡蠣の貝殻の形状に形成され、一端が上記の羽根車円盤に接続され、その接続ラインにおいて羽根車円盤に垂直であり、更に他端が軸方向において半径が増加するよう方向付けられることによって、上述のプロペラ送風機が得られる。この翼は、回転方向へ凹型に湾曲してなる。   Each conveying wing is formed in the shape of an oyster shell extending in the longitudinal direction, one end is connected to the impeller disk, the connection line is perpendicular to the impeller disk, and the other end has a radius in the axial direction. By being directed to increase, the above-described propeller blower is obtained. The wing is curved in a concave shape in the rotational direction.

上記翼は、縦方向への楕円形の延びが、アコヤ貝や川真珠貝(Margaritana margaritifera)に似ている。そのハブ或いは羽根車円盤は、平らな形状を呈し、又は回転楕円体のように若しくは放物形や双曲形で用いられる。   The wing has an elliptical extension in the vertical direction, similar to the pearl oyster and margaritana margaritifera. The hub or impeller disk has a flat shape, or is used like a spheroid or in a parabolic or hyperbolic shape.

提案するプロペラ送風機は、主として半径方向におけるシャフトの傍の内側領域において運搬される媒体を促進する。上記の回転方向へ凹型に湾曲した搬送翼は、送風機の囲い、例えばパイプを要さないように、軸方向に向かう外側端部において外部に流れる媒体をガイドする。単純計算及び実験でも、媒体が外側端部において吸い込まれることを示している。これは、外側端部における周速度が、遠心力により達成できる媒体の視線速度よりも大きいということである。このように、例えば、キッチンにおいて上昇する暖気が、フードなしで放出され得る。翼の形状は、騒音を引き起こす単純な振動も許容しない。測定結果は、同一速度で運転される同一サイズの軸流送風機に比較して最大8dB低いというプロペラ送風機の騒音レベルを裏付ける。適切に翼を形成することによって、提案するプロペラ送風機に伴い、媒体の流出角度がおよそ25°まで開口することにも成功した。その結果、大量に周囲の媒体から取り込まれるので、このように大量に移動される。1250rev/minにおいて最高限度1m/sで排出する直径14cmのプロペラ送風機の1つが、計測された。このように、この小さい送風機は、遅く作動する大きい送風機に取って代わることができる。 The proposed propeller blower promotes the medium carried in the inner region beside the shaft, mainly in the radial direction. The conveying blade curved in a concave shape in the rotational direction guides the medium flowing to the outside at the outer end in the axial direction so as not to require a pipe, for example, a pipe. Simple calculations and experiments also show that the media is sucked at the outer edge. This means that the peripheral speed at the outer end is greater than the line speed of the medium that can be achieved by centrifugal force. Thus, for example, warm air rising in the kitchen can be released without a hood. The shape of the wing does not tolerate simple vibrations that cause noise. The measurement results confirm the noise level of the propeller blower, which is a maximum of 8 dB lower than the same size axial blower operating at the same speed. By properly forming the wings, the outflow angle of the medium was successfully opened to about 25 ° with the proposed propeller blower. As a result, since a large amount is taken in from the surrounding medium, it is moved in such a large amount. One of the 14 cm diameter propeller blowers discharging at a maximum limit of 1 m 3 / s at 1250 rev / min was measured. Thus, this small blower can replace a large blower that operates slowly.

以下、本発明の一例を、図面を参照しながら説明する。
図1乃至図3によれば、羽根車円盤2は、回転軸3を中心に回転駆動される。その回転方向は、矢印5で示されている。
Hereinafter, an example of the present invention will be described with reference to the drawings.
According to FIGS. 1 to 3, the impeller disk 2 is driven to rotate about the rotation shaft 3. The direction of rotation is indicated by arrow 5.

より良い概観のために、ただ1つの翼1が図1乃至図3に示されている。実際の実施では、均一に又は不均一に間隔の空いた、異なる大きさでも、通常いくつかの翼1が羽根車円盤に取付けられるだろう。   For a better overview, only one wing 1 is shown in FIGS. In actual practice, several wings 1 will usually be attached to the impeller disk, even with different sizes, uniformly or non-uniformly spaced.

翼1は、実質的に牡蠣の貝殻の形状を呈しており、一体的に羽根車円盤2に接続され又は羽根車円盤2へ組み込まれ若しくは接着されている。これらは、注入部品又は成形部品によって形成され得る。それには、翼1及び羽根車円盤2が、いわゆる貫入部(penetration)内に入り込むことで、この貫入部の外側を翼1の流出端に併合するような歯元ライン6が形成されることが重要である。歯元ライン6とは反対側の端部は、媒体が流入する翼流入端22である。図1において、この翼流入端が外側領域に延びるのを矢印30で見ることができる。翼1は、領域21において軸方向に向いているが、領域20においては半径方向に向いている。   The wing 1 is substantially in the shape of an oyster shell, and is integrally connected to the impeller disk 2 or is incorporated into or bonded to the impeller disk 2. These can be formed by injection parts or molded parts. To this end, the blade 1 and the impeller disk 2 enter a so-called penetration, and a tooth root line 6 is formed so that the outside of the penetration merges with the outflow end of the blade 1. is important. The end opposite to the tooth root line 6 is a blade inflow end 22 into which the medium flows. In FIG. 1, it can be seen by arrow 30 that this blade inlet end extends into the outer region. The wing 1 faces in the axial direction in the region 21, but faces in the radial direction in the region 20.

図2に翼1の特有の形状を再度示し、図4に図2のA−B断面図を示す。図4に示す角度4は、回転速度のベクトル5と翼1の端部の方向との流入角を示している。
図3では、歯元ライン6の手前に、放射状流の増加に寄与する羽根車円盤2の窪み4を認識することができる。提案するプロペラ送風機では、船や航空機をも駆動することができる。
FIG. 2 shows the specific shape of the blade 1 again, and FIG. 4 shows a cross-sectional view taken along the line AB of FIG. An angle 4 shown in FIG. 4 indicates an inflow angle between the rotational speed vector 5 and the direction of the end of the blade 1.
In FIG. 3, the depression 4 of the impeller disk 2 that contributes to an increase in the radial flow can be recognized before the tooth root line 6. The proposed propeller blower can also drive ships and aircraft.

例えば水や空気のような搬送される媒体を外側端部においても吸い込む本発明に係るプロペラは、図5に提案されている。吸引が流出に変化する場合に外側端部又はプロペラ翼1の位置が、図5のように媒体が流出するスペースにおける外壁10の面内の孔の内部に正確に位置しているとき、圧力差に基づいてスペースから吸い込まれる空気や他の液体の吸引に関してとりわけ有益な新型のプロペラの配置が用いられる。外壁の面は、図5によれば、結果として、プロペラ翼1の外側端部の傍に位置する。矢印30は、流れ方向を示す。プロペラ翼1の端部は、図2の下部に示すように、角を有さないよう丸くなっていることが図5に更に示されている。   For example, a propeller according to the present invention that sucks in a transported medium such as water or air also at the outer end is proposed in FIG. When the suction changes to outflow, the position of the outer end or propeller blade 1 is accurately positioned inside the hole in the surface of the outer wall 10 in the space where the medium flows out as shown in FIG. A new type of propeller arrangement is used which is particularly useful with respect to the suction of air and other liquids drawn from the space. According to FIG. 5, the surface of the outer wall is consequently located near the outer end of the propeller blade 1. Arrow 30 indicates the flow direction. It is further shown in FIG. 5 that the end of the propeller blade 1 is rounded to have no corners, as shown in the lower part of FIG.

適切な形成によって多少拡げることの可能な円錐状に拡がる流出の特性は、流入又は流出端部における任意の制限板を必要とせず、冷却パックされた冷却管を通る空気の噴き出しを可能にする。このように、カルマン渦によって発生する騒音を緩和するために、プロペラが空間内の吸い込み側に位置し開口部が溝付管(slotted pipe)に囲まれた空間から媒体を吸い込むことが可能となる。   The conically spreading outflow characteristic, which can be expanded somewhat by proper formation, does not require any restricting plates at the inflow or outflow end, and allows air to be blown through the cold-packed cooling tubes. As described above, in order to mitigate the noise generated by the Karman vortex, it is possible to suck the medium from the space where the propeller is located on the suction side in the space and the opening is surrounded by the slotted pipe. .

本発明に係るプロペラに関するただ1つの翼を伴う羽根車円盤を示す図である。FIG. 2 shows an impeller disk with only one wing for the propeller according to the invention. 羽根車円盤から分離させた図1に示す翼を示す図である。It is a figure which shows the wing | blade shown in FIG. 1 isolate | separated from the impeller disk. 窪み及び翼のある羽根車円盤を示している。An impeller disk with dents and wings is shown. 図2のA−B断面図を示している。FIG. 3 is a cross-sectional view taken along a line AB in FIG. 2. 本発明に係る他のプロペラ送風機を示す図である。It is a figure which shows the other propeller air blower which concerns on this invention.

Claims (4)

回転軸(3)を中心に回転駆動されると共に流路を内側に制限する羽根車円盤(2)によって吸引される空気の実質上軸方向への流出のためのプロペラ送風機であって、
翼流入端(22)と翼流出端との間の翼領域において流れ方向(30)に湾曲する翼(1)を備え、
前記各翼(1)は、縦へ延びる牡蠣の貝殻の形状に形成され、その端部(20)が貫入(6)の形式で前記羽根車円盤(2)に接続され、他端の自由端(21)が半径方向へ外側に、及び流れ方向における軸方向成分とともに半径距離が増加して延び、前記羽根車円盤(2)の回転駆動の周方向(5)へ向かって湾曲することを特徴とするプロペラ送風機。
A propeller blower for substantially axially flowing out air sucked by an impeller disk (2) that is driven to rotate about a rotating shaft (3) and restricts a flow path to the inside;
A wing (1) curved in the flow direction (30) in the wing region between the wing inflow end (22) and the wing outflow end;
Each wing (1) is formed in the shape of an oyster shell extending vertically, and its end (20) is connected to the impeller disk (2) in the form of penetration (6), and the free end at the other end (21) extends radially outward and with an axial component in the flow direction extending with increasing radial distance and curved toward the circumferential direction (5) of the rotational drive of the impeller disk (2). Propeller blower.
前記運搬翼(1)は、前記回転軸(3)近傍に、回転方向のベクトルに略垂直に配置され、前記翼の流入端(22)は、内側から外側端部にかけて前記回転方向(5)に凹んで湾曲することを特徴とする請求項1記載のプロペラ送風機。   The carrying wing (1) is arranged in the vicinity of the rotation axis (3) and substantially perpendicular to the vector of the rotation direction, and the inflow end (22) of the wing extends from the inner side to the outer end portion in the rotation direction (5). The propeller blower according to claim 1, wherein the propeller blower is recessed and curved. 前記翼の半径方向への内部の延びは、前記回転軸(3)への半径距離を有し、歯元ライン(6)は、前記回転方向における回転軸(3)の傍を通って位置することを特徴とする請求項1又は請求項2記載のプロペラ送風機。   The radial extension of the wing has a radial distance to the rotation axis (3), and the tooth root line (6) is located beside the rotation axis (3) in the rotation direction. The propeller blower according to claim 1 or 2, wherein the propeller blower is provided. 歯元ライン(6)の手前の領域において、窪み(4)が前記羽根車円盤(2)に形成されることを特徴とする請求項1から請求項3のいずれか1項記載のプロペラ送風機。   The propeller blower according to any one of claims 1 to 3, wherein a recess (4) is formed in the impeller disk (2) in a region in front of the tooth root line (6).
JP2006527430A 2004-03-01 2005-02-25 Propeller blower and shell propeller Pending JP2007506037A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE200410010457 DE102004010457B3 (en) 2004-03-01 2004-03-01 Propeller fan with shell propeller for blowing air has each blade in form of shell bowl extending longitudinally
DE200410043618 DE102004043618A1 (en) 2004-09-07 2004-09-07 Propeller blower for axial flow of gas or liquid media blows out suctioned air using impeller disc with convex shell blades which extend in a radial direction from the disc
PCT/EP2005/001976 WO2005083270A1 (en) 2004-03-01 2005-02-25 Propeller blower, shell propeller

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JP2007506037A true JP2007506037A (en) 2007-03-15

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JP2006527430A Pending JP2007506037A (en) 2004-03-01 2005-02-25 Propeller blower and shell propeller

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US (1) US20080050239A1 (en)
EP (1) EP1721080A1 (en)
JP (1) JP2007506037A (en)
WO (1) WO2005083270A1 (en)

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DE2951775A1 (en) * 1978-12-26 1980-07-03 Nissan Motor COOLING FAN
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EP1721080A1 (en) 2006-11-15
US20080050239A1 (en) 2008-02-28

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