WO1998054470A1 - A fan with outer band - Google Patents

A fan with outer band Download PDF

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Publication number
WO1998054470A1
WO1998054470A1 PCT/CN1997/000125 CN9700125W WO9854470A1 WO 1998054470 A1 WO1998054470 A1 WO 1998054470A1 CN 9700125 W CN9700125 W CN 9700125W WO 9854470 A1 WO9854470 A1 WO 9854470A1
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WO
WIPO (PCT)
Prior art keywords
fan
paddle
wheel edge
resistance
wheel
Prior art date
Application number
PCT/CN1997/000125
Other languages
French (fr)
Chinese (zh)
Inventor
Wei Han
Original Assignee
Wei Han
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 Wei Han filed Critical Wei Han
Priority to AU51148/98A priority Critical patent/AU5114898A/en
Publication of WO1998054470A1 publication Critical patent/WO1998054470A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D21/00Pump involving supersonic speed of pumped fluids
    • 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
    • F04D29/326Rotors specially for elastic fluids for axial flow pumps for axial flow fans comprising a rotating shroud

Definitions

  • the present invention relates to a paddle fan mainly used for actively performing work on a fluid, and is mainly used for the propulsion of an aircraft, a ship, a fluid transfer such as an axial flow pump, an axial compressor and a fluid blowing such as a fan. , Ventilator, etc.
  • the existing paddle fan generally consists of a rotating shaft and paddle leaves fixed on it. Its main working area is 0.7 leaf lengths. From 0.7 leaf length to the leaf end, it is the fastest moving area. According to area, this area occupies about half of the entire rotation area of the pulp fan. According to the generated force, this area accounts for Above 75%, in this area, due to the loss of the blade end, the pressure difference between the positive pressure surface and the negative pressure surface of the blade decreases, and it drops to almost 0 at the blade end. A fast position, but it is the position where the maximum effective power contribution of the ordinary paddle fan is zero, and the blade end is seriously lost.
  • the object of the present invention is to provide a pulp fan, which can make up for the above-mentioned disadvantages of the existing pulp fans.
  • the paddle fan of the present invention has a rotating shaft on which paddle leaves are mounted, and is characterized in that a round wheel edge is fixed by the blade ends of the paddle leaves.
  • a hole can be made on the wheel edge of the paddle fan as required.
  • all products are axisymmetric in shape.
  • the paddle fan of the present invention has small rotation resistance, concentrated force, and good directivity, which completely eliminates the blade end loss, expands the main working area of the blade from 0.7 blade length to the blade end, and converts the real work on the rotating shaft into fluid flow.
  • the efficiency of flow work has been increased by more than 40%.
  • the rotational force of the shaft is efficiently converted to thrust under supersonic conditions. Its efficiency is about 60% higher than that of turbojet engines, while also improving the structural strength.
  • the drawing is a schematic diagram of a paddle fan of the present invention.
  • the paddle of the present invention has a rotating shaft (2), and a paddle (3) is mounted on the paddle.
  • the angle is 45. It is placed in a thin cylinder with a corresponding inner diameter, that is, the rim (1), which is welded to the blade end of each paddle (3).
  • the width of the rim (1) is 0.1 meters and the inner diameter It is 0.8 meters, and its plate surface is parallel to the rotation axis (2) and surrounds the latter.
  • the wheel rim (1) is a revolving body with a very smooth surface, which is concentric with the axis (2) that drives it.
  • the wheel edge (1) When working, the wheel edge (1) only generates frictional resistance in the direction of rotation, and the power lost by the latter accounts for only a few thousandths to a few percent of the output power of the pulp fan. And as the speed increases, this part of the loss will be relatively cut back. Experiments have shown that the resistance of this product is less than that of ordinary pulp fans of the same size.
  • the product of the present invention is axially symmetrical in shape or the generated force is basically symmetrical, so the forces acting on the wheel rim (1) in the radial direction cancel each other, and the resultant force is zero (except for gravity). Because the paddle (3), the wheel edge (1) and the hub (2) are connected into multiple triangles and I-shaped shapes. Therefore, the structural strength, stability and bearing capacity of the pulp fan are greatly enhanced. Compared with ordinary propellers, the thickness of the blade can be reduced, which not only reduces weight but also reduces losses.
  • V the average air velocity.
  • the tip speed is set.
  • the V tip is 550 m / s, which is the speed of the compressor blade tip reached by the American IHPTET plan. The effect of gas compressibility is not considered in the calculations.
  • C is the coefficient of resistance
  • P is the density of air
  • V is the loss of V
  • M is the area of the wheel edge

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

Abstract

A fan includes a rotating shaft (2) and a polarity of blades (3) mounted on said shaft (2), characterized in that an annular outer band (1) is mounted on the top of said blades (3). The fan can be worked in low resistant, concentrated effort and centralized direction. The top lost can be eliminated and main working area can be extended to the top of said blades. The power transform efficiency from the shaft to air flow can be increased in 40 % or higher, and the power transform efficiency in supersonic condition can be increased in 60 % or higher. The structure strength can also be improved.

Description

有轮边的浆扇 本发明涉及一种主要用于主动对流体作功的浆扇, 主要用于飞行器、 船只的推进、 流体的输送如轴流泵, 轴流压气机和流体的吹送如风扇、 通 风机等。  The present invention relates to a paddle fan mainly used for actively performing work on a fluid, and is mainly used for the propulsion of an aircraft, a ship, a fluid transfer such as an axial flow pump, an axial compressor and a fluid blowing such as a fan. , Ventilator, etc.
现有的浆扇一般由转轴及固定在其上的浆叶所组成。 它的主要工作区 在 0.7个叶长处, 从 0.7叶长处到叶端是运动速度最快的区域, 按面积, 该 区域占整个浆扇旋转面积的一半左右, 按产生的作用力, 该区域占 75 %以 上, 普通的螺旋浆在这一区域, 由于叶端损失, 浆叶正压面与负压面的压 差反而下降, 在叶端处几乎降到 0 . 叶端是浆叶运动速度最快的位置, 但 却是普通浆扇损耗最大有效功率贡献为零的位置, 叶端损失严重, 因此现 有浆扇的旋转能量转化为流体轴向动能的效率较低, 并且还有浆叶厚, 原 材料用量大, 叶端正负压叶面之间以及与周围介质之间均无稳固界面, 易 受外界条件影响的缺点.  The existing paddle fan generally consists of a rotating shaft and paddle leaves fixed on it. Its main working area is 0.7 leaf lengths. From 0.7 leaf length to the leaf end, it is the fastest moving area. According to area, this area occupies about half of the entire rotation area of the pulp fan. According to the generated force, this area accounts for Above 75%, in this area, due to the loss of the blade end, the pressure difference between the positive pressure surface and the negative pressure surface of the blade decreases, and it drops to almost 0 at the blade end. A fast position, but it is the position where the maximum effective power contribution of the ordinary paddle fan is zero, and the blade end is seriously lost. Therefore, the efficiency of converting the rotational energy of the existing paddle fan to the axial kinetic energy of the fluid is low, and the paddle thickness is also low. , The large amount of raw materials, no positive interface between the positive and negative pressure at the blade end and between the surrounding media and the surrounding medium, vulnerable to the disadvantages of external conditions.
本发明的目的是提供一种浆扇, 它能弥补现有浆扇的上述不足。  The object of the present invention is to provide a pulp fan, which can make up for the above-mentioned disadvantages of the existing pulp fans.
本发明的浆扇, 有一旋 轴, 上面装有浆叶, 其特征是通过各浆叶的 叶端固定一圆形轮边。  The paddle fan of the present invention has a rotating shaft on which paddle leaves are mounted, and is characterized in that a round wheel edge is fixed by the blade ends of the paddle leaves.
按照本发明使用场合, 可根据需要在浆扇的轮边上开孔。  According to the application occasion of the present invention, a hole can be made on the wheel edge of the paddle fan as required.
按照本发明的浆扇, 所有产品在形状上是轴对称的。  According to the paddle fan of the present invention, all products are axisymmetric in shape.
本发明的桨扇旋转阻力小, 作用力集中, 方向性好, 完全消除了叶端 损失, 使浆叶的主要工作区从 0.7 叶长处扩展到叶端, 将转轴上真实功转 换成流体中通流功的效率提高了 40 %以上,在超音速条件下将轴的旋转力 高效地转换为推力, 其效率比涡喷涡扇发动机高约 60 %, 同时还提高了结 构强度.  The paddle fan of the present invention has small rotation resistance, concentrated force, and good directivity, which completely eliminates the blade end loss, expands the main working area of the blade from 0.7 blade length to the blade end, and converts the real work on the rotating shaft into fluid flow. The efficiency of flow work has been increased by more than 40%. The rotational force of the shaft is efficiently converted to thrust under supersonic conditions. Its efficiency is about 60% higher than that of turbojet engines, while also improving the structural strength.
下面通过实施例和附图说明本发明。  The invention will be described below by means of examples and drawings.
附图为本发明的浆扇结构示意图。  The drawing is a schematic diagram of a paddle fan of the present invention.
实施例 1 本发明的浆扃有旋转轴( 2 ) , 上面装有浆叶( 3 ) , 转 角为 45。 , 将其置于冲压成型的具有相应内径的薄圆筒即轮边( 1 ) 内, 后者焊接在各浆叶( 3 ) 的叶端上. 轮边( 1 ) 的宽度为 0.1米, 内径为 0.8米, 其板面与旋转轴( 2 )平行, 环绕后者一團。 轮边( 1 )是一个表 面十分光滑的回转体, 它与带动它旋转的轴( 2 ) 同心。 工作时轮边( 1 ) 在旋转方向上只产生摩擦阻力, 后者损耗的功率只占浆扇输出功率的千分 之凡到百分之几. 而且随转速的提高, 这部分损耗还会相对减少。 实验已 经证明, 本产品的阻力小于相同尺寸的普通浆扇的阻力。 Embodiment 1 The paddle of the present invention has a rotating shaft (2), and a paddle (3) is mounted on the paddle. The angle is 45. It is placed in a thin cylinder with a corresponding inner diameter, that is, the rim (1), which is welded to the blade end of each paddle (3). The width of the rim (1) is 0.1 meters and the inner diameter It is 0.8 meters, and its plate surface is parallel to the rotation axis (2) and surrounds the latter. The wheel rim (1) is a revolving body with a very smooth surface, which is concentric with the axis (2) that drives it. When working, the wheel edge (1) only generates frictional resistance in the direction of rotation, and the power lost by the latter accounts for only a few thousandths to a few percent of the output power of the pulp fan. And as the speed increases, this part of the loss will be relatively cut back. Experiments have shown that the resistance of this product is less than that of ordinary pulp fans of the same size.
本发明的产品在形状上是轴对称的或产生的作用力基本对称, 所以径 向作用于轮边( 1 )上的力相互抵消, 合力为零(重力除外) 。 由于浆叶 ( 3 )、 轮边( 1 )和轮毂( 2 )连成了多个三角形和工字形。 因而大大 地增强了本浆扇的结构强度、 稳定性和承载能力。 与普通螺旋浆比较, 可 以减薄浆叶厚度, 这样既减轻了重量, 又降低损耗.  The product of the present invention is axially symmetrical in shape or the generated force is basically symmetrical, so the forces acting on the wheel rim (1) in the radial direction cancel each other, and the resultant force is zero (except for gravity). Because the paddle (3), the wheel edge (1) and the hub (2) are connected into multiple triangles and I-shaped shapes. Therefore, the structural strength, stability and bearing capacity of the pulp fan are greatly enhanced. Compared with ordinary propellers, the thickness of the blade can be reduced, which not only reduces weight but also reduces losses.
下面从理论上按已知的下述公式计算一下本实施例以大气为介质的静 态推力 F :  The following theoretically calculates the static thrust F of the present embodiment using the atmosphere as a medium:
F = PAV平 V平  F = PAV flat V flat
式中 P为空气密度 0.125公斤秒 2/米 4 , A为轮形浆扇的面积 0.5米 2 (浆扇的直径为 0.8米), V平为空气平均流速. 在本实施例设叶尖速度 V 尖为 550米 /秒, 这是美国 IHPTET计划达到的压气机叶尖的速度。 计算中 未考虑气体可压缩性的影响。 在本实施例中叶尖速度最大, 中心为零, 因 此用上述公式计 算 F时其中的速度应取其平均值,可以证明在此情况下 V 平 2 = 0.5V尖 2 · 于是得出 Where P is the air density of 0.125 kg s 2 / m 4 , A is the area of the paddle fan 0.5 m 2 (the diameter of the paddle fan is 0.8 m), and V is the average air velocity. In this embodiment, the tip speed is set. The V tip is 550 m / s, which is the speed of the compressor blade tip reached by the American IHPTET plan. The effect of gas compressibility is not considered in the calculations. In this embodiment, the tip speed is the largest, and the center is zero. Therefore, when calculating F using the above formula, the speed should be the average value. It can be proved that V flat 2 = 0.5 V tip 2 in this case.
F = 0.5PAV尖 2 = 9453 (公斤力) F = 0.5PAV tip 2 = 9453 (kg force)
再用已知的平板阻力公式 {参照许维德著《流体力学》 (国防工业出版 社 79年 12月出版) P253 P259摩擦力阻力计算公式 }计算本装置轮边产生 的阻力 Z, 以便估计轮边损耗占输出功率的百分数:  Then use the known plate resistance formula {refer to Xu Weide's "Fluid Mechanics" (published in December 79, National Defense Industry Press) P253 P259 friction resistance calculation formula} to calculate the resistance Z generated by the wheel edge of the device in order to estimate the wheel edge loss Percentage of output power:
Z=0.5CPWM  Z = 0.5CPWM
式中 C为阻力系数, P为空气密度, V为 V失, M为轮边面积, 轮 边展开即为一长方形板, 其长 L = 2πΚ = 2.5米, 它的内外表面积之和 Μ 0.5平方米. 上式中的阻力系数可由下式求出 Where C is the coefficient of resistance, P is the density of air, V is the loss of V, M is the area of the wheel edge, and the wheel edge is a rectangular plate with a length of L = 2πκ = 2.5 meters, and the sum of its internal and external surface areas, M 0.5 square meters. The resistance coefficient in the above formula can be obtained from the following formula
C = 0455 =0.0021 C = 0455 = 0.0021
(lgR)2.58  (lgR) 2.58
其中 R为雷 数可由下式求出:  Where R is the thunder number can be obtained by the following formula:
R = ~~― ·~ = 2 5 x 550 =94827586 R = ~~ ― · ~ = 2 5 x 550 = 94827586
1.45 x 0.00001 1.45 x 0.00001  1.45 x 0.00001 1.45 x 0.00001
于是  So
Ζ = 0.5CPV尖 2 · Μ = 0.5 X 0.0021 χ 0.125 χ 5502 χ 0.5 = 19.85 (公斤力) Ζ = 0.5CPV tip 2 · Μ = 0.5 X 0.0021 χ 0.125 χ 550 2 χ 0.5 = 19.85 ( kgf)
如不考虑力矩因素, 则轮边阻力与总推力之比:  If the torque factor is not considered, the ratio of wheel edge resistance to total thrust:
阻力 /推力 =—=0.0021  Resistance / Thrust =-= 0.0021
9453  9453
从以上粗略估算不难得出结论, 即使轮边的阻力比以上估计值大到 10 倍, 它的阻力也不 是总推力的 2.1 %而已.  It is not difficult to conclude from the above rough estimation, even if the resistance of the wheel is 10 times larger than the above estimate, its resistance is not only 2.1% of the total thrust.
实旅例 2 在水槽中, 用直径 150MM的浆扇以海水为介质做试验, 浆 扇的轮边用 0.5ΜΜ厚金属冲压制成, 无烊缝, 浆叶叶端与轮边用锡焊固 定, 轮边宽 20ΜΜ, 轮形浆扇转速 1400转 /分, 据此可以得出 V 尖 = 10.8 米, 于是用下述公式得以算出  Practical Example 2 In a water tank, a paddle fan with a diameter of 150MM was tested with seawater as the medium. The paddle's rim was stamped from 0.5MM thick metal without quilting. The paddle blade end and the rim were fixed by soldering. With a wheel edge width of 20 MM and a wheel-shaped paddle fan speed of 1400 rpm, the V tip = 10.8 meters can be obtained from this, so it can be calculated using the following formula
F = 0.5PAV尖 2 = 107 (公斤力) F = 0.5PAV tip 2 = 107 (kg force)
其中 Ρ为海水密度 104公斤秒 2/米 4, Α为浆扇的面积, 在本实施例 中 A = π(^^ )2=0.0177米 2 Wherein the sea water density 104 kg Ρ 2 sec / m 4, Α fan area of the pulp, in this embodiment, A = π (^^) 2 = 0.0177 m 2
下面仿照实施例 1计算出本浆扇的轮边产生的阻力 Ζ :  The following is an example of calculating the resistance Z generated by the wheel edge of the pulp fan in accordance with Example 1:
Ζ = 0.5CPV尖 2Μ = 0.388公斤力, Z = 0.5CPV tip 2 Μ = 0.388 kgf,
在本实施例中铃 的长度 L = π · 0.15米= 0.47米,轮边面积 Μ = 2 X 0.47米 X 0.02米 = 0,0188米 2. In this embodiment, the length of the bell is L = π · 0.15 m = 0.47 m, and the wheel area M = 2 X 0.47 m X 0.02 m = 0,0188 m 2 .
最后, 仿照实裤例 1估算出轮边阻力与总推力之比  Finally, following the example of real pants, the ratio of wheel resistance to total thrust is estimated
阻力 /推力 = ^ = 0 , 0036  Resistance / Thrust = ^ = 0, 0036
107  107
这就是说, 在介质为海水的情况下, 轮边的推力只占总推力的 3.6 % 。 本发明的浆扇用作风扇时, 在轮边( 1 )上可开有风扇减压孔( 4 ) 。 上述附 ¾和实施例仅作为说明本发明之用, 任何本领域的技术人员可 在本发明权利要求的保护范围之内作出工艺上及技术上的修改, 如浆扇和 轮边的尺寸改变, 及它们之间采用胶接或整体铸造, 或轮边与轴向有夹角 等等, 均不超出本发明的保护范闺. That is to say, when the medium is seawater, the wheel thrust only accounts for 3.6% of the total thrust. When the pulp fan of the present invention is used as a fan, a fan decompression hole (4) may be opened on the wheel edge (1). The above-mentioned appendixes and embodiments are only used to illustrate the present invention. Any person skilled in the art can make technical and technical modifications within the protection scope of the claims of the present invention, such as the size changes of the pulp fan and the wheel edge. And glued or integrally cast between them, or the angle between the wheel edge and the axial direction, etc., are not beyond the scope of the present invention.

Claims

1. 一种有轮边的浆扇, 有一旋转轴( 2 ) , 上面装有浆叶( 3 ) , 其特征 是通过各浆叶( 3 ) 的叶端固定一圆形轮边( 1 ) 。 1. A paddle fan with a wheel edge, which has a rotating shaft (2) and is equipped with paddle leaves (3), which is characterized in that a round wheel edge (1) is fixed by the blade ends of the paddle leaves (3).
2. 如权利要求 1所述的浆扇, 其特征是所述的轮边( 1 )为一表面动力光 滑的圆形回转体, 它与旋转轴( 2 ) 同心。  2. The paddle fan according to claim 1, characterized in that the wheel edge (1) is a circularly rotating body with a smooth and dynamic surface, which is concentric with the rotation axis (2).
3. 如权利要求 1 所述的浆扇, 其特征是所述的轮边( 1 ) 上有減压孔 ( 4 ) .  3. The paddle fan according to claim 1, characterized in that the wheel edge (1) is provided with a pressure relief hole (4).
PCT/CN1997/000125 1997-05-28 1997-11-14 A fan with outer band WO1998054470A1 (en)

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CN97233251U CN2304777Y (en) 1997-05-28 1997-05-28 Fan with wheel style paddles
CN97233251.0 1997-05-28

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EP0168594A1 (en) * 1984-06-27 1986-01-22 Canadian Fram Limited Improved axial fan
US4642023A (en) * 1985-07-29 1987-02-10 Rockwell International Corporation Vented shrouded inducer
CN87205786U (en) * 1987-03-30 1988-06-29 青岛市气割机械厂 Impeller of self-priming vortex pumping machinery
US4871298A (en) * 1987-07-09 1989-10-03 Ecia - Equipments Et Composants Pour L'industrie Automoblie Falciform blade for a propeller and its application in particular in motorized fans for automobiles
US4900229A (en) * 1989-05-30 1990-02-13 Siemens-Bendix Automotive Electronic Limited Axial flow ring fan
WO1991002164A1 (en) * 1989-08-11 1991-02-21 Airflow Research And Manufacturing Corporation High efficiency fan
CN2125748U (en) * 1992-05-08 1992-12-23 傅玉源 Fan for automobile radiator

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2732999A (en) * 1956-01-31 stalker
US2856118A (en) * 1952-07-24 1958-10-14 Gen Motors Corp Blading assembly
US2872998A (en) * 1954-03-30 1959-02-10 American Radiator & Standard Acoustical silencer
SU775396A1 (en) * 1979-01-18 1980-10-30 Сумский филиал Специального конструкторского бюро по созданию воздушных и газовых турбохолодильных машин Axial compressor for pumping contaminated gases
EP0168594A1 (en) * 1984-06-27 1986-01-22 Canadian Fram Limited Improved axial fan
US4642023A (en) * 1985-07-29 1987-02-10 Rockwell International Corporation Vented shrouded inducer
CN87205786U (en) * 1987-03-30 1988-06-29 青岛市气割机械厂 Impeller of self-priming vortex pumping machinery
US4871298A (en) * 1987-07-09 1989-10-03 Ecia - Equipments Et Composants Pour L'industrie Automoblie Falciform blade for a propeller and its application in particular in motorized fans for automobiles
US4900229A (en) * 1989-05-30 1990-02-13 Siemens-Bendix Automotive Electronic Limited Axial flow ring fan
WO1991002164A1 (en) * 1989-08-11 1991-02-21 Airflow Research And Manufacturing Corporation High efficiency fan
CN2125748U (en) * 1992-05-08 1992-12-23 傅玉源 Fan for automobile radiator

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AU5114898A (en) 1998-12-30
CN2304777Y (en) 1999-01-20

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