WO1998054470A1 - A fan with outer band - Google Patents
A fan with outer band Download PDFInfo
- 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
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- fan
- paddle
- wheel edge
- resistance
- wheel
- Prior art date
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
- F04D21/00—Pump involving supersonic speed of pumped fluids
-
- 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
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/325—Rotors specially for elastic fluids for axial flow pumps for axial flow fans
- F04D29/326—Rotors 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
Claims
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU51148/98A AU5114898A (en) | 1997-05-28 | 1997-11-14 | A fan with outer band |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN97233251U CN2304777Y (en) | 1997-05-28 | 1997-05-28 | Fan with wheel style paddles |
CN97233251.0 | 1997-05-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1998054470A1 true WO1998054470A1 (en) | 1998-12-03 |
Family
ID=5202964
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/CN1997/000125 WO1998054470A1 (en) | 1997-05-28 | 1997-11-14 | A fan with outer band |
Country Status (3)
Country | Link |
---|---|
CN (1) | CN2304777Y (en) |
AU (1) | AU5114898A (en) |
WO (1) | WO1998054470A1 (en) |
Citations (11)
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 |
-
1997
- 1997-05-28 CN CN97233251U patent/CN2304777Y/en not_active Expired - Fee Related
- 1997-11-14 AU AU51148/98A patent/AU5114898A/en not_active Abandoned
- 1997-11-14 WO PCT/CN1997/000125 patent/WO1998054470A1/en active Application Filing
Patent Citations (11)
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 |
Also Published As
Publication number | Publication date |
---|---|
AU5114898A (en) | 1998-12-30 |
CN2304777Y (en) | 1999-01-20 |
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