US2077959A - Fan blade - Google Patents
Fan blade Download PDFInfo
- Publication number
- US2077959A US2077959A US36468A US3646835A US2077959A US 2077959 A US2077959 A US 2077959A US 36468 A US36468 A US 36468A US 3646835 A US3646835 A US 3646835A US 2077959 A US2077959 A US 2077959A
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- United States
- Prior art keywords
- blade
- fan
- fan blade
- blades
- insulating material
- 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.)
- Expired - Lifetime
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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
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/38—Blades
- F04D29/388—Blades characterised by construction
Definitions
- This invention relates to ventilating fans of the type intended for use where the blades of a fan are subjected to severe abrasive or corrosive o in unevenness of operation and distortion of the entire structure.
- Another object of the invention lies in the provision of a process by which a thin coating of corrosive-resistant material can be fastened to a fan blade by means of a process similar to the process by which certain metals are electroplated on other materials.
- a still further object of the invention is to provide means whereby a thin coating of corrosive and abrasive resistant material can be securely attached to the blades and hub of a fan in such a manner that the coating material will become an integral part of the structure, thereby resisting the forces tending to remove the protective covering.
- a further object of the invention is to provide a fan blade wherein a perforated core member of metal or other suitable material is employed to shape the blade structure, and a thin layer of insulating material is electroplated on the core member in such a manner that the insulating material flows through the coremember to form insulating rivets extending through the core member to tie the insulating material securely to the fan blades on opposite sides thereof.
- Another object of the invention is to provide a moulded fan blade wherein a small core member conforming to the shape of the finished fan blade, or formed of a metal stamping of any desired shape may be employed to reinforce the structure of 'the moulded fan blade.
- a still further object of the invention is to provide a reinforced fan blade, wherein tension members such as strands of wire are moulded in the fan blade to absorb the centrifugal and torsional forces to which the fan blade is subjected;
- Figure 1 is a plan the construction of partly in section showing the blade
- Figure 2 is a view Figure 1;
- FIG. 3 is Figure 1;
- Figure 4 is a view of a portion of a fan blade, showing a modified form of the method of securing the insulating material to the fan blade;
- Figure'5 is a cross section on the'line 5-5 of Figure 4, showing one desirable manner of securing the insulating material to the metal core of the fan blades;
- Figure 6 is a view similar to Figure 5 showing a modified form
- Figure '7 is a view similar to Figure 4 showing a moulded fan blade, wherein a small apertured metal core is employed;
- FIG. 8 is a view taken on the line 8-8 of Figure "I;
- Figure 9 is a view similar 'to Figure 7, wherein an apertured metal stamping is employed as a rigidifying core;
- Figure 10 is a view taken on the line Ill-l0 of Figure 9;
- Figure 11 is a view similar to Figure 9, showing a moulded. fan blade wherein a core member of drawn wire, or other suitable material is employed;
- a fan blade having a hub section I0, and a. bladed section E2.
- the illustrated blade is of the constant velocity type wherein a uniform quantity of air 5 is delivered over the entire working area of the fan blade. It will be understood, however, that this invention may be applied to other types of fan blades than the one illustrated.
- the fan blade 82 is provided with a plurality of- -10 apertures M, extending through the blade section.
- a thin layer of colloidal solution of latex I6 is fixed to the outer surface of the core and hub 15 structure by means of a process similar to the process whereby certain metals are electroplated on the surface of other metals.
- the hub and cores of the blades of the fan are assembled. The structure is then sand-blasted to remove all foreign matter from the surface of the core, and to roughen the surface of the cores and hub so that the electroplated solution may more securely grip and fuse with the core member to form 25 an integral structure.
- the structure After the structure has been sand-blasted it is placed in a drier, wherein it is subjected to a temperature of a suitable degree such as from 185 to 190 Fahrenheit for a suitable period to adequately dry the structure 30 preparatory to the next operation. It has been found from experiment that approximately two hours is adequate to properly prepare the structure for the electroplating operation.
- the structure After the structure has been thus suitably pre- 35 pared, it is placed in an electroplating tank, wherein a solution of a suitable consistency of a colloidal solution of latex is transferred from the negative or cathode terminal to the positive 1 or anode terminal.
- a solution of a suitable consistency of a colloidal solution of latex is transferred from the negative or cathode terminal to the positive 1 or anode terminal.
- inelec- 40 troplating rubber the article to be plated is positioned on the positive or anode terminal
- electroplating metal the article to be plated is positioned on the negative or cathode terminal.
- the structure to be treated is subjected to the 45 electroplating process for a period of time dependent upon the desired thickness of the .protective covering. It has been found from experiment that approximately of an inch of latex will be deposited upon the structure in approximately thirty minutes. The length of time during which the structure is subjected to the electroplating bath is therefore entirely 7 de-' pendent upon the desired thickness
- the structure is removed from the electroplating bath, and is subjected to a steam vulcanizing process wherein 60 the structure is subjected to both pressure and temperature to dry the colloidal solution of latex, and to harden it to the desired degree. It has been found from experiment that a temperature of approximately 375 Fahrenheit, and a pres- 65 sure of approximately 165 pounds will harden the colloida'lsolution of latex to a proper degree for certain types of workin approximately six to eight hours.
- FIG. 4 to 6 illustrate other desirable embodiments wherein longitudinally extending grooves or slots 29 are formed in the surface of blade structure l2 so that the electro- 30 plated material may flow into the grooves to securely lock the insulating material to the blades.
- Transversely extending grooves 22 may also be positioned in the blades to relieve against centrifugal forces to which the blade is subjected.
- the longitudinally extending grooves 20 are tapered, pointing toward the trailing edge of the blade, and that the transversely extending grooves are also tapered and are pointed toward the outer end of the blade section. This disposition of the grooves tends to cause the insulating material E6 to cling more tightly to the core member it to the centrifugal, torsional and frictional forces acting on the blade during normal operation thereof.
- are formeddn theshape of ways which cause the insulating material 16 to become securely locked in the core member i2.
- FIG. 8 shows a moulded blade structure wherein a small rigidifying core 30 of airfoil cross section is employed to stiffen and strengthen the blades.
- a moulded blade structure of a composition of rubber or other suitable material is provided.
- - blade structure is formed with a suitable airfoil shaped core member having apertures formed therein to permit the moulded material to flow through the core member, thereby forming insulating rivets extending through the 'core structure to securely tie the insulating material together on opposite sides of the core member.
- an insulating material of suitable consistency is moulded upon the core member at a temperature and pressilre'to produce a blade structure of the proper hardness consistent with the requirements of the finished product. After the structure has been moulded it is removed from the mould and subjected to a polishing and waxing operation to obtain the desired friction coefiicient.
- a core member 40 formed of a metal stamping or other suitable material is positioned in the mould. It will be observed that in this design it is not necessary that the core member to conform to the airfoil section of the finished product.
- apertures 52 extend through the core member it to securely tie the insulating material together on opposite sides of the core member. Insulating material 46 of rubber or other suitable composi tion is moulded around the core member M in a manner similar to that discussed in connection with the embodiment illustrated'in Figures 7 and 8.
- the core structure comprises several strands of drawn wire 50 interposed within the moulded material 52 of the fan blade.
- the core structure may extend through both blades of the fan, passing around the hub structure to securely tie the blades together, and to aid in ab-' sorbing centrifugal and other forces to which the blades are subjected during normal operation.
- the moulded material may be moulded to the core member direct. In order to secure a more perfect bond between the insulating material and the core member, however, I prefer to electroplate a thin coating of insulating material to the core member before it is subjected to the moulding operation.
- this invention provides a fan blade wherein insulating material is securely fixed to or formed integral with the core structure, to form a fan structure adapted to resist corrosive action, and to minimize abrasion, where the fan is employed in industrial or chemical plants, or in places where dust or grit is mixed with the air driven by the fan, which would impede the operation of the fan, and injure a conventional metal fan.
- a metal fan blade having a plurality of longitudinally and transversely extending undercut grooves formed in the surface of the metal blade, the pointed ends of the grooves project-' ing toward the trailing and tip ends of the blade respectively, a protective covering of a colloidal solution of latex electroplated on the metal blade and engaging in the grooves to securely tie the protective covering to the blade and to cause it to cling more tightly thereto during normal operation of the fan when the blade is subjected to centrifugal, torsional and frictional forces.
- a metal fan blade having a plurality of Iongitudinally extending undercut grooves formed in the surface of the metal blade, the pointed ends of the grooves projecting toward the trailing edge of the blade, a protective covering of a colloidal solution of latex electroplated on the metal blade and engaging the grooves to securely lock the protective covering to the blade and to cause it to cling thereto during normal operation of the fan when the blade is subjected to centrifugal, torsional and frictional forces.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
Aprii 20, 1937. M sMn-H, JR 2,077,959
FAN BLADE Filed Aug. 16, 1935 3 Sheets-Sheet l INVENTOR. Mew/1m 4 5mm, Jr
ATTORNEY April 20, 1937. M. A. SMITH, JR
FAN BLADE Filed Aug. 16, 1935 3 Sheets-Sheet 2 III/ll IN VEN TOR. Mira/14114 JM/m, Je BY f g ATTORNEY.
April 20, 1937. M. A. SMITH, JR
FAN BLADE Filed Aug. 16, 1935 I5 Sheets-Sheet 3 IN V EN TOR. MI/JJHHLL Fl. 5mm, J2 BY M A TTORNEY Patented pr. 20, 1937 PATENT Marshall A. Smit Jr., South Bend, Ind, as-
signor to Bendix Products Corporation, South Bend, Ind., a corporation of Indiana Application August 16, 1935', Serial No. 36,468 2 Claims. (or. 170-159 This invention relates to ventilating fans of the type intended for use where the blades of a fan are subjected to severe abrasive or corrosive o in unevenness of operation and distortion of the entire structure.
It is therefore an object of this invention to provide a ventilating fan wherein the blades and hub of the fan are provided with a protective covering of rubber Or other corrosive-resistant material.
Another object of the invention lies in the provision of a process by which a thin coating of corrosive-resistant material can be fastened to a fan blade by means of a process similar to the process by which certain metals are electroplated on other materials.
A still further object of the invention is to provide means whereby a thin coating of corrosive and abrasive resistant material can be securely attached to the blades and hub of a fan in such a manner that the coating material will become an integral part of the structure, thereby resisting the forces tending to remove the protective covering.
A further object of the invention is to provide a fan blade wherein a perforated core member of metal or other suitable material is employed to shape the blade structure, and a thin layer of insulating material is electroplated on the core member in such a manner that the insulating material flows through the coremember to form insulating rivets extending through the core member to tie the insulating material securely to the fan blades on opposite sides thereof.
Another object of the invention is to provide a moulded fan blade wherein a small core member conforming to the shape of the finished fan blade, or formed of a metal stamping of any desired shape may be employed to reinforce the structure of 'the moulded fan blade.
A still further object of the invention is to provide a reinforced fan blade, wherein tension members such as strands of wire are moulded in the fan blade to absorb the centrifugal and torsional forces to which the fan blade is subjected;
Other desirable features and combinations of this invention relate to forming longitudinally and transversely extending grooves in the surcore member to securely tie the rial to the fan blade on opposite sides thereof;
face of the core of the fan blade to-aid in securing the insulating material to the fan; forming a plurality of apertures through the core member to which the insulating material is secured to form insulating rivets extending through the insulating mateand'to provide an insulated fan blade wherein the skin friction of the blade is minimized.
Other objects and advantages of this invention will be apparent from the following detailed description, considered in connection with the accompanying drawings, submitted for purposes of illustration only and not intended to define the scope of the invention, reference being had for that purpose to the s bjoined claims:
In the drawings, wherein similar reference characters refer to similar parts throughout the several views:
Figure 1 is a plan the construction of partly in section showing the blade;
Figure 2 is a view Figure 1;
Figure 3 is Figure 1;
Figure 4 is a view of a portion of a fan blade, showing a modified form of the method of securing the insulating material to the fan blade;
Figure'5 is a cross section on the'line 5-5 of Figure 4, showing one desirable manner of securing the insulating material to the metal core of the fan blades;
Figure 6 is a view similar to Figure 5 showing a modified form;
Figure '7 is a view similar to Figure 4 showing a moulded fan blade, wherein a small apertured metal core is employed;
Figure 8 is a view taken on the line 8-8 of Figure "I;
Figure 9 is a view similar 'to Figure 7, wherein an apertured metal stamping is employed as a rigidifying core;
Figure 10 is a view taken on the line Ill-l0 of Figure 9;
Figure 11 is a view similar to Figure 9, showing a moulded. fan blade wherein a core member of drawn wire, or other suitable material is employed; and
taken on the line 2-2 of a view taken on the line 3-3 of Figure 11.-
Referring more particularly to Figure 1, there is shown a fan blade of the general type disclosed in my copending application Serial No. 5,691, filed February 9, 1935. In this embodi-,
. ment of the invention there is shown a fan blade having a hub section I0, and a. bladed section E2. The illustrated blade is of the constant velocity type wherein a uniform quantity of air 5 is delivered over the entire working area of the fan blade. It will be understood, however, that this invention may be applied to other types of fan blades than the one illustrated. As shown the fan blade 82 is provided with a plurality of- -10 apertures M, extending through the blade section.
In the preferred embodiment of the invention a thin layer of colloidal solution of latex I6 is fixed to the outer surface of the core and hub 15 structure by means of a process similar to the process whereby certain metals are electroplated on the surface of other metals. To prepare the structure for latex electroplating process the hub and cores of the blades of the fan are assembled. The structure is then sand-blasted to remove all foreign matter from the surface of the core, and to roughen the surface of the cores and hub so that the electroplated solution may more securely grip and fuse with the core member to form 25 an integral structure. After the structure has been sand-blasted it is placed in a drier, wherein it is subjected to a temperature of a suitable degree such as from 185 to 190 Fahrenheit for a suitable period to adequately dry the structure 30 preparatory to the next operation. It has been found from experiment that approximately two hours is adequate to properly prepare the structure for the electroplating operation.
7 After the structure has been thus suitably pre- 35 pared, it is placed in an electroplating tank, wherein a solution of a suitable consistency of a colloidal solution of latex is transferred from the negative or cathode terminal to the positive 1 or anode terminal.- It will be noted that inelec- 40 troplating rubber, the article to be plated is positioned on the positive or anode terminal, whereas in electroplating metal, the article to be plated is positioned on the negative or cathode terminal. The structure to be treated is subjected to the 45 electroplating process for a period of time dependent upon the desired thickness of the .protective covering. It has been found from experiment that approximately of an inch of latex will be deposited upon the structure in approximately thirty minutes. The length of time during which the structure is subjected to the electroplating bath is therefore entirely 7 de-' pendent upon the desired thickness of the insu- 55 lating material.
After the desired thickness of insulating material has been deposited, the structure is removed from the electroplating bath, and is subjected to a steam vulcanizing process wherein 60 the structure is subjected to both pressure and temperature to dry the colloidal solution of latex, and to harden it to the desired degree. It has been found from experiment that a temperature of approximately 375 Fahrenheit, and a pres- 65 sure of approximately 165 pounds will harden the colloida'lsolution of latex to a proper degree for certain types of workin approximately six to eight hours.
After the structure has been vulcanized it is 7 removed from the vulcanizer, and is subjected to a bufiing and polishing operation. A soft bufier or polisher is employed, and after the structure has been suitably polished it is'waxed to decrease the skin friction of the blades and hub. 75 Ithas been found that a fan blade prepared tend through the blade section.
in accordance with the process indicated above will possess a skin friction approximating that of the best metal blade structure now in use.
One of the greatest difficulties encountered in electroplating insulating material on fan blades 5 is to secure the insulating material to the fan blades in such a manner that centrifugal and torsional forces will not cause it to crack or slip on the fan blades. The upper surface of the blade as viewed in Figure 2 is subjected to the 10 greatest stress because of the fact that the upper surface of the blades is subjected to negative pressure developed in the normal operation of the fan. The lower surface of the blades of the fan is subjected to pressure which tends to urge the covering material l6 toward the blades l2. In the embodiment of the invention illustrated in Figures 1 and 2 a plurality of apertures M ex- When the insulating material I6 is electroplated on the blade structure it flows through the apertures M to form, in effect, rubber rivets i8 joining the in sulating material I6 on opposite sides to the blade section #0.
Other expedients may be resorted to to securely tie the insulating material l6 to the core member E2 of the blades. Figures 4 to 6 illustrate other desirable embodiments wherein longitudinally extending grooves or slots 29 are formed in the surface of blade structure l2 so that the electro- 30 plated material may flow into the grooves to securely lock the insulating material to the blades. Transversely extending grooves 22 may also be positioned in the blades to relieve against centrifugal forces to which the blade is subjected. 30
In the embodiment illustrated in Figure 5, it will be observed that the longitudinally extending grooves 20 are tapered, pointing toward the trailing edge of the blade, and that the transversely extending grooves are also tapered and are pointed toward the outer end of the blade section. This disposition of the grooves tends to cause the insulating material E6 to cling more tightly to the core member it to the centrifugal, torsional and frictional forces acting on the blade during normal operation thereof.
In the embodiment of Figure 6, the grooves 2| are formeddn theshape of ways which cause the insulating material 16 to become securely locked in the core member i2.
The embodiment of the invention illustrated in Figures '7 and 8 shows a moulded blade structure wherein a small rigidifying core 30 of airfoil cross section is employed to stiffen and strengthen the blades. In thisembodiment of the invention, a moulded blade structure of a composition of rubber or other suitable material is provided. The
- blade structure is formed with a suitable airfoil shaped core member having apertures formed therein to permit the moulded material to flow through the core member, thereby forming insulating rivets extending through the 'core structure to securely tie the insulating material together on opposite sides of the core member. In this embodiment of the invention an insulating material of suitable consistency is moulded upon the core member at a temperature and pressilre'to produce a blade structure of the proper hardness consistent with the requirements of the finished product. After the structure has been moulded it is removed from the mould and subjected to a polishing and waxing operation to obtain the desired friction coefiicient.
In the embodiment illustrated in Figures 9 and 10, a core member 40 formed of a metal stamping or other suitable material is positioned in the mould. It will be observed that in this design it is not necessary that the core member to conform to the airfoil section of the finished product. In this embodiment of the invention apertures 52 extend through the core member it to securely tie the insulating material together on opposite sides of the core member. Insulating material 46 of rubber or other suitable composi tion is moulded around the core member M in a manner similar to that discussed in connection with the embodiment illustrated'in Figures 7 and 8.
In the embodiment illustrated in Figures 11 and 12, the core structure comprises several strands of drawn wire 50 interposed within the moulded material 52 of the fan blade. The core structure may extend through both blades of the fan, passing around the hub structure to securely tie the blades together, and to aid in ab-' sorbing centrifugal and other forces to which the blades are subjected during normal operation. In the embodiments of the invention illustrated in Figures '7 to 12, the moulded material may be moulded to the core member direct. In order to secure a more perfect bond between the insulating material and the core member, however, I prefer to electroplate a thin coating of insulating material to the core member before it is subjected to the moulding operation. a
It will be observed that this invention provides a fan blade wherein insulating material is securely fixed to or formed integral with the core structure, to form a fan structure adapted to resist corrosive action, and to minimize abrasion, where the fan is employed in industrial or chemical plants, or in places where dust or grit is mixed with the air driven by the fan, which would impede the operation of the fan, and injure a conventional metal fan.
While the invention has been described with particular reference to certain preferred embodiments thereof, it is understood that the scope of the invention is not limited to the details illustrated and described nor otherwise than by the terms of the following claims.
I claim:
1. A metal fan blade having a plurality of longitudinally and transversely extending undercut grooves formed in the surface of the metal blade, the pointed ends of the grooves project-' ing toward the trailing and tip ends of the blade respectively, a protective covering of a colloidal solution of latex electroplated on the metal blade and engaging in the grooves to securely tie the protective covering to the blade and to cause it to cling more tightly thereto during normal operation of the fan when the blade is subjected to centrifugal, torsional and frictional forces.
2. A metal fan blade having a plurality of Iongitudinally extending undercut grooves formed in the surface of the metal blade, the pointed ends of the grooves projecting toward the trailing edge of the blade, a protective covering of a colloidal solution of latex electroplated on the metal blade and engaging the grooves to securely lock the protective covering to the blade and to cause it to cling thereto during normal operation of the fan when the blade is subjected to centrifugal, torsional and frictional forces.
MARSHALL A. SMITH, JR.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US36468A US2077959A (en) | 1935-08-16 | 1935-08-16 | Fan blade |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US36468A US2077959A (en) | 1935-08-16 | 1935-08-16 | Fan blade |
Publications (1)
Publication Number | Publication Date |
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US2077959A true US2077959A (en) | 1937-04-20 |
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Application Number | Title | Priority Date | Filing Date |
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US36468A Expired - Lifetime US2077959A (en) | 1935-08-16 | 1935-08-16 | Fan blade |
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Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2423700A (en) * | 1943-06-16 | 1947-07-08 | Marquette Metal Products Co | Propeller blade |
US2473665A (en) * | 1946-09-20 | 1949-06-21 | William W K Van Nort | Propeller |
US2498348A (en) * | 1947-05-29 | 1950-02-21 | Jr Frank E Thompson | Marine propeller |
US2555314A (en) * | 1946-07-10 | 1951-06-05 | William L Buckley | Mud driven apparatus for treating mud |
DE757651C (en) * | 1937-12-05 | 1953-10-12 | Siemens Schuckertwerke A G | Wing for fan |
DE917808C (en) * | 1950-07-06 | 1954-09-13 | Mauz & Pfeiffer | Impeller for blower, vacuum cleaner and. like |
US3241493A (en) * | 1964-05-04 | 1966-03-22 | Cascade Corp | Pump impeller |
US3248082A (en) * | 1965-08-19 | 1966-04-26 | Whitfield Lab Inc | Reinforced gas-turbine blade or vane |
US3744931A (en) * | 1971-07-26 | 1973-07-10 | Logic Syst Corp Ltd | Brine resistant propeller |
US3918838A (en) * | 1974-01-04 | 1975-11-11 | Dunham Bush Inc | Metal reinforced plastic helical screw compressor rotor |
US20080106867A1 (en) * | 2006-05-29 | 2008-05-08 | Sony Corporation | Fan motor device and electronic apparatus |
WO2010097225A1 (en) * | 2009-02-26 | 2010-09-02 | W & S Management Gmbh & Co Kg | Fan blade and fastening means therefor |
WO2012035008A3 (en) * | 2010-09-16 | 2012-05-24 | Grundfos Holding A/S | Axial flow impeller |
EP2295816A3 (en) * | 2009-07-31 | 2016-10-05 | Nuovo Pignone S.p.A. | Impeller Cover And Method |
-
1935
- 1935-08-16 US US36468A patent/US2077959A/en not_active Expired - Lifetime
Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE757651C (en) * | 1937-12-05 | 1953-10-12 | Siemens Schuckertwerke A G | Wing for fan |
US2423700A (en) * | 1943-06-16 | 1947-07-08 | Marquette Metal Products Co | Propeller blade |
US2555314A (en) * | 1946-07-10 | 1951-06-05 | William L Buckley | Mud driven apparatus for treating mud |
US2473665A (en) * | 1946-09-20 | 1949-06-21 | William W K Van Nort | Propeller |
US2498348A (en) * | 1947-05-29 | 1950-02-21 | Jr Frank E Thompson | Marine propeller |
DE917808C (en) * | 1950-07-06 | 1954-09-13 | Mauz & Pfeiffer | Impeller for blower, vacuum cleaner and. like |
US3241493A (en) * | 1964-05-04 | 1966-03-22 | Cascade Corp | Pump impeller |
US3248082A (en) * | 1965-08-19 | 1966-04-26 | Whitfield Lab Inc | Reinforced gas-turbine blade or vane |
US3744931A (en) * | 1971-07-26 | 1973-07-10 | Logic Syst Corp Ltd | Brine resistant propeller |
US3918838A (en) * | 1974-01-04 | 1975-11-11 | Dunham Bush Inc | Metal reinforced plastic helical screw compressor rotor |
US20080106867A1 (en) * | 2006-05-29 | 2008-05-08 | Sony Corporation | Fan motor device and electronic apparatus |
WO2010097225A1 (en) * | 2009-02-26 | 2010-09-02 | W & S Management Gmbh & Co Kg | Fan blade and fastening means therefor |
CN102333960A (en) * | 2009-02-26 | 2012-01-25 | W&S管理公司 | Fan blade and fastening means therefor |
US9856888B2 (en) | 2009-02-26 | 2018-01-02 | W & S Management Gmbh & Co. Kg | Fan blade and attaching means therefor |
EP2295816A3 (en) * | 2009-07-31 | 2016-10-05 | Nuovo Pignone S.p.A. | Impeller Cover And Method |
WO2012035008A3 (en) * | 2010-09-16 | 2012-05-24 | Grundfos Holding A/S | Axial flow impeller |
US9435349B2 (en) | 2010-09-16 | 2016-09-06 | Grundfos Holding A/S | Axial flow impeller |
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