US1495222A - Method of manufacturing impellers - Google Patents
Method of manufacturing impellers Download PDFInfo
- Publication number
- US1495222A US1495222A US414225A US41422520A US1495222A US 1495222 A US1495222 A US 1495222A US 414225 A US414225 A US 414225A US 41422520 A US41422520 A US 41422520A US 1495222 A US1495222 A US 1495222A
- Authority
- US
- United States
- Prior art keywords
- blades
- blade
- buckets
- forming
- face
- 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
Links
- 238000004519 manufacturing process Methods 0.000 title description 5
- 238000003801 milling Methods 0.000 description 8
- 238000000034 method Methods 0.000 description 6
- 239000000463 material Substances 0.000 description 4
- 238000010276 construction Methods 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23C—MILLING
- B23C3/00—Milling particular work; Special milling operations; Machines therefor
- B23C3/16—Working surfaces curved in two directions
- B23C3/18—Working surfaces curved in two directions for shaping screw-propellers, turbine blades, or impellers
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
- Y10T29/49325—Shaping integrally bladed rotor
Definitions
- FIG. 1 is a face view of an impeller unit, constructed in accordance with the present invention.
- Figure 2 is a similar view, with the reenforcing ring removed,
- Figure 3 is a detail sectional view on an enlarged scale and taken on the line 3-3 80 of Figure 1,
- Figure 4 is a vertical sectional view through the unit, with the retaining ring removed, and
- Figure 5 is a detail face view of a section of the body, illustrating the blades or buckets at different stages of their formation.
- the member consists of a hub 6 having an outstanding integral and outwardly ta ered body 7, one face 8 of which is pre erably curved, as illustrated. From the terminal portion of the curved face project laterally disposed buckets 9 arranged in the form of an annular series, and integral with the body 7. These buckets are provided with integral lugs or stems 10 that pass through openings in a retaining or reentorcing ring 11 abutted against their outer ends. the said stems or lugs being upset, as illusi rated in Figure B reference part icularly to Figure I. it will benoted that the inner faces of the blades or buckets are concave. and each is on the arc of a circle that embraces the adjacent bucket. The 0pposite faces of the bucket are convex, and each of said convex faces constitutes the arc of a circle that surrounds the bucket and extends between said bucket and the adjacent bucket.
- the method of forming these buckets is disclosed more particularly in Figure 5.
- the body 7 is initially formed with a lateral continuous flange 12, into which are drilled spaced holes 13.
- a hollow milling cutter is then utilized, as indicated at 14 to cut the concave face of each blade, this milling cutter giving the proper form tothe face,
- each blade 18 formed by a hollow milling cutter, indicated at 15 of less diameter than the milling cutter 14.
- the milling cutter 14 operates around or encloses the material of the adjacent blade.
- buckets or blades can be made inte a1 with the bod that carries them, and wi l more successful y retain their shape and position than those which are attached to the rotating carrier.
- the buckets constructed as above described are properly sha ed to successfully operate, and are suificient y strong to withstand the various influences to which they are subjected in operation.
- the method of forming im ller blades integrally on a rotary body w ich consists in forming the body with a flange thereon, and forming out of said flange a series of blades b cuttin a convex face on one side of the b ade wit a hollow cutter that encircles said blade and passes between it and the adjacent blade and b cutting an opposite concave face with a ollow cutter that encircles the adjacent blade.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Crushing And Pulverization Processes (AREA)
Description
May 27, 1924. 1,495,222
. Cl E4 Cl AF?K METHOD OF MANUFACTURING IMFELLERS FllPd Och 2 1920 2 Sheets-Sheet 1 O. E. CLARK v May 27, 1924. 1,49 22 whim M Patented May 27, 1924.
UNITED STATES PATENT OFFICE.
OMAR E. CLARK, OF DENVER, COLORADO, ASSIGNOR TO THEJDENVER ROCK DRILL MANUFACTURING COMPANY, OF DENVER. COLORADO, A CORPORATION OF DELA- WARE.
METHOD OF MANUFACTURING IMPELLERS.
Application filed October 2, 1920. Serial No. 414,225.
To all whom it may roar-rm.
Be it known that I. ()MA]: E. CLARK, a citizen of the l'nited States, residing at Denver. in the county' of Denver and State 50f Colorado. have invented certain new and useful Improvements in Methods of Manufacturing Impellers. of which the following is a specification.
In the construction of high speed rotary 10 impellers, such as are used in air compressors and t er apparatus of an analogous character, a very serious difiiculty has always been experienced in securing the blades or buckets to the rotary body or support. It
is would appear that the most satisfactory method is to make the blades integralwith the wheel, and it is the primary object of the present invention to produce a structure of this type in which the blades are not only so integral, at are properly proportioned and formed for the work to be accomplished.
In the accompanying drawings Figure 1 is a face view of an impeller unit, constructed in accordance with the present invention,
Figure 2 is a similar view, with the reenforcing ring removed,
Figure 3 is a detail sectional view on an enlarged scale and taken on the line 3-3 80 of Figure 1,
Figure 4 is a vertical sectional view through the unit, with the retaining ring removed, and
Figure 5 is a detail face view of a section of the body, illustrating the blades or buckets at different stages of their formation.
The device illustrated in the accompanying drawings is primarily intended as an impeller for a rotary compressor, but it will be obvious to those skilled in the art, that the invention is not limited to devices for this specific use, and may be successfully employed for any type of rotary member having buckets, being especially useful, as heretofore indicated, for those operated at hi h speed.
The member, as disclosed, consists of a hub 6 having an outstanding integral and outwardly ta ered body 7, one face 8 of which is pre erably curved, as illustrated. From the terminal portion of the curved face project laterally disposed buckets 9 arranged in the form of an annular series, and integral with the body 7. These buckets are provided with integral lugs or stems 10 that pass through openings in a retaining or reentorcing ring 11 abutted against their outer ends. the said stems or lugs being upset, as illusi rated in Figure B reference part icularly to Figure I. it will benoted that the inner faces of the blades or buckets are concave. and each is on the arc of a circle that embraces the adjacent bucket. The 0pposite faces of the bucket are convex, and each of said convex faces constitutes the arc of a circle that surrounds the bucket and extends between said bucket and the adjacent bucket.
The method of forming these buckets is disclosed more particularly in Figure 5. The body 7 is initially formed with a lateral continuous flange 12, into which are drilled spaced holes 13. A hollow milling cutter is then utilized, as indicated at 14 to cut the concave face of each blade, this milling cutter giving the proper form tothe face,
and surrounding the material of which said blade is formed, while operating between it and the material for the ad'acent blade. The convex face of each blade 18 formed by a hollow milling cutter, indicated at 15 of less diameter than the milling cutter 14. The milling cutter 14 operates around or encloses the material of the adjacent blade. These two cutters leave the portions designated 16, which are then removed by suitable tools, and the stems 10 are then produced by the employment of a hollow milling cutter that cuts down the ends of the blade blanks. The blades or buckets are thus completed and are ready to receive the reenforcing ring that is placed in position, and the parts either welded or upset, as shown.
As a consequence, buckets or blades can be made inte a1 with the bod that carries them, and wi l more successful y retain their shape and position than those which are attached to the rotating carrier. Moreover tests and experience have demonstrated that the buckets constructed as above described, are properly sha ed to successfully operate, and are suificient y strong to withstand the various influences to which they are subjected in operation.
From the foregoing, it is thought that the construction, operation and many advantages of the herein described invention will be a parent to those skilled in the art, without urther description, and it will be understood that various changes in the size, shape,
proportion and minor details of construe-A what I c aim as new, and desire to secure by Letters Patent, is e 1. The method of forming impeller blades integrally on a rotary body which consists in forming the bod with a flange thereon, and forming out 0 said flange a series of blades having their opposite faces respectively concave and convex by cutting each blade with a pair of hollow milling cutters, one of which encircles the blade being cutand the other encircling the bladeadjacent to that being cut.
2. The method of forming im ller blades integrally on a rotary body w ich consists in forming the body with a flange thereon, and forming out of said flange a series of blades b cuttin a convex face on one side of the b ade wit a hollow cutter that encircles said blade and passes between it and the adjacent blade and b cutting an opposite concave face with a ollow cutter that encircles the adjacent blade.
3. The method of forming integral buckets or blades on an impeller or like rotary member, which consists in forming a flange on the side of the member, drilling spaced holes into said flange, and cutting out of the material between said holes blades having opposite convex and concave faces, by emp oying milling cutters that respectively encircle the blade being cut and the next adj acent blade.
In testimony whereof I aflix my signature in the presence of two witnesses.
OMAR E. CLARK.
Witnesses:
SULLINA W. Jormson, ELIZABETH Jomrson.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US414225A US1495222A (en) | 1920-10-02 | 1920-10-02 | Method of manufacturing impellers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US414225A US1495222A (en) | 1920-10-02 | 1920-10-02 | Method of manufacturing impellers |
Publications (1)
Publication Number | Publication Date |
---|---|
US1495222A true US1495222A (en) | 1924-05-27 |
Family
ID=23640514
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US414225A Expired - Lifetime US1495222A (en) | 1920-10-02 | 1920-10-02 | Method of manufacturing impellers |
Country Status (1)
Country | Link |
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US (1) | US1495222A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2486619A (en) * | 1946-09-07 | 1949-11-01 | Hoover Co | Plastic fan for suction cleaners |
US3130481A (en) * | 1959-03-14 | 1964-04-28 | Ahlen Karl Gustav | Method of manufacturing a blade wheel |
EP0193181A2 (en) * | 1985-03-01 | 1986-09-03 | Arthur Pfeiffer Vakuumtechnik Wetzlar GmbH | Highly stable blade wheels for turbomolecular pumps |
US5443362A (en) * | 1994-03-16 | 1995-08-22 | The Hoover Company | Air turbine |
US5860188A (en) * | 1995-08-11 | 1999-01-19 | The Hoover Company | Carpet extractor |
-
1920
- 1920-10-02 US US414225A patent/US1495222A/en not_active Expired - Lifetime
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2486619A (en) * | 1946-09-07 | 1949-11-01 | Hoover Co | Plastic fan for suction cleaners |
US3130481A (en) * | 1959-03-14 | 1964-04-28 | Ahlen Karl Gustav | Method of manufacturing a blade wheel |
EP0193181A2 (en) * | 1985-03-01 | 1986-09-03 | Arthur Pfeiffer Vakuumtechnik Wetzlar GmbH | Highly stable blade wheels for turbomolecular pumps |
FR2578287A1 (en) * | 1985-03-01 | 1986-09-05 | Pfeiffer Vakuumtechnik | LARGE STABILITY DISKS FOR TURBOMOLECULAR PUMPS AND PROCESS FOR PRODUCING SUCH DISCS |
EP0193181A3 (en) * | 1985-03-01 | 1988-07-27 | Arthur Pfeiffer Vakuumtechnik Wetzlar Gmbh | Highly stable blade wheels for turbomolecular pumps |
US5443362A (en) * | 1994-03-16 | 1995-08-22 | The Hoover Company | Air turbine |
US5860188A (en) * | 1995-08-11 | 1999-01-19 | The Hoover Company | Carpet extractor |
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