US832083A - Manufacture of turbine-vanes. - Google Patents

Manufacture of turbine-vanes. Download PDF

Info

Publication number
US832083A
US832083A US29089705A US1905290897A US832083A US 832083 A US832083 A US 832083A US 29089705 A US29089705 A US 29089705A US 1905290897 A US1905290897 A US 1905290897A US 832083 A US832083 A US 832083A
Authority
US
United States
Prior art keywords
vanes
mandrel
manufacture
turbine
cylinder
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
Application number
US29089705A
Inventor
Carl Roth
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Melms & Pfenninger GmbH
Melms & Pfenninger Ges mbH
Original Assignee
Melms & Pfenninger Ges mbH
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 Melms & Pfenninger Ges mbH filed Critical Melms & Pfenninger Ges mbH
Priority to US29089705A priority Critical patent/US832083A/en
Application granted granted Critical
Publication of US832083A publication Critical patent/US832083A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/04Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/49336Blade making
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12188All metal or with adjacent metals having marginal feature for indexing or weakened portion for severing
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12229Intermediate article [e.g., blank, etc.]
    • Y10T428/12264Intermediate article [e.g., blank, etc.] having outward flange, gripping means or interlocking feature
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12229Intermediate article [e.g., blank, etc.]
    • Y10T428/12271Intermediate article [e.g., blank, etc.] having discrete fastener, marginal fastening, taper, or end structure
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12389All metal or with adjacent metals having variation in thickness
    • Y10T428/12403Longitudinally smooth and symmetrical

Definitions

  • My invention relates to the manufacture UNITED STATES PATENT oFFIon.
  • Patented Oct. 2 recs. I
  • FIG. 1 shows a mandrel, blank, and die-ring.
  • FigF13 shows a mandrel, blank, and die-ring.
  • 'gs. 4 and 5 show, respectively, a cross-section of the mandrel and plan view of the 6 shows vertical and horizontal sections of the comIpleted i 7 and 8 show vertical sectionsofit fini slled varies, the last three figures being on a large sca e.
  • the blank used in the process is formed of metal pieces-for instance, cast or stamped and eit er (plain or cup-shaped, as shown in Figs. 1 an 2. These disks are forced, b means of a suitably-shaped mandrel, throng a die-ring of suitably-shaped cross-section.
  • the inner sides of the vanes are formed by the mandrel according to its coutour, while at the same time the corresponding outer vane profiles are made by the inner ring-sun face, as illustrated in Figs. 3, 4, and 5.
  • the disk or blank I) is placed on or under the mandrel a, and thereupon the mandrel is forced in the direction of the arrows, thus forcing the blank throu h the fixed die-ring c.
  • the inner diameter of the die is sli htly smaller than the outer diameter of the b ank.
  • the blank is in this way com ressed about the mandrel and shaped as in cated in dotthickene through a suitably s ted lines, Fig. 3, while at the same time the blank assumes the sha e of the vane. This process can'be repeate several times, a diering of smaller diameter bein used at each operation until a sleeve of the ength desired a is obtained.
  • Fi 6 shows a finished vane-sleeve, from whic after a hole a has been bored or stamped out in the center of the base part It finished vanes can be obtained by cutting through on the lines'x.
  • the projection f formed from the base It andserving as a means for securing the vane or for use as a distance-piecefls shown;
  • b meansof a mandrel having a series of Iongitudinal curved surfaces, through a corresponding suitably-fluted die-rin and finally cutting longitudinally throug the cylinder so formed to produce aseries of vanes corresponding in number to the faces on the mandrel substantially as set forth.
  • a connected assemble e of turbinevanes formed from a metal lank stamped between a shaped mandrel and corresponding dies consisting of longitudinal curved sections connected together at their longitudinal edges in the form of a cylinder, and an inwardly-extending flange at the base of said cylinder substantially as set forth.
  • a connected assembla e of turbinevanes formed from a metal ilank stamped between a shaped mandrel and corresponding dies consisting of longitudinal curved sections connected together at their longitudinal edges-in the form of a cylinder, thickened roots on said sections and an inwardlyextending flange at the base of said cylinder substantially as set forth.

Description

PATENTED OCT. 2, 1906.
0'. ROTH. MANUFACTURE OF TURBINE VANE$.
APPLICATION FILED 10130.3. 1905.
Fig.6.
enables vanes of any desired shape to be vanes before they are divided up;
specification. My invention relates to the manufacture UNITED STATES PATENT oFFIon.
CARL ROTH, OF MUNICH, GERMANY, ASSIGNOR TO MELMS & PFEN-- NINGER, GESELLSCHAFT Ml'l BESCHRANKTER HAFTUNG, OF
MUNICH-HIRSCHAU, GERMANY.
A MANUFACTURE OF TURBINE-MANES;
Application filed December 8,
Specification of Letters Patent.
Patented Oct. 2, recs. I
1906. suninojzaasa'l. 4
To all whom it may concern:
Be it known that I, CARL ROTH, engineer, a citizen of the Republic of Switzerland, and a resident of Munich, Miihlbauerstrasse 2, Bavaria, Germany, have invented a certain new and useful Improvement in the Methods of the Manufacture of Turbine-vanes; and I do hereb declare the following to be a full, clear, an exact description of the invention, such as will enable others skilled in the art to which it appertains to make and use the same, reference being had to the accompanying drawings, and to letters of reference marked thereon, which'form a part of this of turbine-vanes; and my improved method manufactured with great accuracy, each vane being at the same time provided with a projection serving for securing it or as adistance-piece.
The accompanying drawings illustrative of the invention s ow in Figures 1 and 2 two forms of blanks used in the manufacture of the vanes. FigF13 shows a mandrel, blank, and die-ring. 'gs. 4 and 5 show, respectively, a cross-section of the mandrel and plan view of the 6 shows vertical and horizontal sections of the comIpleted i 7 and 8 show vertical sectionsofit fini slled varies, the last three figures being on a large sca e.
' The blank used in the process is formed of metal pieces-for instance, cast or stamped and eit er (plain or cup-shaped, as shown in Figs. 1 an 2. These disks are forced, b means of a suitably-shaped mandrel, throng a die-ring of suitably-shaped cross-section. The inner sides of the vanes are formed by the mandrel according to its coutour, while at the same time the corresponding outer vane profiles are made by the inner ring-sun face, as illustrated in Figs. 3, 4, and 5. The disk or blank I) is placed on or under the mandrel a, and thereupon the mandrel is forced in the direction of the arrows, thus forcing the blank throu h the fixed die-ring c. The inner diameter of the die is sli htly smaller than the outer diameter of the b ank. The blank is in this way com ressed about the mandrel and shaped as in cated in dotthickene through a suitably s ted lines, Fig. 3, while at the same time the blank assumes the sha e of the vane. This process can'be repeate several times, a diering of smaller diameter bein used at each operation until a sleeve of the ength desired a is obtained.
Fi 6 shows a finished vane-sleeve, from whic after a hole a has been bored or stamped out in the center of the base part It finished vanes can be obtained by cutting through on the lines'x.
' In ig. 7 the projection f, formed from the base It andserving as a means for securing the vane or for use as a distance-piecefls shown;
By ma the end of the mandrel of suitable sha e t e vanes can be made with a root portion of anydesired sha e, as shown at gin Fig. 8. i
aving thus described my invention, what I claim as new, and desire to secure byLetters Patent of the United States of America, is
1. The methodof manufacturing'turbinevanes consisting of forcing a metal blank, by means of a mandrel having a series of faces corresponding in shape to the desired contour of the inner surfaces of the vanes,
inner faces corresponding to the outer sur- 8o through a suitably-shaped die-ring having faces of the vanes and finally cutting longitudinally through the cylinder so formed to produce a series of vanes corresponding in number to the faces on they mandrel substantially as set forth.
2.. The method of manufacturing turbinevanes consisting of forcing a metal, blank,
b meansof a mandrel having a series of Iongitudinal curved surfaces, through a corresponding suitably-fluted die-rin and finally cutting longitudinally throug the cylinder so formed to produce aseries of vanes corresponding in number to the faces on the mandrel substantially as set forth.
3. The method of manufacturin turbinevanes consisting of forcing a metafiilank, by means of a'mandrel having a series of faces corresponding in shape to the desired con tour of the inner surfaces of the vanes, ped die-ring having inner faces correspon ing to the outer surfaces of the vanes, removmgthe central portion of the base of thecylinder of'connected vanes so formed and finally longitudinally through the cylinder to produce a series of vanes corresponding in number to the faces on the mandrel substantially as set forth.
4. The method of manufacturin turbinevanes consisting of forcing a metal lank, by means of a mandrel having a series of longitudinal curved surfaces, through a corresponding suitably-fluted die-rlng, removing the central portion of the base of the cylinder of connected vanes so formed and finally cutting longitudinally through the cylinder to produce a series of vanes corresiponding in number to the faces on the manrel substantially as set forth.
5. A connected assemble e of turbinevanes formed from a metal lank stamped between a shaped mandrel and corresponding dies consisting of longitudinal curved sections connected together at their longitudinal edges in the form of a cylinder, and an inwardly-extending flange at the base of said cylinder substantially as set forth.
6; A connected assembla e of turbinevanes formed from a metal ilank stamped between a shaped mandrel and corresponding dies consisting of longitudinal curved sections connected together at their longitudinal edges-in the form of a cylinder, thickened roots on said sections and an inwardlyextending flange at the base of said cylinder substantially as set forth.
In testimony that I claim the foregoing as my invention I have signed my name in presence of tWo subscribing Witnesses.
CARL ROTH.
Witnesses:
ULYSSES J. BYWATER, ABRAHAM SCHLESINGER.
US29089705A 1905-12-08 1905-12-08 Manufacture of turbine-vanes. Expired - Lifetime US832083A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US29089705A US832083A (en) 1905-12-08 1905-12-08 Manufacture of turbine-vanes.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US29089705A US832083A (en) 1905-12-08 1905-12-08 Manufacture of turbine-vanes.

Publications (1)

Publication Number Publication Date
US832083A true US832083A (en) 1906-10-02

Family

ID=2900558

Family Applications (1)

Application Number Title Priority Date Filing Date
US29089705A Expired - Lifetime US832083A (en) 1905-12-08 1905-12-08 Manufacture of turbine-vanes.

Country Status (1)

Country Link
US (1) US832083A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2430368A (en) * 1946-04-12 1947-11-04 Moore Drop Forging Company Apparatus and method for drawing and broaching socket wrenches
US4271240A (en) * 1977-12-27 1981-06-02 Braun Engineering Company Lobed preparatory blank for cold extruding a cup-shaped article with hollow polygonal interior

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2430368A (en) * 1946-04-12 1947-11-04 Moore Drop Forging Company Apparatus and method for drawing and broaching socket wrenches
US4271240A (en) * 1977-12-27 1981-06-02 Braun Engineering Company Lobed preparatory blank for cold extruding a cup-shaped article with hollow polygonal interior

Similar Documents

Publication Publication Date Title
US2849788A (en) Method and apparatus for making hollow blades
US4031601A (en) Method of fabricating and mounting a fiberglass fan blade
US832083A (en) Manufacture of turbine-vanes.
US1360558A (en) Method of producing interiorly-cylindrical surfaces having an exact diameter
US1925721A (en) Method of making yoke ends
JP2004243515A (en) Method of manufacturing hollow member, and method of manufacturing hollow turbine blade preform
US1869478A (en) Method of forming a propeller
US3058202A (en) Method of making hollow blades for compressors, turbines, and the like
US1738567A (en) Method of forging steel-gate valve bodies
US325692A (en) Hub-band
US1706703A (en) Method of production of turbine blandes
US2703022A (en) Die-cutting apparatus and method of producing same
US2673709A (en) Compounded airfoil blade structure and method of making same
US651841A (en) Manufacture of brushes.
JPS5951222B2 (en) Manufacturing method of yoke for rotating electric machines
US2638021A (en) Crown drill and method of making same
US1701547A (en) Method of shaping gtjttljs g bulbs foe
US916968A (en) Nozzle for elastic-fluid turbines.
US3416211A (en) Method of punch-forming windows in bearing retainers
US1893711A (en) Method of making valve casings
US1278746A (en) Process of making odometer-wheels.
JPS6123545A (en) Working method of valve-shaped forming body
US520194A (en) Die for the manufacture of crown gear-wheels
US373348A (en) George evans
US3747182A (en) Method of fabricating a hollow turbine blade having an insert therein