US1417029A - Rotor - Google Patents

Rotor Download PDF

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Publication number
US1417029A
US1417029A US310003A US31000319A US1417029A US 1417029 A US1417029 A US 1417029A US 310003 A US310003 A US 310003A US 31000319 A US31000319 A US 31000319A US 1417029 A US1417029 A US 1417029A
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US
United States
Prior art keywords
vanes
rotor
stock
discs
bands
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
US310003A
Inventor
Axel W Carlson
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.)
CARLING TURBINE BLOWER Co
Original Assignee
CARLING TURBINE BLOWER CO
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 CARLING TURBINE BLOWER CO filed Critical CARLING TURBINE BLOWER CO
Priority to US310003A priority Critical patent/US1417029A/en
Application granted granted Critical
Publication of US1417029A publication Critical patent/US1417029A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/021Blade-carrying members, e.g. rotors for flow machines or engines with only one axial stage
    • 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
    • Y10T29/4932Turbomachine making
    • Y10T29/49321Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member

Definitions

  • This vinvention relates to a rotor for a steam turbine or other similar machine.
  • the bronze vanes in such rotors are sube ject to excessive wear and it is desirable to use hard drawn bar stock for these parts. It is the object of my invention to provide a rotor construction in which the vanes are separately formed of bar stock, and in which they are securelyheld against accidental displacement when in use. Y
  • each vane with non-circular projections at each end by which it may be secured in perforated -concentric bands provided for the. purpose.
  • This construction holds the vanes 1n the desired spaced relation and effectively prevents relative angular displacement.
  • Another obj ect of my invention is to provide a firm and satisfactory support for the 3 in Fig. l;
  • Fig. 4 shows themethod of forming the vanes fromlb-ar stock
  • Fig. 5 is a detail view of a portion of one of the bands.
  • my improved rotor in its preferred form comprises a hub 10, side plates or discs 11, inner and outer concentric bands 13 and 14, and a plurality of separate vanes 15.
  • the vanes 15 are preferably formed from bar stock drawn Specification of Letters Patent.
  • This stock may be fed through a press or other machine by which successive notches 16, (Fig. 4) are formed on the opposite edges of the stock. After these notches are formed, the stock is severed along the dotted lines a to form a plurality of separate vanes, each having a short upper projection 17 and a longer lower proj ection 18.
  • the bands 13 and 14 are provided with a succession of openings of perforations 2O (Fig. 5) of irregular outline corresponding to the cross section of the projections 17 and 18.
  • the vanes are then assembled between the bands 13 and 14 and the short upper projections 17 areheaded down or riveted on the band 14.
  • a plurality of holes 21 are formed in the discs 11, so disposed that they each lie be tween two adjacent vanes. After the parts are assembled, a drill is inserted in each ⁇ hole 21 and is advanced between the corresponding vanes, thus forming notches in their adjacent faces through which a rivet 22 may be inserted. Additional rivets 23 secure the discs firmly to the hub 10. W'hen the rivets 22 and 23 are securely headed, a very rigid structure results in which accidental displacements of the vanes is practically impossible. Furthermore, the noncircular section of the projections 17 and 18 prevents angular displacement of the vanes.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Description

AXEL CARLSON, or WORCESTER, ivrAsSnCrr'U-snTTs, Assienon 'To cantine TURBINE BLOWER Co.,` .or WORCESTER., T/mssaorrusnrrs A CORPORATION OF MASSACHUSETTS.
ROTOR.
Appncatin filed July 11,
T0 all w hom t may concern Be it known that I, AXEL W. CARLSON, a citizen of the United States, residing at VVorcester, in the county of `Worcester and State of Massachusetts, have invented a new and useful Rotor, of which the following is a specification.
This vinvention relates to a rotor for a steam turbine or other similar machine.`
. The bronze vanes in such rotors are sube ject to excessive wear and it is desirable to use hard drawn bar stock for these parts. It is the object of my invention to provide a rotor construction in which the vanes are separately formed of bar stock, and in which they are securelyheld against accidental displacement when in use. Y
To this end I preferably p-rovide each vane with non-circular projections at each end by which it may be secured in perforated -concentric bands provided for the. purpose. This construction holds the vanes 1n the desired spaced relation and effectively prevents relative angular displacement. j
Another obj ect of my invention is to provide a firm and satisfactory support for the 3 in Fig. l;
Fig. 4 shows themethod of forming the vanes fromlb-ar stock,- and Fig. 5 is a detail view of a portion of one of the bands.
Referring to the drawings, my improved rotor in its preferred form comprises a hub 10, side plates or discs 11, inner and outer concentric bands 13 and 14, and a plurality of separate vanes 15. The vanes 15 are preferably formed from bar stock drawn Specification of Letters Patent.
1an view, partly in Patented May 23, 119122. 1919. serial No. 310,003.
tothe exact shape of the vane, such as is shown in Fig. 3. This stock may be fed through a press or other machine by which successive notches 16, (Fig. 4) are formed on the opposite edges of the stock. After these notches are formed, the stock is severed along the dotted lines a to form a plurality of separate vanes, each having a short upper projection 17 and a longer lower proj ection 18.
The bands 13 and 14 are provided with a succession of openings of perforations 2O (Fig. 5) of irregular outline corresponding to the cross section of the projections 17 and 18. The vanes are then assembled between the bands 13 and 14 and the short upper projections 17 areheaded down or riveted on the band 14.
These assembled parts may then be mounted upon the hub 10 and discs 11 with the projections 18 between the discs 11.
A plurality of holes 21 are formed in the discs 11, so disposed that they each lie be tween two adjacent vanes. After the parts are assembled, a drill is inserted in each` hole 21 and is advanced between the corresponding vanes, thus forming notches in their adjacent faces through which a rivet 22 may be inserted. Additional rivets 23 secure the discs firmly to the hub 10. W'hen the rivets 22 and 23 are securely headed, a very rigid structure results in which accidental displacements of the vanes is practically impossible. Furthermore, the noncircular section of the projections 17 and 18 prevents angular displacement of the vanes.
Having thus described my invention it will be evident that my improved construction enables me to utilize hard drawn stock for the vanes and also to mount these vanes in a simple, economical and edective manner. It will be evident to those skilled in the art that changes and modifications can be made in my invention within the scope of my invention as set forth in the claim, and l do not wish to be oth erwise limited to the details herein disclosed, but what Ido claim is 'A rotor having in combination a hub, a pair of discs mounted thereon, inner and outer concentric bands, a plurality of vanes having their outer ends secured to the outer band and their reduced inner ends formed of uniform Cross section throughout their length and projecting through the inner band and between said dises, and fasten` ing devices extending through said dises 5 and between certain of said projecting portions7 each fastening device being disposed in notches in the adjacent faces of two adjacent projecting portions` :nul preventing nf'ithdrzuval thereof und also irinly holding said dises against the outer 10 faces oi. the inner ende oi Suid vaines.
In testimony whereof I have herel'into aixed my signature.
AXEL 7. CARLSON.
US310003A 1919-07-11 1919-07-11 Rotor Expired - Lifetime US1417029A (en)

Priority Applications (1)

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US310003A US1417029A (en) 1919-07-11 1919-07-11 Rotor

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US310003A US1417029A (en) 1919-07-11 1919-07-11 Rotor

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US1417029A true US1417029A (en) 1922-05-23

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2880962A (en) * 1951-03-02 1959-04-07 Stalker Dev Company Axial flow bladed rotor construction
US2891719A (en) * 1951-03-02 1959-06-23 Stalker Corp Fabricated axial flow bladed structures
US2996281A (en) * 1956-09-05 1961-08-15 Orenda Engines Ltd Mounting ring for blading in a gas turbine engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2880962A (en) * 1951-03-02 1959-04-07 Stalker Dev Company Axial flow bladed rotor construction
US2891719A (en) * 1951-03-02 1959-06-23 Stalker Corp Fabricated axial flow bladed structures
US2996281A (en) * 1956-09-05 1961-08-15 Orenda Engines Ltd Mounting ring for blading in a gas turbine engine

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