US792659A - Intermediate bucket and support for turbines. - Google Patents

Intermediate bucket and support for turbines. Download PDF

Info

Publication number
US792659A
US792659A US19420404A US1904194204A US792659A US 792659 A US792659 A US 792659A US 19420404 A US19420404 A US 19420404A US 1904194204 A US1904194204 A US 1904194204A US 792659 A US792659 A US 792659A
Authority
US
United States
Prior art keywords
buckets
support
bucket
base
wheel
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
US19420404A
Inventor
Oscar Junggren
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.)
General Electric Co
Original Assignee
General Electric 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 General Electric Co filed Critical General Electric Co
Priority to US19420404A priority Critical patent/US792659A/en
Application granted granted Critical
Publication of US792659A publication Critical patent/US792659A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246Fastening of diaphragms or stator-rings

Definitions

  • Witm eeee s nvenbor Oscar unggren
  • the present invention relates to intermediate turbine-buckets which are situated between the rows of wheel-buckets and are employed to reverse the direction of the fluid stream or streams and discharge it or them at the proper angle against the adjacent row of wheel-buckets.
  • the intermediate buckets are stationary and are separated from the wheelbuckets or some part of the wheel by a very small clearance, which clearance to a very great degree affects the economy of the machine. The smaller it is the greater will be the economy, because the leakage of the motive fluid is correspondingly reduced.
  • the clearance is frequently as low as .02 of an inch and varies from that to .05 of an inch.
  • My invention has for its object to improve and simplify the construction of intermediate buckets and their support, whereby the cost is reduced and the buckets may be quickly and accurately set.
  • I cast the buckets integral with a segmental base or support located at their outer ends, the inner ends adjacent to the wheel being disconnected. Some or all of the buckets are provided with integral tenons by which a thin cover forming one part of the bucket-spaces is attached.
  • the segmental support is beveled between buckets to give the necessary enlargement toward the exhaust, the thin cover being straight, or substantially so.
  • the periphery of the segmental support is finished in any suitable manner and is seated in a closefitting groove in the wheel casing or support. Bolts of substantial size are arranged to pass through the casing and secure the parts in place.
  • segmental base-piece on which the buckets are formed is located at the point of greatest diameter, whereas with the old construction it was located at the point of least diameter.
  • Figure 1 is a detail sectional view of a set of segmental buckets.
  • Fig. 2 is a sectional view taken at right angles to that shown in Fig. 1; and
  • Fig. 3 is a longitudinal section of an intermediate bucket, illustrating the old construction.
  • 1 represents the segmental base-piece adjacent to the-wheel and having buckets 2 formed integrally therewith.
  • These buckets are cut from the solid stock by a suitable bucket-cutting machine and radiate from acommon center.
  • the outer ends of the buckets are beveled, as indicated at 3, and these beveled ends engage with the correspondingly-beveled surfaces on the support 4.
  • the buckets and support are drilled to receive the retaining-bolts 5, which radiate outwardly from a common center.
  • the head of the bolt is located adjacent to the wheel and the nut at a point adjacent to the wheel-inclosing casing.
  • the nut When the nut is tightened, it has a tendency to move the buckets bodily to the right, owing to the inclination of the surface 3. ,There is always some space around the body of the bolt which is sufficient to throw the buckets out of their proper alinement.
  • Figs. 1 and 2 a construction by means of which I obviate the objections referred to in connection with the old style of bucket shown in Fig. 3.
  • This represents a plurality of radial or substantially radial buckets 6, which are cast integral with a basepiece 7, which is preferably although not necessarily made up in segments. This depends largely on whether the buckets are to cover a small or great angular portion of the wheel.
  • the base portion is formed at the outer ends of the buckets where the diameter is greatgle thereto if it be desired to change the cross-sectional area of the bucket-spaces. In order to compensate for the increased volume of the motive fluid, it is necessary to expand the bucket-spaces in the direction of the exhaust.
  • the beveled surface extends from one side of the bucket to the other, which insures a gradual expansion of the cross-sectional area of the passage.
  • the periphery of the base-piece 7 is finished in any suitable manner in order that it may be securely mounted in the wheel-casing 12 or other support.
  • the base-piece is provided with a smooth peripheral surface and side walls 18, which are parallel with each other and extend at right angles to the peripheral surface.
  • the walls 13 are arranged to engage with the side walls of a groove formed in the support or casing 12.
  • the base-piece is tapped at a number of points to receive the retaining-bolts 1 1, the latter being of substantial size and accessible from the outside of the casing.
  • a tapered portion 15 Between the head and the body of each bolt is a tapered portion 15, which engages with a conical seat formed on the support or casing 12 and which prevents the escape of any steam or other motive fluid around the body of the bolt.
  • a casing a plurality of radial or substantially radial buckets, a base which is formed integral with the buckets and located at the point of greatest diameter, the said buckets being unconnected at their inner ends, means for securing the base which are accessible outside of the casing, a cover for the buckets which is located at the point of least diameter, and means for mounting the base in place.
  • a grooved casing or support a segmental base-piece having a finished periphery which fits into the groove, integral buckets which extend inwardly toward a common point of lesser diameter, and cut-away portions which increase the cross-sectional area of the spaces between buckets, a cover for the inner ends of the buckets, and bolts for retaining the buckets in place, which pass through the support into the segmental base-piece.
  • an intermediate for an elastic-fluid turbine comprising a base-piece, buckets formed integral with the base at their outer ends or point of greatest diameter, and having separate inner ends, the working passages between the buckets eX- ITO panding toward the exhaust, a separable cover for the inner ends of the buckets, which is curved on a smaller radius than the base-piece, and means passing through holes in the cover for securing it in place.
  • an intermediate for an elastic-fluid turbine comprising a segmental base having a finished outer surface for engagement with a support, and
  • I0 cut-away portions to increase the area of the bucket-spaces, a plurality of integral buckets extending inwardly toward a point of lesser diameter, and a sheet-metal cover which is attached to the inner ends of the buckets.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Earth Drilling (AREA)

Description

No. 792,659. I PATENTED JUNE 20, 19-95.
O.JUNGGREN. INTERMEDIATE BUCKET AND SUPPORT FOR TURBINES.
PPPPPPPPPPPPPPPPP 3318,1904.
Witm eeee s: nvenbor Oscar unggren,
NITED STATES latentecl June 20, 1905.
PATENT OFFICE.
OSCAR J UNGGREN, OF SCHENEOTADY, NEW YORK, ASSIGNOR TO GEL ERAL ELECTRIC COMPANY, A CORPORATION OF NEW YORK.
INTERMEDIATE BUCKET AND SUPPORT FOR TURBINES.
SPECIFICATION forming part of Letters Patent No. 792,659, dated June 20, 1905.
Application filed February 18, 1904. Serial No. 194,204.
To all iii/1,0712 [/7 iii/my concern:
Be it known that I, OSCAR J UNGGREN, a citizen of the United States, residing at Schenectady, county of Schenectady, State of New York, have invented certain new and useful Improvements in Intermediate Buckets and Their Supports for Elastic-Fluid Turbines, of which the following is a specification.
The present invention relates to intermediate turbine-buckets which are situated between the rows of wheel-buckets and are employed to reverse the direction of the fluid stream or streams and discharge it or them at the proper angle against the adjacent row of wheel-buckets. The intermediate buckets are stationary and are separated from the wheelbuckets or some part of the wheel by a very small clearance, which clearance to a very great degree affects the economy of the machine. The smaller it is the greater will be the economy, because the leakage of the motive fluid is correspondingly reduced. The clearance is frequently as low as .02 of an inch and varies from that to .05 of an inch. In order to efliciently transform the energy of the motive fluid into useful work, it is necessary to have a relatively high bucket speed, and it is common practice to operate turbines with a bucket speed of four miles per minute and above. Owing to the high peripheral speed of the wheel and to the distortion of the parts due to unequal expansion, the support for the intermediates becomes an important consideration because of the liability of injury due to contacting of the relatively movable parts. Another thing to be taken into account is the expansion in a radial direction of the working passage between the buckets.
Prior to my invention it was the practice to cut the intermediate on the convex side of a segmental piece of stock by means of a bucketcutting machine, it being the only way that buckets can be cut on the machines with which I am familiar. This meant'that in order to get the desired gradual expansion of the passage it was necessary .to bevel the outer ends of the buckets, which engage with a fixed support carried by the casing. Bolts for securing the parts in place were arranged to extend through the segment on which the buckets were formed andalso through the buckets themselves into the support. tion is open to the serious objection that when the securing-bolts are tightened they have a tendency to cause the intermediates to shift bodily in the direction of the bevel on theends of the buckets. Any clearance what- This construc' ever around the body of the bolt such as is through long thin buckets having a tapered end. When the intermediates extend around or largely around the wheel and are made in several sections, the difficulty of adjusting all of the sections exactly right is apparent.
My invention has for its object to improve and simplify the construction of intermediate buckets and their support, whereby the cost is reduced and the buckets may be quickly and accurately set.
In carrying out my invention I cast the buckets integral with a segmental base or support located at their outer ends, the inner ends adjacent to the wheel being disconnected. Some or all of the buckets are provided with integral tenons by which a thin cover forming one part of the bucket-spaces is attached. The segmental support is beveled between buckets to give the necessary enlargement toward the exhaust, the thin cover being straight, or substantially so. The periphery of the segmental support is finished in any suitable manner and is seated in a closefitting groove in the wheel casing or support. Bolts of substantial size are arranged to pass through the casing and secure the parts in place.
One of the distinguishing features of my invention is that the segmental base-piece on which the buckets are formed is located at the point of greatest diameter, whereas with the old construction it was located at the point of least diameter.
In the accompanying drawings, which illustrate one embodiment of my invention, Figure 1 is a detail sectional view of a set of segmental buckets. Fig. 2 is a sectional view taken at right angles to that shown in Fig. 1; and Fig. 3 is a longitudinal section of an intermediate bucket, illustrating the old construction.
Referring to Fig. 3, 1 represents the segmental base-piece adjacent to the-wheel and having buckets 2 formed integrally therewith. These buckets are cut from the solid stock by a suitable bucket-cutting machine and radiate from acommon center. The outer ends of the buckets are beveled, as indicated at 3, and these beveled ends engage with the correspondingly-beveled surfaces on the support 4. The buckets and support are drilled to receive the retaining-bolts 5, which radiate outwardly from a common center. In other words, the head of the bolt is located adjacent to the wheel and the nut at a point adjacent to the wheel-inclosing casing. When the nut is tightened, it has a tendency to move the buckets bodily to the right, owing to the inclination of the surface 3. ,There is always some space around the body of the bolt which is sufficient to throw the buckets out of their proper alinement.
In Figs. 1 and 2 is shown a construction by means of which I obviate the objections referred to in connection with the old style of bucket shown in Fig. 3. This represents a plurality of radial or substantially radial buckets 6, which are cast integral with a basepiece 7, which is preferably although not necessarily made up in segments. This depends largely on whether the buckets are to cover a small or great angular portion of the wheel. The base portion is formed at the outer ends of the buckets where the diameter is greatgle thereto if it be desired to change the cross-sectional area of the bucket-spaces. In order to compensate for the increased volume of the motive fluid, it is necessary to expand the bucket-spaces in the direction of the exhaust. It is preferable to make this expansion gradual, and in the present instance I obtain this expansion by beveling or cutting away the space between the adjacent buckets, as indicated at 11. It is to be noted that the beveled surface extends from one side of the bucket to the other, which insures a gradual expansion of the cross-sectional area of the passage. The periphery of the base-piece 7 is finished in any suitable manner in order that it may be securely mounted in the wheel-casing 12 or other support. In the present instance the base-piece is provided with a smooth peripheral surface and side walls 18, which are parallel with each other and extend at right angles to the peripheral surface. The walls 13 are arranged to engage with the side walls of a groove formed in the support or casing 12. The base-piece is tapped at a number of points to receive the retaining-bolts 1 1, the latter being of substantial size and accessible from the outside of the casing. Between the head and the body of each bolt is a tapered portion 15, which engages with a conical seat formed on the support or casing 12 and which prevents the escape of any steam or other motive fluid around the body of the bolt.
What I claim as new, and desire to secure by Letters Patent of the United States, is
1. In an elastic-fluid turbine, the combination of a casing, a plurality of radial or substantially radial buckets, a base which is formed integral with the buckets and located at the point of greatest diameter, the said buckets being unconnected at their inner ends, means for securing the base which are accessible outside of the casing, a cover for the buckets which is located at the point of least diameter, and means for mounting the base in place.
2. In an elastic-fluid turbine, the combination of a grooved casing or support, a segmental base-piece having a finished periphery which fits into the groove, integral buckets which extend inwardly toward a common point of lesser diameter, and cut-away portions which increase the cross-sectional area of the spaces between buckets, a cover for the inner ends of the buckets, and bolts for retaining the buckets in place, which pass through the support into the segmental base-piece.
3. As an article of manufacture, an intermediate for an elastic-fluid turbine, comprising a base-piece, buckets formed integral with the base at their outer ends or point of greatest diameter, and having separate inner ends, the working passages between the buckets eX- ITO panding toward the exhaust, a separable cover for the inner ends of the buckets, which is curved on a smaller radius than the base-piece, and means passing through holes in the cover for securing it in place.
4. As an article of manufacture, an intermediate for an elastic-fluid turbine, comprising a segmental base having a finished outer surface for engagement with a support, and
I0 cut-away portions to increase the area of the bucket-spaces, a plurality of integral buckets extending inwardly toward a point of lesser diameter, and a sheet-metal cover which is attached to the inner ends of the buckets.
In witness whereof I have hereunto set my 5
US19420404A 1904-02-18 1904-02-18 Intermediate bucket and support for turbines. Expired - Lifetime US792659A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US19420404A US792659A (en) 1904-02-18 1904-02-18 Intermediate bucket and support for turbines.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US19420404A US792659A (en) 1904-02-18 1904-02-18 Intermediate bucket and support for turbines.

Publications (1)

Publication Number Publication Date
US792659A true US792659A (en) 1905-06-20

Family

ID=2861148

Family Applications (1)

Application Number Title Priority Date Filing Date
US19420404A Expired - Lifetime US792659A (en) 1904-02-18 1904-02-18 Intermediate bucket and support for turbines.

Country Status (1)

Country Link
US (1) US792659A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2623728A (en) * 1945-01-16 1952-12-30 Power Jets Res & Dev Ltd Mounting of blades in compressors, turbines, and the like
US5511940A (en) * 1995-01-06 1996-04-30 Solar Turbines Incorporated Ceramic turbine nozzle
US6000906A (en) * 1997-09-12 1999-12-14 Alliedsignal Inc. Ceramic airfoil
US20070110575A1 (en) * 2005-11-17 2007-05-17 General Electric Company Methods and apparatus for assembling steam turbines

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2623728A (en) * 1945-01-16 1952-12-30 Power Jets Res & Dev Ltd Mounting of blades in compressors, turbines, and the like
US5511940A (en) * 1995-01-06 1996-04-30 Solar Turbines Incorporated Ceramic turbine nozzle
US5616001A (en) * 1995-01-06 1997-04-01 Solar Turbines Incorporated Ceramic cerami turbine nozzle
US6000906A (en) * 1997-09-12 1999-12-14 Alliedsignal Inc. Ceramic airfoil
US20070110575A1 (en) * 2005-11-17 2007-05-17 General Electric Company Methods and apparatus for assembling steam turbines
US7654794B2 (en) * 2005-11-17 2010-02-02 General Electric Company Methods and apparatus for assembling steam turbines

Similar Documents

Publication Publication Date Title
US2641440A (en) Turbine blade with cooling means and carrier therefor
US2326145A (en) Turbine blade fastening
US792659A (en) Intermediate bucket and support for turbines.
US730363A (en) Detachable turbine-bucket.
US1072189A (en) Rotary fan.
JP6506533B2 (en) Method and system for securing a turbine nozzle
US841503A (en) Attachment of blades for turbines.
US768597A (en) Turbine-bucket.
US770207A (en) Elastic-fluid turbine-wheel.
US1967962A (en) Steam turbine rotor
US764452A (en) Turbine-bucket cover.
US784431A (en) Steam-turbine.
US1286204A (en) Steam-turbine.
US953241A (en) Elastic-fluid turbine.
US927658A (en) Steam-turbine.
US1266973A (en) Nozzle construction for elastic-fluid turbines.
US809277A (en) Turbine.
US768604A (en) Elastic-fluid turbine.
US785066A (en) Nozzle for turbine-engines.
US1031757A (en) Reentrant turbine.
US1073421A (en) Elastic-fluid turbine.
US803678A (en) Turbine.
US784371A (en) Elastic-fluid turbine.
US841258A (en) Means for securing buckets in turbines.
US1213930A (en) Turbine-nozzle.