Casing design for rotating machinery and method for manufacture thereof

Information

  • Patent Grant
  • 6506018
  • Patent Number
    6,506,018
  • Date Filed
    Monday, July 16, 2001
    23 years ago
  • Date Issued
    Tuesday, January 14, 2003
    22 years ago
Abstract
A casing design for rotating machinery that includes two semi-cylindrical shaped shell sections. Each of the sections includes a machined flange adapted to receive fasteners. The two sections are attached together through fasteners passing through the machined flanges.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




This invention relates to casings for rotating machinery and, more particularly, to split casings for use with gas compressors.




2. Brief Description of the Prior Art





FIG. 1

shows a prior art split casing section A for use with a gas compressor. The split casing section A includes a semi-cylindrical rolled plate B having two opposing edges C, C′ and extending about a longitudinal axis X. A pair of flanges D, D′ extend along each the opposing edges C, C′ with each flange D, D′ attached to the semi-cylindrical rolled plate B through welds E. The flanges D, D′ define a plurality of bore holes F that extend from a top flange side G to a bottom flange side H.




Two of the prior art split casing sections A are traditionally joined together at their respective flanges D, D′, forming a cylindrically shaped split case assembly. The split casing sections A are secured by fasteners, such as bolts, passing through the bore holes F. Rotating machinery components, such as compressor components, are then received within a cavity defined by inner surfaces of the joined split casing assembly.




One method for manufacturing a split casing section A is to roll a flat plate K (shown in FIG.


2


), about the longitudinal axis X into a semi-cylindrical shaped rolled plate B. As shown in

FIG. 3

, flanges D, D′ are then secured to the rolled plate B at edges C, C′ through welds E (shown in FIG.


1


). The bore holes F are drilled or formed in the flanges D, D′ prior to welding the flanges D, D′ to the rolled plate B or after the welding of the flanges D, D′ to the rolled plate B.




The prior art split casing sections A shown in

FIGS. 1 and 3

are expensive to manufacture due to numerous welds. Further, there always exists a possibility of failure due to improper welds between the flanges D, D′ and the rolled plate B. Other prior art casing designs are shown in U.S. Pat. Nos. 1,352,276; 1,839,849; 2,683,017; 3,160,107; 3,390,830; 3,544,232; 4,137,006; 4,305,192; 4,551,065; 4,915,581; and, 5,063,661.




Therefore, it is an object of the present invention to provide a split casing section design that is less expensive to manufacture and does not require welded flanges.




SUMMARY OF THE INVENTION




The present invention is a casing design for rotating machinery, such as gas compressors or turbines, that generally includes a first casing section, a second casing section, and a plurality of fasteners. The first casing section is formed from a single plate into a substantially semi-cylindrical shaped shell having two opposing edges, two opposite external sides, and machined flanges. The second casing section is also formed from a single plate into a substantially semi-cylindrical shaped shell having two opposing edges, two opposing edges, and machined flanges. Opposing edges of each first casing section are aligned with corresponding opposing edges of each second casing section to form a substantially cylindrical structure held together by the plurality of fasteners. The fasteners pass through bore holes formed by each of the machined flanges.




A hollow receiving cavity is defined by inner surfaces of the joined first and second casing sections, as well as end plates joined to the first and second casing sections. The receiving cavity can receive rotating machinery components, such as compressor or turbine components.




The present invention is also a method for manufacturing a one-half section of a split casing assembly that includes the steps of:




a. providing a substantially semi-cylindrical casing section; and




b. forming flanges on opposite exterior sides of the semi-cylindrical section by removing material from the substantially semi-cylindrical shaped casing section. The method can also include the steps of,




c. forming a plurality of bore holes in the flanges;




d. forming port holes in the casing section;




e. connecting ports to the port holes; and




f. connecting the semi-cylindrical casing section to another semi-cylindrical casing section, forming a cylindrically shaped split casing assembly having a hollow receiving cavity in fluid communication with the ports.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is an elevational end view of a prior art split casing section;





FIG. 2

is an elevational end view of a flat plate used to manufacture the prior art split casing section shown in

FIG. 1

;





FIG. 3

is an exploded elevational end view of the prior art split casing section shown in

FIG. 1

;





FIG. 4

is a perspective view of a casing design for rotating machinery having a first casing section and a second casing section made in accordance with the present invention;





FIG. 5

is an exploded perspective view of the casing design for rotating machinery shown in

FIG. 4

;





FIG. 6

is a top perspective view of the first casing section shown in

FIG. 4

;





FIG. 7

is a top perspective view of the second casing section shown in

FIG. 4

;





FIG. 8

is another top perspective view of the second casing section shown in

FIGS. 4 and 7

; and





FIG. 9

is a side view of a flat plate.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT





FIGS. 4 and 5

show a split casing assembly


10


for rotating machinery made in accordance with the present invention. The present invention generally includes a first casing section


12


attached to a second casing section


14


. The first casing section


12


and the second casing section


14


are made from rolled plate


16


, preferably steel, and form semi-cylindrical shaped shell structures, each having the same radius of curvature R. Alternatively, it is believed that the first casing section


12


and the second casing section


14


can be cast or forged. The split casing assembly


10


is adapted to receive rotating machines


54


(shown schematically), such as components for a gas compressor or a gas turbine. A plurality of ports


18


are attached to the first casing section


12


or, as shown in

FIGS. 4 and 5

, to the second casing section


14


. End plates


20


are secured to first and second opposite ends


22


,


24


of the split casing assembly


10


and may be equipped with seals to form a sealed pressure arrangement.




Referring specifically to

FIG. 5

, a hollow receiving cavity


26


is defined by inner surfaces


27


of the first casing section


12


, the second casing section


14


, and the end plates


20


. The hollow receiving cavity


26


is adapted to receive rotating machinery


54


, such as components for a compressor or a turbine, as shown in FIG.


5


.




With continuing reference to

FIG. 5

, as well as

FIG. 4

, the first casing section


12


is a substantially semi-cylindrical shaped shell or rolled plate


16


that extends along a longitudinal axis L. The first casing section


12


has radius R, a longitudinal length CL, first and second external sides


30


,


32


, and includes two machined flanges


28


each positioned on the first or second external sides


30


,


32


and each extending the longitudinal length CL of the first casing section


12


. The machined flanges


28


, shown in greater detail in

FIG. 6

, are defined by two surfaces, a first surface


34


and a second surface


36


, which are substantially transverse or perpendicular to one another.




The second casing section


14


, shown in detail in

FIGS. 7 and 8

, is similar to the first casing section


12


and like reference numerals will be used for like elements. The second casing section


14


has radius R, a longitudinal length CL, first and second external sides


30


,


32


, and includes two machined flanges


28


extending the longitudinal length CL of the second casing section


14


. The machined flanges


28


are defined by two surfaces, a first surface


34


and a second surface


36


, which are substantially transverse or perpendicular to one another. The first and second casing sections


12


,


14


are preferably thick enough to allow machined flanges


28


and still function as a pressure vessel. Likewise, the end plates


20


are also preferably thick enough to withstand elevated pressures.




One difference between the first and second casing sections


12


,


14


is that a plurality of port holes


46


are preferably defined on the second casing section


14


, as shown in

FIGS. 7 and 8

, although the first casing section


12


can form port holes


46


as well. Referring to

FIGS. 4 and 5

, the ports


18


are welded to the second casing section


14


. The ports


18


are adapted to align with the port holes


46


so that the ports


18


are in fluid communication with the hollow receiving cavity


26


.




As shown in

FIG. 6

, the machined flanges


28


are integrally formed on the first and second external sides


30


,


32


of the first and second casing sections


12


,


14


at circumferential distances RD


1


and RD


2


. Circumferential distances RD


1


and RD


2


are functions of angles α and β and their corresponding radius vectors R


1


and R


2


. Radius vectors R


1


and R


2


originate at a midpoint M of an imaginary diameter line DL that connects the first and second opposite ends


22


,


24


of the first casing section


12


and/or the second casing section


14


and is equal in length to the interior diameter DL of the casing sections


12


,


14


. In contrast to radius R, shown in

FIG. 5

, radius vectors R


1


and R


2


extend to the external sides


30


,


32


of the casing sections


12


,


14


.




A plurality of bore holes


38


are drilled or formed through the respective second surfaces


36


of the flanges


28


. The bore holes


38


extend from the second surfaces


36


to the respective first and second edges


40


,


42


of the first or second casing sections


12


,


14


. The bore holes


38


are spaced along the second surfaces


36


throughout the length CL of the first and second casing sections


12


,


14


, as shown in

FIG. 4

, and are configured to receive fasteners, such as bolts.




With continuing reference to

FIG. 4

, the first casing section


12


is secured to the second casing section


14


by placing or abutting respective first and second edges


40


,


42


against each other so that respective bore holes


38


are aligned with one another. Threaded bolts or fasteners


44


, shown in

FIG. 5

, pass through the bore holes


38


until threaded ends of the bolts


44


extend from the second surfaces


36


of the flanges


28


in the second casing section


14


. Threaded ends of the bolts


44


also extend from the second surfaces


36


of the first casing section


12


. Threaded cover nuts


48


are threadably received by the ends of the bolts


44


positioned adjacent the first casing section


12


and nuts


50


are threadably received by the ends of the bolts


44


positioned adjacent the second casing section


14


, so as to secure the first casing section


12


to the second casing section


14


and form a split casing assembly


10


. In this arrangement, axes L, L′, L′′ are aligned with one another, wherein the split casing assembly


10


is substantially cylindrical in shape and has a constant radius of curvature R. The end plates


20


can then be secured internally before bolting or externally after bolting to the split casing assembly


10


, thereby forming the casing design for rotating machinery


54


. Preferably, the end plates


20


are mounted internally against a retaining step or face in the hollow receiving cavity


26


or can be mounted externally with fasteners (not shown).




It should be appreciated that the end plates


20


can be secured to either or both of the first and/or second casing sections


12


,


14


and rotating machinery components can be attached to end plates


20


and sections


12


,


14


prior to securing the first casing section


12


to the second casing section


14


.




The method for manufacturing the first casing section


12


is set forth as follows. First, a flat plate


52


, preferably made from steel, is provided. As shown in FIG.


9


, the flat plate


52


is then rolled in the direction of the arrows so that the plate


52


is curved about the axis L and has a semi-cylindrical shape. As shown in

FIG. 6

, flanges


28


having first and second surfaces


34


,


36


are then machined in the rolled plate


16


. The first and second surfaces


34


,


36


are defined on opposite sides


22


,


24


of the rolled plate


16


and the respective surfaces


34


,


36


are substantially transverse to one another. A plurality of bore holes


38


are then machined or drilled in the second surfaces


36


of the machined flanges


28


. The bore holes


38


can be recessed to provide clearance for nuts


48


,


50


and are preferable spaced apart to provide for the bolts


44


and nuts


48


,


50


. Further, the bore holes


38


are spaced sufficiently away from first surface


34


to provide clearance for nuts


48


and


50


. The bore holes


38


extend from the second surfaces


36


to respective first and second edges


40


,


42


.




As shown in

FIGS. 7 and 8

, the method for manufacturing the second casing section


14


is substantially the same as the method for manufacturing a first casing section


12


except that a plurality of port holes


46


are formed on the rolled plate


16


by, for example, machining or drilling. Preferably, both the first and second casing sections


12


,


14


are semi-cylindrical shaped and have the same radius R of curvature. Ports


18


can be connected to the port holes


46


and the first and second casing sections


12


,


14


can be connected to one another, forming a cylindrically shaped split casing assembly


10


having a hollow receiving cavity


26


in fluid communication with the ports


18


. Port holes


46


may also be formed in the first casing section


12


or no port holes


46


formed in either the first casing section


12


or the second casing section


14


.




The present invention is less expensive to manufacture than the prior art casings, which require separate flanges to be welded to the rolled plate. Further, the present invention results in a stronger design through increased wall thickness and the elimination of welded flanges.




The invention has been described with reference to the preferred embodiment. Obvious modifications and alterations will occur to others upon reading and understanding the preceding detailed description. It is intended that the invention be construed as including all such modifications and alterations insofar as they come within the scope of the appended claims or the equivalents thereof.



Claims
  • 1. A casing for rotating machinery comprising:a first casing section formed from a single plate into a substantially semi-cylindrical shaped shell, said first casing section having two opposing edges and two opposite external sides, said two opposite external sides having machined flanges forming bore holes; a second casing section formed from a single plate into a substantially semi-cylindrical shaped shell, said second casing section having two opposing edges and two opposite external sides, said two opposite external sides having machined flanges forming bore holes, said second casing defining a port hole; and a plurality of fasteners, wherein said opposing edges of each first casing section are aligned with corresponding opposing edges of said second casing section to form a substantially cylindrical structure held together by said plurality of fasteners passing through said bore holes.
  • 2. The casing design for rotating machinery as claimed in claim 1 wherein said flanges extend along a length of said first casing section and extend along a length of said second casing section.
  • 3. The casing design for rotating machinery as claimed in claim 1 wherein said machined flanges are defined by a first surface and a second surface, wherein said first surface and said second surface are transverse to one another.
  • 4. The casing design for rotating machinery as claimed in claim 1 wherein said flanges are integrally formed on said external sides of said first and second casing sections.
  • 5. The casing design for rotating machinery as claimed in claim 1 wherein said first and second casing sections are made from steel.
  • 6. A method for manufacturing one-half of a split casing assembly for rotating machinery, comprising the steps of:a. providing a substantially semi-cylindrical casing section; and b. forming flanges on opposite exterior sides of the semi-cylindrical section by removing material from said substantially semi-cylindrical shaped casing section.
  • 7. A method for manufacturing a split casing section as claimed in claim 6, further comprising the step of forming a plurality of bore holes in said flanges.
  • 8. A method for manufacturing a split casing section as claimed in claim 6, further comprising the step of forming port holes in said casing section.
  • 9. A method for manufacturing a split casing section as claimed in claim 8, further comprising the step of connecting ports to said port holes.
  • 10. A high pressure split vessel comprising:a first casing section formed from a single plate into a substantially semi-cylindrical shaped shell, said first casing section having two opposing edges, two opposite external sides, and an inner surface, said two opposite external sides having machined flanges forming bore holes; a second casing section formed from a single plate into a substantially semi-cylindrical shaped shell, said second casing section having two opposing edges, two opposite external sides, and an inner surface, said two opposite external sides having machined flanges forming bore holes, wherein said opposing edges of each first casing section are aligned with corresponding opposing edges of said second casing section to form a substantially cylindrical structure, said second casing defining a port hole; a plurality of fasteners passing through said bore holes in said second surface of said machined flanges; at least one end plate having an inner surface joined to said first casing section and said second casing section, wherein said inner surface of said first casing section, said inner surface of said second casing section, and said inner surface of said at least one end plate form a hollow receiving cavity; and a rotating machine positioned inside said hollow receiving cavity.
  • 11. The high pressure split vessel as claimed in claim 10 wherein a port is connected to said port hole.
  • 12. The high pressure split vessel as claimed in claim 11 wherein said hollow receiving cavity is in fluid communication with said port.
  • 13. The high pressure split vessel as claimed in claim 10 wherein said machined flanges extend along a length of said first casing section and extend along a length of said second casing section.
  • 14. The high pressure split vessel as claimed in claim 10 wherein said machined flanges are integrally formed on said external sides of said first and second casing sections.
  • 15. The high pressure split vessel as claimed in claim 10 wherein said first and second casing sections are made from steel.
  • 16. The high pressure split vessel as claimed in claim 10 wherein said rotating machine is a turbine.
  • 17. The high pressure split vessel as claimed in claim 10 wherein said rotating machine is a compressor.
Parent Case Info

This application claims the benefit of provisional application No. 60/117,090 filed Jan. 25, 1999.

PCT Information
Filing Document Filing Date Country Kind
PCT/US00/01746 WO 00
Publishing Document Publishing Date Country Kind
WO00/43640 7/27/2000 WO A
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Number Name Date Kind
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4915581 Groenendaal, Jr. et al. Apr 1990 A
5063661 Lindsay Nov 1991 A
5149248 Cramer Sep 1992 A
Foreign Referenced Citations (1)
Number Date Country
58-138208 Aug 1993 JP
Provisional Applications (1)
Number Date Country
60/117090 Jan 1999 US