US2278304A - Joint construction - Google Patents

Joint construction Download PDF

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Publication number
US2278304A
US2278304A US348332A US34833240A US2278304A US 2278304 A US2278304 A US 2278304A US 348332 A US348332 A US 348332A US 34833240 A US34833240 A US 34833240A US 2278304 A US2278304 A US 2278304A
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Prior art keywords
casing
joint
bolts
outer contact
contact surface
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Expired - Lifetime
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US348332A
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Joseph D Conrad
Kenneth R Stearns
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CBS Corp
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Westinghouse Electric and Manufacturing Co
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Application filed by Westinghouse Electric and Manufacturing Co filed Critical Westinghouse Electric and Manufacturing Co
Priority to US348332A priority Critical patent/US2278304A/en
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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
    • 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
    • F01D25/243Flange connections; Bolting arrangements

Definitions

  • Yet another object of the invention is the provision of a turbine casing having its wall thickened in the vicinity of the horizontal main joint, with the interior wall of the casing forming an oval whose major axis is perpendicular to the plane of the casing main joint, together with motive fluid inlets for both the top and the bottom part of the casing.
  • an elastic fluid turbine comprised by a casing II and a rotor l2, together with a plurality of rows of blades I3, alternate rowsbeing mounted upon the rotor I2 and upon blade rings l4, respectively.
  • the casing H is comprised. by a base portion l6 and a cover portion ll haVing meeting surfaces providing a horizontal joint l8 lying approximately in a plane containing the longitudinal axis of the rotor.
  • the base and cover portions are provided with integral flanges l9 and 20, respectively, and held in assembled relation by suitable means, such as the bolts 21.
  • Motive fluid is supplied to the steam space 22, between the casing and rotor, through a plurality of inlets 23 opening through both the base It and cover [1.
  • At least one of the meeting surfaces defining the joint I8 is relieved at 25 to provide outer contact surfaces 26 and inner contact surfaces 21.
  • the inner contact surface is provided with the conventional leak-off groove 28.
  • This invention provides a design and structure avoiding, insofar as possible, any eccentricity of the bolts.
  • the bolts in the preferred embodiment herein illustrated, are positioned with their longitudinal centerlines C disposed tangent to an are describing the center of the casing wall.
  • the bolts shall be positioned so that the ratio of the distance from the point at which a pure force would hold the halve-s of the cylinder in equilibrium, against the internal pressure, without rotation of the contact surfaces, to the centroid of the compression stressin the outer contact surface, divided by the distance from the centroid of the bolt pull to the centroid of the compression stress in the outer contact surface, is of a value between 1.5 and 0.6.
  • this ratio may be expressed as the distance from the are describing the center of the main casing wall, indicated by the dot-dash line A, to the center of the outer contact surface dotdash line B, divided by the distance from the centerline C of the bolts to the centerline B of the outer contact surface.
  • ratio greater than unity are a direct measure of the lever arm of the bolting, that is, the steam load on the joint multiplied by the ratio gives the required bolt pull to obtain contact at the inner contact surface.
  • the fulcrum changes to the inner contact surface, and the foregoing ratio loses its meaning as a ratio of bolt pull.
  • a casing subject to high internal pressure comprising a pair of parts; flange portions integral with said parts; said parts, including the flange portions, having meeting surfaces defining a joint; at least one of said surfaces having a groove extending longitudinally thereof and defining inner and outer contact surfaces; and a plurality of bolts associated with said flanges for connecting said parts, said bolts being positioned with said inner and outer contact surfaces disposed inwardly and outwardly thereof and at such a distance from the longitudinal centerline of the casing that the ratio of the distance from an arc describing the center of the casing wall to the center of the outer contact surface to the distance from the centerline of said bolts to said center of the outer contact surface lies between the limits 1.5 and 0.6.
  • a turbine cylinder casing subject to high internal pressure comprising a base and a cover both provided with steam inlets; flange portions integral with said base and cover; said base and cover, including the flange portions, having meeting surfaces defining a horizontal joint; at least one of said surfaces having a groove extending longitudinally thereof and separating inner and outer contact surfaces; a cylindrical rotor within the casing, said casing in cross-section having an oval interior, with the major axis of said oval disposed perpendicular to the plane of the joint between the base and cover, whereby the casing wall is thickened adjacent said joint and the steam space between the rotor and easing decreases in area from the top and bottom of the casing toward the joint; and a plurality of bolts associated with the flanges for connecting the base and cover, said bolts being positioned with said inner and outer contact surfaces disposed inwardly and outwardly thereof and at such a distance from the longitudinal centerline of the casing that the distance from an are describing the center of the casing Wall to the center of
  • a casing subject to high internal pressure comprising a pair of parts having meeting surfaces defining a joint, at least one of the parts having a longitudinal groove providing inner and outer contact surfaces cooperating with the surface of the other part, and a plurality of bolts extending through the walls of said parts at right angles to the plane of the joint and disposed so that said inner and outer contact surfaces are arranged inwardly and outwardly thereof, respectively, with the longitudinal centerlines of said bolts approximately tangent to an are describing the radial center of the casing Wall.

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

Description

March 31, 1942.
2|. ao I J. D. CONRAD ET AL JOINT..CONSTRUCTION Filed July 30, 1940 as a7 I l ll l lm l3 .INVENTORS 1 ATTORNEY Patented Mar. 31, 1942 UETED STATES PATENT OFFICE JOINT CONSTRUCTION Vania Application July 30, 1940, Serial No. 348,332
3 Claims.
Yet another object of the invention is the provision of a turbine casing having its wall thickened in the vicinity of the horizontal main joint, with the interior wall of the casing forming an oval whose major axis is perpendicular to the plane of the casing main joint, together with motive fluid inlets for both the top and the bottom part of the casing.
These and other objects are efiected by the invention as will be apparent from the following description and claims taken in connection with the accompanying drawing, forming a part of this application, in which:
In the drawing, the single figure is a transverse sectional view through an elastic fluid turbine embodying the invention.
Referring now to the drawing more in detail,
there is shown, at ID, an elastic fluid turbine comprised by a casing II and a rotor l2, together with a plurality of rows of blades I3, alternate rowsbeing mounted upon the rotor I2 and upon blade rings l4, respectively. The casing H is comprised. by a base portion l6 and a cover portion ll haVing meeting surfaces providing a horizontal joint l8 lying approximately in a plane containing the longitudinal axis of the rotor. The base and cover portions are provided with integral flanges l9 and 20, respectively, and held in assembled relation by suitable means, such as the bolts 21. Motive fluid is supplied to the steam space 22, between the casing and rotor, through a plurality of inlets 23 opening through both the base It and cover [1. At least one of the meeting surfaces defining the joint I8 is relieved at 25 to provide outer contact surfaces 26 and inner contact surfaces 21. Preferably, the inner contact surface is provided with the conventional leak-off groove 28.
The high pressures and temperatures encountered in present-day turbine practice render it increasingly diflicult to design the turbine casing with a joint free of leakage, where the conventional bolted flanges are relied upon for maintaining the joint fluid tight. Such joints are subject, not only to direct force, but also to a bending moment, the latter being due to the eccentric location of the bolts with respect to the centroid of the main-casing wall.
This invention provides a design and structure avoiding, insofar as possible, any eccentricity of the bolts.
To this end, the bolts, in the preferred embodiment herein illustrated, are positioned with their longitudinal centerlines C disposed tangent to an are describing the center of the casing wall.
While this tangent relationship of the centerline of the bolts with respect to the centroid of the turbine casing wall is the preferable arrangement, it will be readily appreciated that any positioning of the bolts closely approximating the preferred arrangement, would be a big improvement over prior practice. Therefore, it is proposed that the bolts shall be positioned so that the ratio of the distance from the point at which a pure force would hold the halve-s of the cylinder in equilibrium, against the internal pressure, without rotation of the contact surfaces, to the centroid of the compression stressin the outer contact surface, divided by the distance from the centroid of the bolt pull to the centroid of the compression stress in the outer contact surface, is of a value between 1.5 and 0.6. For all practical purposes, this ratio may be expressed as the distance from the are describing the center of the main casing wall, indicated by the dot-dash line A, to the center of the outer contact surface dotdash line B, divided by the distance from the centerline C of the bolts to the centerline B of the outer contact surface.
Values of ratio greater than unity are a direct measure of the lever arm of the bolting, that is, the steam load on the joint multiplied by the ratio gives the required bolt pull to obtain contact at the inner contact surface. For values of the ratio below unity, the fulcrum changes to the inner contact surface, and the foregoing ratio loses its meaning as a ratio of bolt pull. Al-
1 though, as the bolts are moved inward below a ratio of unity, the bolt stress to prevent rotation of the joint increases, nevertheless, under certain conditions, it may be desirable to employ the self sealing effect of the pressure by transferring load from the outer to the inner contact surface under this condition.
The value of unity for the ratio previously defined eliminates the inherent eccentricity of the conventional flanged joint and is unique in freeing the bolting of the duty of preventing the flanges from rotating, but very great benefit compared to past practice can be had without realizing a ratio value of exactly unity. For example, a ratio of 1.1 would increase the bolt stress 10%.
Moving the bolts inwardly in the manner proposed, would, in many cases, result in the bolt holes extending through the inner walls of the casing, and hence it is necessary to thicken the walls at this point by increasing the amount of 1' material at the inner portions thereof adjacent the joints. As shown in the drawing, this produces an inner casing wall of elliptical section, resulting in a steam passage 22 which tapers in cross-section from the top and bottom of the casing toward the horizontal joint. Due to this narrowing of the steam passage 22 in the vicinity of the horizontal joint l8, it is necessary to have steam inlets, such as at 23, for both the base l6 and cover I! of the casing.
While the invention has beenshown in but one form, it will be obvious to those skilled in the art that it is not so limited, but is susceptible of various changes and modifications without departing from the spirit thereof, and it is desired, therefore, that only such limitations shall be placed thereupon as are specifically set forth in the appended claims.
What is claimed is:
1. A casing subject to high internal pressure comprising a pair of parts; flange portions integral with said parts; said parts, including the flange portions, having meeting surfaces defining a joint; at least one of said surfaces having a groove extending longitudinally thereof and defining inner and outer contact surfaces; and a plurality of bolts associated with said flanges for connecting said parts, said bolts being positioned with said inner and outer contact surfaces disposed inwardly and outwardly thereof and at such a distance from the longitudinal centerline of the casing that the ratio of the distance from an arc describing the center of the casing wall to the center of the outer contact surface to the distance from the centerline of said bolts to said center of the outer contact surface lies between the limits 1.5 and 0.6.
2. A turbine cylinder casing subject to high internal pressure comprising a base and a cover both provided with steam inlets; flange portions integral with said base and cover; said base and cover, including the flange portions, having meeting surfaces defining a horizontal joint; at least one of said surfaces having a groove extending longitudinally thereof and separating inner and outer contact surfaces; a cylindrical rotor within the casing, said casing in cross-section having an oval interior, with the major axis of said oval disposed perpendicular to the plane of the joint between the base and cover, whereby the casing wall is thickened adjacent said joint and the steam space between the rotor and easing decreases in area from the top and bottom of the casing toward the joint; and a plurality of bolts associated with the flanges for connecting the base and cover, said bolts being positioned with said inner and outer contact surfaces disposed inwardly and outwardly thereof and at such a distance from the longitudinal centerline of the casing that the distance from an are describing the center of the casing Wall to the center of the outer contact surface, divided by the distance from the centerline of the bolt to said center of the outer contact surface results in a quotient between 1.5 and 0.6.
3. A casing subject to high internal pressure comprising a pair of parts having meeting surfaces defining a joint, at least one of the parts having a longitudinal groove providing inner and outer contact surfaces cooperating with the surface of the other part, and a plurality of bolts extending through the walls of said parts at right angles to the plane of the joint and disposed so that said inner and outer contact surfaces are arranged inwardly and outwardly thereof, respectively, with the longitudinal centerlines of said bolts approximately tangent to an are describing the radial center of the casing Wall.
JOSEPH D. CONRAD. KENNETH R. STEARNS.
US348332A 1940-07-30 1940-07-30 Joint construction Expired - Lifetime US2278304A (en)

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2527445A (en) * 1947-06-02 1950-10-24 Westinghouse Electric Corp Turbine steam supply connection
US2808813A (en) * 1952-05-21 1957-10-08 Svenska Rotor Maskiner Ab Rotary positive displacement engine with helically grooved cooled rotors
US20040007263A1 (en) * 2001-01-09 2004-01-15 Font Juan Anguera Two-way trap
EP2405105A3 (en) * 2010-07-08 2014-04-23 General Electric Company Steam turbine shell
WO2017182106A1 (en) * 2016-04-18 2017-10-26 Man Diesel & Turbo Se Turbomachine housing
EP3690202A1 (en) * 2019-01-31 2020-08-05 Elliott Company Oval steam turbine casing
US10968887B2 (en) * 2018-01-29 2021-04-06 Siemens Gamesa Renewable Energy A/S Trailing edge assembly
USD941360S1 (en) 2019-01-31 2022-01-18 Elliott Company Oval steam turbine casing

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2527445A (en) * 1947-06-02 1950-10-24 Westinghouse Electric Corp Turbine steam supply connection
US2808813A (en) * 1952-05-21 1957-10-08 Svenska Rotor Maskiner Ab Rotary positive displacement engine with helically grooved cooled rotors
US20040007263A1 (en) * 2001-01-09 2004-01-15 Font Juan Anguera Two-way trap
US7066195B2 (en) 2001-01-09 2006-06-27 Juan Anguera Font Two-way trap
EP2405105A3 (en) * 2010-07-08 2014-04-23 General Electric Company Steam turbine shell
CN109154207A (en) * 2016-04-18 2019-01-04 曼能源解决方案欧洲股份公司 Turbine cylinder
WO2017182106A1 (en) * 2016-04-18 2017-10-26 Man Diesel & Turbo Se Turbomachine housing
JP2019513944A (en) * 2016-04-18 2019-05-30 マン・エナジー・ソリューションズ・エスイー Turbo machine housing
EP3445953B1 (en) 2016-04-18 2020-04-01 MAN Energy Solutions SE Turbomachine housing
US10968887B2 (en) * 2018-01-29 2021-04-06 Siemens Gamesa Renewable Energy A/S Trailing edge assembly
EP3690202A1 (en) * 2019-01-31 2020-08-05 Elliott Company Oval steam turbine casing
US20200248589A1 (en) * 2019-01-31 2020-08-06 Elliott Company Oval Steam Turbine Casing
JP2020125750A (en) * 2019-01-31 2020-08-20 エリオット・カンパニー Oval steam turbine casing
USD941360S1 (en) 2019-01-31 2022-01-18 Elliott Company Oval steam turbine casing

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