US2729491A - High pressure closure fastener - Google Patents

High pressure closure fastener Download PDF

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US2729491A
US2729491A US278081A US27808152A US2729491A US 2729491 A US2729491 A US 2729491A US 278081 A US278081 A US 278081A US 27808152 A US27808152 A US 27808152A US 2729491 A US2729491 A US 2729491A
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Prior art keywords
cover
barrel
ring
shear
wall
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Expired - Lifetime
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US278081A
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Everett N Sieder
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Alco Products Inc
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Alco Products Inc
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F22STEAM GENERATION
    • F22GSUPERHEATING OF STEAM
    • F22G3/00Steam superheaters characterised by constructional features; Details of component parts thereof
    • F22G3/009Connecting or sealing of superheater or reheater tubes with collectors or distributors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J13/00Covers or similar closure members for pressure vessels in general
    • F16J13/02Detachable closure members; Means for tightening closures
    • F16J13/10Detachable closure members; Means for tightening closures attached by means of a divided ring
    • 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
    • Y10T292/00Closure fasteners
    • Y10T292/20Clamps
    • Y10T292/205Ring

Definitions

  • This invention relates to closures for pressure vessels 'andmoreparticularly toclosur'e's for high pressure heads of heat exchangers.
  • the principal object of the invention is the provision of a closure for the head of a high pressure vessel, such as a feed Water heater, wherein the hydrostatic load of the shell fluid upon the cover 'is "transmitted to the barrel by a novel shea'r ring structure.
  • Another object is the provision of a novel 'sh'ea'r'rihg structure wherein cocking of the shear pieces is elimina't'ed.
  • a further object is to provide a shear ring construction employing a minimum number of elements 'toprovide a simple and economical closure.
  • barrel of the-head of a heatexchanger of the shell and 'tube type is formed with a shoulder 11 against which "cover 12i's located when ithe cover is originally assembled into thelbarrel.
  • Barrel 10 is provided with at least one inwardly opening annular recess defined by radial walls 13 and 14 and end wall 15.
  • Cover 12 has an annular cut-out portion, generally indicated at 16, defined by longitudinal wall 17, radial wall 18, longitudinal wall 19, preferably a tapered wall 20, and radial wall 21.
  • the chamber 22 forming part of said cut-out is provided to facilitate assembly of shear ring 23 which has a tapered wall 24 conforming to the tapered wall portion 20.
  • the tapered portion serves two purposes in the illustrative embodiment.
  • the cover permits a greater amount of material to be used than a square corner would permit.
  • the cover which is a disc supported at its edges, can thus better resist the bending moment created by the internal pressure.
  • the tapered wall 24 or the shear ring conforms to the wall 20 and facilitates assembly. it has a more important function as a means of localizing the force on the shear ring as will later appear.
  • the forward portion of the cover between the chamber 22 and the forward face 12a of the cover is shaped as an annular flange 12b whose peripheral wall 17 is spaced from the barrel thus forming an annular opening.
  • the diameter of the flange is intermediate the diameters of the cover and of the cut-out portion.
  • a's'used herein is the direction of the open end of the barrel, or upward as viewed in the drawing.
  • shear ring 23 conventionally segmented to permit its assembly into operative position between the barrel and cove 'is retained in assembled position in the barrel by any suitable 'rneatns such as the continuous backing ring 25.
  • shear ring 23 comprises a main body having an annular radial flange 26 extending into the barrel recess and preferably although not necessarily an annular projection 27 extending forwardly between "backing ring 25 and the barrel.
  • the radial dimension of the forward wall of flange 26 is substantially equal to that of the forward "radial wall 14 of the barrel recess so that there is full mating engagement between the adjacent surfaces.
  • cover 12 When hydrostatic pres sure builds up in the chamber '28 of the heat exchanger head, cover 12 will be forced forwardly to the small extent permitted by the manufacturing clearances of the parts so that its wall '21 engages the shear ring. The latter is forced into tight sealing engagement with the shear bearing wall 14.
  • the forward wall of shear ring 23 extends radially inward to overlap a portion of wall 18 and provide an outer contact area thereof. It is this novel overlap structure that comprises the essence of 'the present i vention.
  • any balancing force can be created by the ways mentioned above or by a combination of them. Suitable equivalents will readily suggest themselves, such as projections in the cover or ring to provide contact, all within the scope of the invention.
  • the median diameter of the outer contact area must lie radially inwardly of the median diameter of the inner contact area.
  • the median diameter is defined as that diameter which divides each annular contact area into two equal areas. If a non-circular member such as an elliptical barrel is used, the median line of each contact area corresponds to the median diameter as defined for circular members. Expressed in another manner, the total peripheral length of the inner contact area must exceed the total peripheral length of the outer contact area.
  • a conventional sealing structure which consists of two gaskets 30 secured in position by a gasket retaining ring 31.
  • the gaskets are received in slots or channels'in the cover and barrel as clearly seen in the drawing.
  • Gasket ring 31, spanning the joints where leakage may occur, has gasket-compressing projections 32 joined by a relatively thin flexible central portion.
  • Inner and outer compression rings 33 and 34 respectively are used to hold the gasket ring in position and are fastened to the cover and barrel by bolts 35 and 36 respectively.
  • Such construction provides a fluid tight seal.
  • a plurality of radial holes 37 and axial holes 38 are provided around the periphery of the cover for the purpose of blowing out the chamber 22 in the event it shouldbecome clogged with foreign matter.
  • a plug 39 is provided to seal off hole 38.
  • Apparatus of the character described comprising a pressure-sustaining barrel having an opening at one end and an inwardly facing continuous recess having a shear bearing wall adjacent the opening, a segmented shear member disposed in said recess and extending into the barrel, a cover in the opening radially overlapping the shear member on each side thereof to form. an inner contact area and an outer contact area between the shear member and the cover, the median line of said outer contact area being radially inward of the median line of said inner contact area.
  • Apparatus of the character described comprising a hollow pressure-sustaining barrel having an opening at one end thereof and an inwardly facing annular recess having a shear bearing wall adjacent the opening, a cover disposed in the opening and. having an annular cut-out portion radially opposite said recess, an annular flange on the cover between the cut out portion and. the forward face of the cover, said flange having a lesser diameter than said cover diameter, a. segmented shear ring having a radial flange extending into the barrel recess to engage the shear bearing wall of the recess and a forward wall extending radially inward into overlapping engagement with the flange of the cover, and means to hold said shear ring in place.
  • Apparatus of the character described comprising a hollow pressure-sustaining barrel having an opening at one end thereof and an inwardly facing annular recess having a shear bearing wall adjacent the opening, a cylindrical cover disposed in the opening, the diameter of the rear portion of the cover being substantially equal to the inner diameter of the barrel and the diameter of the forward portion of the cover being less than that of the barrel thus defining an annular opening between the barrel and cover, an annular cut out portion in the cover opposite the barrel recess, a segmented shear ring filling the barrel recess and extending into the cut out portion to form an overlapping engagement with the forward portion of the cover, and means to hold the shear ring in place.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Pressure Vessels And Lids Thereof (AREA)

Description

Jan. 3, 1956 E. N. SIEDER 2,729,491
HIGH PRESSURE CLOSURE FASTENER Filed March 22, 1952 EVERETT N. SIED'ER INVENTOR ATTORN United States Patent Products, Ineorpor'ated, New York, N. Y., a corporation of New York Application March 22, 1952, Serial No. 278,081
3 Claims. (Cl. 292-456.)
This invention relates to closures for pressure vessels 'andmoreparticularly toclosur'e's for high pressure heads of heat exchangers.
In high pressure closures of the class in which "the cover is inserted within the head barrel and which employs shear pieces to transmit the hydrostatic ressure load from the cover to the barrel, one of the problemsencountered is the cocking of the sh'ear pieces due to the couple acting upon them. Such cocking permits looseness in the seating of the cover with consequent move- 'ment thereof and binding at the corners of the recess where the shear pieces fit into the channel barrel.
The principal object of the invention is the provision of a closure for the head of a high pressure vessel, such as a feed Water heater, wherein the hydrostatic load of the shell fluid upon the cover 'is "transmitted to the barrel by a novel shea'r ring structure.
Another object is the provision of a novel 'sh'ea'r'rihg structure wherein cocking of the shear pieces is elimina't'ed.
A further object is to provide a shear ring construction employing a minimum number of elements 'toprovide a simple and economical closure.
Other and further objects of the invention will appear from the following description, the accompanying drawings and the appended claims.
In the drawing, there is shown a "partial-sectional view ot a closure construction employing the present inventiOh.
Referring now to the drawing, barrel of the-head of a heatexchanger of the shell and 'tube type is formed with a shoulder 11 against which "cover 12i's located when ithe cover is originally assembled into thelbarrel. Barrel 10 is provided with at least one inwardly opening annular recess defined by radial walls 13 and 14 and end wall 15. Cover 12 has an annular cut-out portion, generally indicated at 16, defined by longitudinal wall 17, radial wall 18, longitudinal wall 19, preferably a tapered wall 20, and radial wall 21. The chamber 22 forming part of said cut-out is provided to facilitate assembly of shear ring 23 which has a tapered wall 24 conforming to the tapered wall portion 20. The tapered portion serves two purposes in the illustrative embodiment. On the cover, it permits a greater amount of material to be used than a square corner would permit. The cover, which is a disc supported at its edges, can thus better resist the bending moment created by the internal pressure. The tapered wall 24 or the shear ring, of course, conforms to the wall 20 and facilitates assembly. it has a more important function as a means of localizing the force on the shear ring as will later appear. The forward portion of the cover between the chamber 22 and the forward face 12a of the cover is shaped as an annular flange 12b whose peripheral wall 17 is spaced from the barrel thus forming an annular opening. The diameter of the flange is intermediate the diameters of the cover and of the cut-out portion. Forward or outer,
a's'used herein, is the direction of the open end of the barrel, or upward as viewed in the drawing.
Shear ring 23, conventionally segmented to permit its assembly into operative position between the barrel and cove 'is retained in assembled position in the barrel by any suitable 'rneatns such as the continuous backing ring 25. In cross section, shear ring 23 comprises a main body having an annular radial flange 26 extending into the barrel recess and preferably although not necessarily an annular projection 27 extending forwardly between "backing ring 25 and the barrel. The radial dimension of the forward wall of flange 26 is substantially equal to that of the forward "radial wall 14 of the barrel recess so that there is full mating engagement between the adjacent surfaces. When hydrostatic pres sure builds up in the chamber '28 of the heat exchanger head, cover 12 will be forced forwardly to the small extent permitted by the manufacturing clearances of the parts so that its wall '21 engages the shear ring. The latter is forced into tight sealing engagement with the shear bearing wall 14.
It should be pointed out that the projection 27 on shear ring 23 used in conjunction with ring 25, is illustrative only of one means to hold the shear ring in .position during initial assembly. Other equally suitable means will readily suggest themselves for the same purpose. I
It should be noted that the forward wall of shear ring 23 extends radially inward to overlap a portion of wall 18 and provide an outer contact area thereof. It is this novel overlap structure that comprises the essence of 'the present i vention.
Without 'the overlapping Contact area an unbalanced couple tends to rotate the shear ring counterclockwise as is customary in all the shear ring closures with which applicant is familiar. This couple is made up of the forward pressure force of the cover applied on radial wall '21 forming an inner contact area, times its lever arm, and the rearward reactive force in the shell applied on wall 14 times its lever arm. The lever arm extends from the point of application of the forces to a fulcrum: that lies within the shear ringan'd on an extension of thefjoint line "29 for "this example. This couple, which 'inducescoc king, is resisted by a clockwise movement on the shear ring which consists of an inward reactive force exerted 'by Wall IS on the shear ring through the outer contact area -'as cover "12 moves outwardly under load, times its longerlever arm to "the same fulcrum. So under load the shear ring, in effect, becomes an integral part of the cover.
It will be apparent that the balancing or reactive force can be changed. The point of application of the cover force to ring 23 can be localized on the ring by suitable means such as the hereinbefore mentioned tapered wall 24. If the taper is changed or the rings radial dimension or the diameter of flange 12b changed, the point of application of the force can be moved radially inwardly or outwardly. Thus any balancing force can be created by the ways mentioned above or by a combination of them. Suitable equivalents will readily suggest themselves, such as projections in the cover or ring to provide contact, all within the scope of the invention.
It is then apparent that a number of arrangements will produce the desirable and reactive force to prevent the cocking of shear ring 23. The. salient features of the invention require that the cover overlap the shear ring on the forward or outer edge to provide an outer contact area between the cover and ring. It is necessary that the elements be formed, as previously described in the illustrative embodiment, so that the reactive force is applied radially inwardly of the outward force applied by the cover to the shear ring. That is to say, there are two annular contact areas between the cover and the ring, one on each side of the ring. These are 'an outer and an inner contact area at walls 18 and 21 respectively. If the uniformly distributed force or, load applied at either contact area is treated as applied at a line, it will be applied on the median diameter of the contact areas. Then, according to the invention, the median diameter of the outer contact area must lie radially inwardly of the median diameter of the inner contact area. The median diameter is defined as that diameter which divides each annular contact area into two equal areas. If a non-circular member such as an elliptical barrel is used, the median line of each contact area corresponds to the median diameter as defined for circular members. Expressed in another manner, the total peripheral length of the inner contact area must exceed the total peripheral length of the outer contact area.
A construction, however made, must fall within these limitations. If it does, it will balance the twisting couple and prevent cocking of the shear ring.
To provide a seal for the joint 29 between the cover and the barrel, a conventional sealing structure is used which consists of two gaskets 30 secured in position by a gasket retaining ring 31. The gaskets are received in slots or channels'in the cover and barrel as clearly seen in the drawing. Gasket ring 31, spanning the joints where leakage may occur, has gasket-compressing projections 32 joined by a relatively thin flexible central portion. Inner and outer compression rings 33 and 34 respectively are used to hold the gasket ring in position and are fastened to the cover and barrel by bolts 35 and 36 respectively. Such construction provides a fluid tight seal.
A plurality of radial holes 37 and axial holes 38 (only one of each being shown) are provided around the periphery of the cover for the purpose of blowing out the chamber 22 in the event it shouldbecome clogged with foreign matter. A plug 39 is provided to seal off hole 38.
From the above description, it will be apparent that cocking of the shear ring is prevented by the novel overlapping arrangement described.
While therehas been hereinbefore described an approved embodiment of this invention, it will be understood that many and various changes and modifications in form, arrangement of parts and details'of construction thereof may be made without departing from the spirit of the invention, and that all such changes and modifications as fall within the scope of the appended claims are contemplated as a part of this invention.
What I claim is:
1. Apparatus of the character described comprising a pressure-sustaining barrel having an opening at one end and an inwardly facing continuous recess having a shear bearing wall adjacent the opening, a segmented shear member disposed in said recess and extending into the barrel, a cover in the opening radially overlapping the shear member on each side thereof to form. an inner contact area and an outer contact area between the shear member and the cover, the median line of said outer contact area being radially inward of the median line of said inner contact area.
2. Apparatus of the character described comprising a hollow pressure-sustaining barrel having an opening at one end thereof and an inwardly facing annular recess having a shear bearing wall adjacent the opening, a cover disposed in the opening and. having an annular cut-out portion radially opposite said recess, an annular flange on the cover between the cut out portion and. the forward face of the cover, said flange having a lesser diameter than said cover diameter, a. segmented shear ring having a radial flange extending into the barrel recess to engage the shear bearing wall of the recess and a forward wall extending radially inward into overlapping engagement with the flange of the cover, and means to hold said shear ring in place.
3. Apparatus of the character described comprising a hollow pressure-sustaining barrel having an opening at one end thereof and an inwardly facing annular recess having a shear bearing wall adjacent the opening, a cylindrical cover disposed in the opening, the diameter of the rear portion of the cover being substantially equal to the inner diameter of the barrel and the diameter of the forward portion of the cover being less than that of the barrel thus defining an annular opening between the barrel and cover, an annular cut out portion in the cover opposite the barrel recess, a segmented shear ring filling the barrel recess and extending into the cut out portion to form an overlapping engagement with the forward portion of the cover, and means to hold the shear ring in place.
References Cited in the file of this patent UNITED STATES PATENTS 2,196,895 Bowman Apr. 9, 1940 2,268,507 Gertzon Dec. 30, 1941 2,296,620 Tinker Sept. 22, 1942 2,298,511 Rathbon Oct. 13, 1942 2,342,186 Fischer Feb. 22, 1944 2,559,564 Sperling July 3, 1951
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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2869910A (en) * 1956-02-20 1959-01-20 Bristol Aircraft Ltd Snap ring devices
US2954894A (en) * 1957-03-28 1960-10-04 Acf Ind Inc Closure assembly
US3156375A (en) * 1963-08-29 1964-11-10 Charles A Long External pressure seal for pressure vessels
US3161317A (en) * 1962-10-26 1964-12-15 Babcock & Wilcox Co Pressure vessel closure
US4438866A (en) * 1982-08-03 1984-03-27 Westinghouse Electric Corp. Prestressed dome closure flange
US4565297A (en) * 1982-08-16 1986-01-21 Uhde Gmbh High-pressure vessel with inner closure

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2196895A (en) * 1938-05-18 1940-04-09 Westinghouse Electric & Mfg Co High-pressure sealing head
US2268507A (en) * 1940-05-04 1941-12-30 Lummus Co Heat exchanger
US2296620A (en) * 1939-05-11 1942-09-22 Ross Heater & Mfg Co Inc Closure for pressure vessels
US2298511A (en) * 1938-05-11 1942-10-13 Westinghouse Electric & Mfg Co Sealing closure for high-pressure heads
US2342186A (en) * 1938-04-23 1944-02-22 Westinghouse Electric & Mfg Co High-pressure sealing head
US2559564A (en) * 1945-09-10 1951-07-03 Curren C Sperling Pneumatic and air sweep closure

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2342186A (en) * 1938-04-23 1944-02-22 Westinghouse Electric & Mfg Co High-pressure sealing head
US2298511A (en) * 1938-05-11 1942-10-13 Westinghouse Electric & Mfg Co Sealing closure for high-pressure heads
US2196895A (en) * 1938-05-18 1940-04-09 Westinghouse Electric & Mfg Co High-pressure sealing head
US2296620A (en) * 1939-05-11 1942-09-22 Ross Heater & Mfg Co Inc Closure for pressure vessels
US2268507A (en) * 1940-05-04 1941-12-30 Lummus Co Heat exchanger
US2559564A (en) * 1945-09-10 1951-07-03 Curren C Sperling Pneumatic and air sweep closure

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2869910A (en) * 1956-02-20 1959-01-20 Bristol Aircraft Ltd Snap ring devices
US2954894A (en) * 1957-03-28 1960-10-04 Acf Ind Inc Closure assembly
US3161317A (en) * 1962-10-26 1964-12-15 Babcock & Wilcox Co Pressure vessel closure
US3156375A (en) * 1963-08-29 1964-11-10 Charles A Long External pressure seal for pressure vessels
US4438866A (en) * 1982-08-03 1984-03-27 Westinghouse Electric Corp. Prestressed dome closure flange
US4565297A (en) * 1982-08-16 1986-01-21 Uhde Gmbh High-pressure vessel with inner closure

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