CA1122835A - Necked-down bolt for connecting thermal shock-stressed structural parts - Google Patents

Necked-down bolt for connecting thermal shock-stressed structural parts

Info

Publication number
CA1122835A
CA1122835A CA341,034A CA341034A CA1122835A CA 1122835 A CA1122835 A CA 1122835A CA 341034 A CA341034 A CA 341034A CA 1122835 A CA1122835 A CA 1122835A
Authority
CA
Canada
Prior art keywords
bolt
packing
necked
structural parts
reduced diameter
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
Application number
CA341,034A
Other languages
French (fr)
Inventor
Johannes Sporri
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.)
BBC Brown Boveri AG Switzerland
Original Assignee
BBC Brown Boveri AG Switzerland
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 BBC Brown Boveri AG Switzerland filed Critical BBC Brown Boveri AG Switzerland
Application granted granted Critical
Publication of CA1122835A publication Critical patent/CA1122835A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/02Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
    • 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
    • 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
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B31/00Screwed connections specially modified in view of tensile load; Break-bolts
    • F16B31/04Screwed connections specially modified in view of tensile load; Break-bolts for maintaining a tensile load
    • 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
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B35/00Screw-bolts; Stay-bolts; Screw-threaded studs; Screws; Set screws
    • 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
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L23/00Flanged joints
    • F16L23/16Flanged joints characterised by the sealing means
    • F16L23/24Flanged joints characterised by the sealing means specially adapted for unequal expansion of the parts of the joint

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Connection Of Plates (AREA)
  • Pressure Vessels And Lids Thereof (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Joining Of Building Structures In Genera (AREA)

Abstract

ABSTRACT OF THE DISCLOSURE
Necked-down bolt for connecting thermal shock-stressed structural parts. A thermally conducting packing encloses the reduced diameter portion of the bolt and sub-stantially fills-up the air gap between the reduced diameter portion and a borehole wall in order to increase the heat transfer to the bolt and accordingly reduce the heat stresses in the bolt.

Description

s BACKGROUND AND OBJECTS OF THE INVENTION

The present invention refers to a necked-down bolt for connecting thermal shock-stressed structural parts.
With conventional necked-down bolts, the threadless part of the necked-dbwn bolt features a smaller diameter than the core cross-section of the threaded ends. As a result, this necked-down bolt part in the installed state is seated with relatively great play in the borehole of at least one of the two structural parts to be connected.
With thermal shock-stressed structural parts, as perhaps with casings and similar components of high pressure and medium-pressure steam turbines, when starting from the cold state, there appears as a consequence of this great play between borehole and bolt barrel or shaft a poor heat transfer from, for.example, the casing flanges on the necked-down bolt. There can thus occur a temperature difference between the bolt and the flange parts which leads to thermal stresses owing to the differing thermal expansions of bolt and flange parts. If the thermal conductivity of the high-strength bolt barrel is relatively`low, these thermal stresses can become so great that the bolt connection is endangered and the packing strips on the casing flanges can become plastically defor~ed.

`' ` '' ~

33~i It is, therefore, an object of the present invention to provide for improved thermal conductivity to the necked-down bolt.

SUMMARY OF THE INVENTION

This object is achieved by a bolt assembly for use in connecting thermal shock-stressed structural parts.
The assembly comprises a necked-down bolt having a reduced diameter portion intermediate its ends and a threaded end for connection to one of the structural parts, and a thermal conductive packing surrounding said reduced diameter portion with essentially no play. The outer diameter of the packing is at least equal to the major thread diameter of the threaded end of the bolt.

THE DRA~ING ~ ~-Examples of preferred embod;ments of the invention are described in detail in the following with reference to the accompanying drawing wherein: ' Figure 1 is a cross~section through portions of two casing halvas depicting a stratn pin bolt according to the invention with a strain measuring pin, for inter~
connecting the casing halves~ , ~: '
- 2 ~ ~

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Figuxe 2 depicts a modified form of a thermal packing according to the invention, and Figure 3 depicts a two-part form of construction of the thermal packing.

DETAILED DESCRIPTION OF A PREFERRED

EMBODIMENT OF THE INVENTION

In Figure 1, two casing halves 1, 2 of a stream turbine to be connected are depicted. The bolt used for achieving this connection is a strain pin bolt 3 whose one threaded end 4 is threaded to the casing lower half 1. A resilien~ sleeve 6 is provided between the bolt nut 5 and a contact surface of the casing upper part 2.
The necked-down bolt 3 features a measuring pin 7 which is used in the well-known manner to measure, with the aid of a dial guage 8 and a support 9, the elongation and thereby the initial stress of the bolt when tightening the nut 5.
The reduced diameter barrel part of the bolt is enclosed by a thermal packing which comprises a two-part sleeve 10 divided longitudinally and formed of a good heat-conducting material. It features essentially no play or clearance with respect to both the bolt barrel as well :

.~. .
3 -~, . . .
: ' ' .

~, as the wall of the borehole 11. A ~light play may be provided such that, in operation, i.e,, in the heated state of the connection, the sleeve is not jammed between the bolt barrel and the borehole wall; otherwise, in the case of an eccentricity of the bolt axis with respect to the borehole axis which may be present, a bending of the bolt may occur. ~t can be stated in reference to the dimensions of the strain pin bolt 3, that the outside diameter of the sleeve is at least equal to, and preferably at least a few tenths of a millimeter larger than the diameter of the threaded part 40 As a result of the presence of the thermal packing, heat will be effectively transferred to the reduced diameter portion of the bolt 3 to avoid the afore-ment;oned problems. -Another form of sleeve used as a thermal packingis shown in Figure 2. Th~s sleeve 12 is constructed of one piece and features an ;nternal thread 13 extending over its entire length and which corresponds to the thread ends of the bolt 3. This enables the sleeve to be screwed over one of the two threaded ends of the bolt 3 in order to arr;ve at its position enveIoping the necked-down bolt barrel, ~ d~ r3~lD ~ ~

In order for design of Figure 2 to achieve a good heat transfer from the sleeve to the bolt barrel, necked-down bolts will mainly be used whose reduced shaft diameter substantially corresponds to the thread core diameter of the thread 13 so that the internal thread crests substantially contact the reduced shaft in the heated state.
For the purpose of an improved manipulation of the bolt during installation, it is possible according to an embodiment depicted in Figure 3 to hold together a two-part sleeve 14 in its position encompassing the reduced shaft by means of spring rings 15 which engage in the peripheral slots 16 of the two sleeve halves 17 and 18.
In order to hold together the two halves of a two~
part sleeve, it is naturally also possible to use other means such as hinges, set pins, pushbutton-type pin connections, etc.
The material for the thermal packing used for steam turbines should feature a good heat conductivity approximately in the order of magnitude of 40 W/m C.
In this way, a reduction of about one-third of the additional stress in the reduced diameter barrel of the bolt appearing during start-up may be achieved~

- 5 -: :

- ~ , .

3~i Here, the invention is described with application `to a strain pin bolt, and it is, however, naturally also possible to design other necked-down bolts, for example bolts with a head, possibly for large connecting and torque rods, according to the features of the invention.
Although the invention has been descriked in connec-tion with a preferred embodiment thereof, it will be appreciated by those skilled in the art that additions, modifications, substitutions, and deletions not specifically described may be made without departing from the spirit and scope of the inventlon as defined in the appended claims.

.

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, ~

Claims (4)

The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows:
1. A bolt assembly for use in connecting thermal shock-stressed structural parts comprising a necked-down bolt having a reduced diameter portion intermediate its ends and a threaded end of larger diameter for connection to one of the structural parts, and a thermal conductive packing surrounding said reduced diameter portion, said packing comprising a one-piece member having internal threading over its entire length corresponding to the threading of said bolt to enable said packing to be inserted past said threaded end of said bolt.
2. Apparatus according to claim 1, wherein said packing has a slight play relative to said reduced diameter portion to prevent bending of the bolt.
3. Apparatus according to claim 1, wherein one axial end of said packing is free of axial compressive forces.
4. Apparatus according to claim 1, wherein said packing comprises a rigid, non-porous material.
CA341,034A 1978-12-01 1979-11-30 Necked-down bolt for connecting thermal shock-stressed structural parts Expired CA1122835A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH12296/78 1978-12-01
CH1229678 1978-12-01

Publications (1)

Publication Number Publication Date
CA1122835A true CA1122835A (en) 1982-05-04

Family

ID=4381676

Family Applications (1)

Application Number Title Priority Date Filing Date
CA341,034A Expired CA1122835A (en) 1978-12-01 1979-11-30 Necked-down bolt for connecting thermal shock-stressed structural parts

Country Status (6)

Country Link
CA (1) CA1122835A (en)
DE (1) DE2854139A1 (en)
DK (1) DK506079A (en)
FR (1) FR2442988A1 (en)
NL (1) NL7908644A (en)
SE (1) SE7909820L (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2545888B1 (en) * 1983-05-10 1987-07-17 Compair Climax Sa CYLINDER, ESPECIALLY MICROVERIN COMPRISING A DEVICE FOR SUPPORTING EXTERNAL EXTERNAL ELEMENTS
DE3320460C1 (en) * 1983-06-07 1984-10-18 Thyssen Industrie Ag, 4300 Essen Resilient mountain anchor
FR2577632B1 (en) * 1985-02-19 1987-09-25 Framatome Sa ELEMENT FILTERING VARIATIONS OF CONSTRAINTS IN A BOLT ASSEMBLY
EP2025882A1 (en) * 2007-08-14 2009-02-18 Siemens Aktiengesellschaft Casing assembly for a stationary turbo engine

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB417053A (en) * 1933-03-22 1934-09-24 Richard William Bailey Improvements in and relating to flanged and like joints
FR1306491A (en) * 1961-11-20 1962-10-13 Ind Fernand Courtoy Bureau Et Device for establishing a clampable joint between two elements

Also Published As

Publication number Publication date
DE2854139A1 (en) 1980-06-12
SE7909820L (en) 1980-06-02
FR2442988A1 (en) 1980-06-27
DK506079A (en) 1980-06-02
NL7908644A (en) 1980-06-03

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