MULTILAYER HIGH PRESSURE CYLINDRICAL VESSEL APT IN PARTICULAR FOR HIGH PRESSURE PROCESSING

Abstract

A multilayer high pressure cylindrical vessel (1) has an inner metal cylinder (3), the inner surface defining an inner volume of the vessel (1) along the radial direction, an outer metal cylinder (4), and one intermediate cylindrical layer sandwiched in space between the inner cylinder (3) and the outer cylinder (4) has and comprising a number of circular wedge segments (51) separated by gaps (52). To improve the vessel there exists an interference fit between the one intermediate cylindrical layer and the adjoining solid cylinders and said gaps (52) are broken by bridges (522) connecting angularly adjacent circular segments (51) and defining two axially adjacent gap sections (521) so that the cylindrical layer is a single cylindrical element (5), and the circular wedge segments (51) separated by gaps (52) both extend in parallel to each other along the longitudinal axis of the vessel (1).

Claims

1. A multilayer high pressure cylindrical vessel (1) comprising an inner metal cylinder (3), the inner surface of which defines inner volume of the vessel (1) along the radial direction, an outer metal cylinder (4), and one intermediate cylindrical layer sandwiched in space between the inner cylinder (3) and the outer cylinder (4) and comprising a number of circular wedge segments (51) separated by gaps (52), wherein, there exists an interference fit between said one intermediate cylindrical layer and the adjoining solid cylinders and said gaps (52) are broken by bridges (522) connecting angularly adjacent circular segments (51) and defining two axially adjacent gap sections (521), so that said cylindrical layer is a single cylindrical element (5), and The circular wedge segments (51) separated by gaps (52) both extend in parallel to each other along the longitudinal axis of the vessel (1).

2. High pressure cylindrical vessel according to claim 1, characterised in that, the bridges (522) of the cylindrical element (5, 5a) have the same axial locations between every two gaps (52) in angular direction.

3. High pressure cylindrical vessel according to claim 2, characterised in that, the bridges (522) of the cylindrical element (5, 5a) in a given gap (52) are located in the centres of the gap sections (521) of angularly adjacent gaps (52).

4. High pressure cylindrical vessel according to claim 1, characterised in that, the bridges (522) are disposed in offset with relation to each other forming a spiral line running through all the bridges (522) around the axis of the cylindrical element (5d).

5. High pressure cylindrical vessel according to claim 3, characterised in that, the ratio between the length of the gap section (521) and the length of the bridge (522) is in a range between 1 to 10000.

6. High pressure cylindrical vessel according to claim 1, characterised in that, the width of the gap (52) remains constant along the radial direction.

7. High pressure cylindrical vessel according to claim 1, characterised in that, the angular length of each pair of the segment (51) and the gap (52) is in a range between 5 and 90.

8. High pressure cylindrical vessel according to claim 1, characterised in that, inner cylinder (3) and/or outer cylinder (4) is/are autofrettaged.

9. High pressure cylindrical vessel according to claim 1, characterised in that, inner cylinder (3), outer cylinder (4) and/or a prefabricate for said at least one intermediate cylindrical layer (5) is/are made of forged cylinder(s).

Description

BRIEF DESCRIPTION OF DRAWINGS

[0020] The invention shall be described and explained below in connection with the attached drawings on which:

[0021] FIG. 1 is a schematic perspective view of a multilayer high pressure cylindrical vessel according to the present invention;

[0022] FIG. 2 is a schematic cross-sectional view of the vessel shown in FIG. 1;

[0023] FIG. 3 is a schematic perspective view of a fragment of an intermediate cylindrical layer of the vessel shown in FIG. 1;

[0024] FIG. 4 is a schematic top view of a fragment of another embodiment of an intermediate cylindrical layer;

[0025] FIG. 5 is a schematic cross-sectional view of another embodiment of a multilayer high pressure cylindrical vessel according to the present invention; and

[0026] FIG. 6 is a schematic top view of a fragment of yet another embodiment of an intermediate cylindrical layer of the vessel according to the present invention.

DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS

[0027] An exemplary embodiment of a multilayer high pressure cylindrical vessel 1 shown in in FIG. 1 comprises two axial closures 2 known to those skilled in the art that shall not be described in detail. Obviously the vessel 1 may be closed by various types of closure systems such as yoke frame, threaded closure, gate valve, pin closure, breech closure etc. Furthermore the vessel 1 may be used for various applications, and in particular for food High Pressure Processing.

[0028] As shown in FIG. 2 the vessel 1 comprises inner metal cylinder 3, outer metal cylinder 4 and an intermediate cylindrical layer 5 sandwiched between the inner cylinder 3 and the outer cylinder 4.

[0029] Elements 3 and 4 are made of high strength alloy steel. Element 5 is made of common steel as it is not subjected to significant stresses. Inner diameters of cylinder 3, cylindrical layer 5 and outer cylinder 4 amount respectively 63 mm, 118 mm and 170 mm. Outer diameter of the vessel 1 amounts 250 mm. To reduce the costs of manufacturing the vessel these dimensions were chosen in order to utilize standard forged cylinders as the inner cylinder 3, the outer cylinder 4 and a prefabricate for the intermediate cylindrical layer 5.

[0030] Obviously unrestricted diameters and thickness relations of elements can be combined together depending on desired pressure resistance and vessel capacity with respect to fabrication costs. Moreover the length of the vessel may be freely changed according to practical applications.

[0031] The intermediate cylindrical layer 5 after assembling is compressed in radial direction between cylinders 3 and 4, as there exists an interference fit so of about 0.2 mm between the layer 5 and the inner cylinder 3, as well as between the layer 5 and the outer cylinder 4.

[0032] FIG. 3 shows in details the intermediate layer 5 of the vessel 1. As shown the layer 5 comprises twenty four equiangularly disposed circular segments 51 separated by gaps 52, both extending in parallel to each other along the longitudinal axis of the vessel 1. The segment 51 and the gap 52 have an angular length of 15.

[0033] Each gap 52 does not entirely separate the angularly adjacent segments 51 but is broken by equidistantly disposed bridges 522 having rounded edges. Bridges 522 connect angularly adjacent segments 51, as well as separate each two axially adjacent gap sections 521.

[0034] The structure of bridges 522 and gap sections 521 may be formed by water jet cutting, milling or any other machining technology known to those skilled in the art that shall not be described in detail.

[0035] In an embodiment of the intermediate layer 5a shown in FIG. 4 axial length of each gap section 521 amounts 180 mm, axial length of each bridge 522 amounts 20 mm and the width of the gap 52 amounts 4 mm and remains constant along the radial direction.

[0036] In embodiments of the intermediate layer 5 and 5a shown in FIG. 3 and FIG. 4 the bridges 522 are alternately disposed in consecutive gaps 52, i.e. the bridges 522 have the same locations along the longitudinal axis between every two alternate gaps 52. Furthermore the bridges 522 in a given gap 52 are located in the centres of the gap sections 521 of angularly adjacent gaps 52.

[0037] In an another embodiment of the vessel according to the present invention shown in FIG. 5 the vessel 1a comprises two intermediate layers 5b and 5c and sandwiched in the space between the inner cylinder 3 and the outer cylinder 4. Both layers 5b and 5c are separated by an additional intermediate solid cylinder 6.

[0038] FIG. 6 shows an another embodiment of an intermediate layer 5d in which the bridges 522 are disposed in offset with relation to each other forming a spiral line running through all the bridges 522 around the axis of the layer 5d.

[0039] The above embodiments of the present invention are merely exemplary. The figures are not necessarily to scale, and some features may be exaggerated or minimized. These and other factors, however, should not be considered as limiting the spirit of the invention, the intended scope of protection of which is indicated in appended claims.