Heat-stationed bayonet connector for cryogenic fluid lines

• US 4,011,732 A
• Filed: 02/14/1974
• Issued: 03/15/1977
• Est. Priority Date: 02/14/1974
• Status: Expired due to Term

• Current Assignee: Process Systems International, Inc. (Chart Industries Incorporated)
• Original Assignee: Helix Technology Incorporated
• Inventors: Johnson, Robert W., Doherty, Paul R.
• Primary Examiner(s): O'Dea, William F.
• Assistant Examiner(s): Capossela, Ronald C.
• Application Number:
  US05/442,326
• Time in Patent Office: 1,125 Days
• Field of Search: 62/45, 62/55, 285/41, 285/47, 285/133 R, 285/138, 285/DIG. 5
• US Class Current: 62/50.7
• CPC Class Codes: F16L 39/005 for concentric pipes
• CPC Class Codes: F16L 59/141 in which the temperature of the medium is below that of the ambient temperature rigid pipes of wood F16L9/006; vacuum insulation F16L59/065
• CPC Class Codes: F16L 59/184 Flanged joints in general F16L23/00
• CPC Class Codes: Y10S 285/904 Cryogenic
• CPC Class Codes: Y10S 505/897 Cryogenic media transfer

Abstract

A heat-stationed bayonet connector suitable for connecting liquid cryogen sources and refrigeration loads to a cryogenic fluid transfer line or for connecting components such as flexible sections, etc., into the transfer line. The incorporation of a cold heat station in the bayonet connector and its thermal connection to a coolant makes it possible to intercept heat flow along the length of the bayonet and thereby to minimize heat losses associated with the connector. The use of a cryogenic coolant transfer line in the form of a flexible bypass connecting the male and female sections of the bayonet makes it possible to use the bayonet connector in a transfer line which incorporates a cooled radiation shield along essentially its entire length.

Claims

1. In a heat-stationed bayonet connector suitable for joining cryogenic fluid transfer lines including male and female sections engageable to form a continuous cryogenic liquid process line with a radiation shielding means therearound for shielding radiation therefrom, the improvement comprising:

a support means for supporting the connector outside the radiation shielding means;

a heat station means for intercepting heat flow, said heat station means being positioned on said radiation shielding means and bonded thereto;

a first tubular means located between and concentric with said process line and said radiation shielding means for inter-connecting said process line and said radiation shielding means, a first end of said first tubular means being attached to said heat station and a second end thereof being attached to said process line at a position offset from said heat station along said process line; and

a second tubular means located outside and concentric with said radiation shielding means for interconnecting said radiation shielding means to said support means, a first end of said second tubular means being attached to said heat station and a second end thereof being adapted for attaching to said support means, at a position offset from said heat station along said process line, whereby when said radiation shielding means are cooled said heat station means is cooled to intercept heat flow from said support means to said process line.

2. A heat-stationed bayonet in accordance with claim 1 wherein said heat station means comprises a first annular heat station in said female section intermediate its length and a second annular heat station in said male section intermediate its length.

3. A heat-stationed bayonet in accordance with claim 2 including a compressible thermal conducting ring between said first and second heat stations providing thermal engagement of said first and second annular heat stations.

4. A heat-stationed bayonet in accordance with claim 1 including means to cool said radiation shielding means.

5. A heat-stationed bayonet in accordance with claim 4 wherein said means to cool said radiation shielding means comprises tubing means bonded to said radiation shielding means and being suitable for circulation of a cryogenic coolant therethrough.

6. A heat-stationed bayonet in accordance with claim 4 wherein said means to cool said radiation shielding means comprises a first cryogenic coolant transfer line bonded to said female section and a second cryogenic coolant transfer line bonded to said male section and bypass means connecting said first and second coolant transfer lines.

7. A heat-stationed bayonet in accordance with claim 6 wherein said bypass means comprises in combination, first and second bayonet connector means having coolant process line means and vacuum jacketing means and being joined through a flexible section formed of inner bellows means coupled to said coolant line means, outer bellows means coupled to said vacuum jacketing means and insulation means interposed between said inner and outer bellows means.

8. A heat-stationed bayonet connector suitable for joining sections of a cryogenic fluid transfer line, comprising in combination

a. a female section comprisinga mating flange defining a female mating surface,

a first extension tube affixed at one end to and extending from said female mating flange,a first annular heat station affixed to the other end of said first extension tube, and bonded thereto,a first radiation shield bonded to said heat station,a second extension tube affixed at one end to said first heat station, extending from it within said first radiation shield and defining therewith a first annular evacuatable spacing, said second tube terminating in a mating seat having affixed thereto a short length of a process line tubing;

and

b. a male section comprising

1. a mating flange having a male mating surface engageable with said female mating surface,

2. a third extension tube affixed at one end to said male mating surface, extending therefrom and sized to define when engaged with said female section a first narrow annular spacing with the internal wall of said first entension tube of said female section,

3. a second annular heat station terminating said third extension tube,

4. a second radiation shield bonded to said second heat station, extending therefrom through said male mating flange and defining with the internal wall of said third extension tube a second annular evacuatable spacing,

10. A bayonet connector in accordance with claim 8 including clamp means to ensure engagement of said male and female mating surfaces.

11. A bayonet connector in accordance with claim 8 including a compressible thermal conducting ring providing a thermal connection between said first and second annular heat stations when said male and female sections are engaged.

12. A heat-stationed bayonet in accordance with claim 8 including means to cool at least one of said radiation shields.

13. A heat-stationed bayonet in accordance with claim 11 wherein said means to cool at least one of said radiation shields comprises tubing means bonded to at least one of said radiation shields and being suitable for circulation of a cryogenic coolant therethrough.

14. A heat-stationed bayonet in accordance with claim 11 wherein said means to cool at least one of said radiation shields comprises a first cryogenic coolant transfer line bonded to said first radiation shield of said female section and a second cryogenic coolant transfer line bonded to said second radiation shield of said male section and bypass means connecting said first and second coolant transfer lines.

15. A heat-stationed bayonet in accordance with claim 13 wherein said bypass means comprises in combination, first and second bayonet connector means having coolant process line means and vacuum jacketing means and being joined through a flexible section formed of inner bellows means coupled to said coolant line means, outer bellows means coupled to said vacuum jacketing means and insulation means interposed between said inner and outer bellows means.

16. A heat-stationed bayonet in accordance with claim 8 wherein said second radiation shield has fluid ports thereby to connect said second and third evacuatable spacings.

17. A heat-stationed bayonet in accordance with claim 8 including multilayer insulation within said first, second and third evacuatable spacings.

19. A heat-stationed bayonet in accordance with claim 17 including a compressible thermal conducting ring between said first and second heat stations providing thermal engagement thereof.

20. A heat-stationed bayonet in accordance with claim 17 including means to cool at least one of said radiation shields.

21. A heat-stationed bayonet in accordance with claim 19 wherein said means to cool at least one of said radiation shields comprises tubing means bonded to at least one of said radiation shields and being suitable for circulation of a cryogenic coolant therethrough.

22. A heat-stationed bayonet in accordance with claim 19 wherein said means to cool at least one of said radiation shields comprises a first cryogenic coolant transfer line bonded to said female section and a second cryogenic coolant transfer line bonded to said male section.

23. A heat-stationed bayonet in accordance with claim 21 including bypass means connecting said first and second coolant transfer lines.

24. A heat-stationed bayonet in accordance with claim 21 wherein said bypass means comprises in combination, first and second bayonet connector means having coolant process line means and vacuum jacketing means and being joined through a flexible section formed of inner bellows means coupled to said coolant line means, outer bellows means coupled to said vacuum jacketing means and insulation means interposed between said inner and outer bellows means.

9. a fourth extension tube affixed to said second heat station, extending therefrom and sized to define when engaged with said female section a second narrow annular spacing with the internal wall of said second extension tube,a nose piece terminating said fourth extension tube and having a sealing ring sized to make a liquid-tight seal within said mating seat, anda cryogenic fluid process line extending from said nose piece to beyond the end of said second radiation shield and defining with the internal walls of said second radiation shield and said fourth extension tube a third annular evacuatable spacing.

18. A heat-stationed bayonet connector suitable for joining sections of a cryogen fluid transfer line, comprising in combination

a. male and female sections engageable to form a continuous fluid helium process line;

b. a first annular heat station in said female section intermediate its length;

c. a second annular heat station in said male section intermediate its length;

d. a first radiation shield thermally bonded to said first annular heat station;

e. a second radiation shield thermally bonded to said second annular heat station.