Abstract:
A tubular connector adapted to extend between two tubular components comprising a tubular body having an internal diameter, a first free end including an annular radial flange having a tapered surface adapted to engage a complementary seating surface on a first of the two tubular components, the internal diameter remaining constant through the first free end; and a second free end having an annular bulbous shape adapted to seat within a cylindrical end of a second of the two tubular components.

Description:
This application is a continuation of 09/384,198 filed Aug. 27, 1999 now abandoned. 
    
    
     This invention was made with Government support under Contract No. DE-FC21-95MC31176 awarded by the Department of Energy. The Government has certain rights in this invention. 
    
    
     BACKGROUND OF THE INVENTION 
     This invention relates generally to land based gas turbine power plants, and specifically to a tubular connector used to radially connect axially extending cooling tubes in a gas turbine rotor cooling circuit. 
     A steam cooling circuit for a gas turbine rotor is disclosed in commonly owned U.S. Pat. No. 5,593,274. Briefly, cooling steam is supplied via a tube concentric to the rotor and then via radial passages to axially extending tubes (parallel to but radially outwardly of the rotor axis) which supply cooling steam to the buckets of one or more of the turbine stages. A similar return path is employed to remove the steam. Because of the rotating environment of the turbine rotor assembly and the centrifugal forces generated thereby, and because of thermal expansion of the various components, any radially oriented coolant tubes must be designed to accommodate relative axial and radial shifting movements where the radial tubes interface at opposite ends with the axial tube fittings. 
     BRIEF SUMMARY OF THE INVENTION 
     This invention relates to a tube having coupling profiles at opposite ends which are particularly advantageous in the context of radial connecting tubes in a rotating environment. Specifically, the tubes to be coupled are substantially parallel but radially offset relative to the rotor axis The fittings which mate with the tube of this invention, however, are in axial alignment with the radial tube. For purposes of this discussion, and unless otherwise explained, references to radial vs. axial or to radially “outer” or radially “inner,” take into account the orientation of the tube as installed in a turbine rotor assembly. References to the “upper” or “lower” ends of the tube correspond to radially outer and inner ends of the tube, respectively, relative to the rotor axis. Reference to a “radial flange” on the tube, however, is made with respect to the longitudinal center axis of the tube itself. 
     In one exemplary embodiment, the radially outer or upper end of the tube has an enlarged radial flange (but with a constant tube ID) formed with a tapered edge, the taper extending inwardly toward the longitudinal center axis of the tube in an upward or radially outer direction. This taper is part spherical in shape so that engagement with a flat conical seat formed on an axially aligned end of an elbow component attached to the radially outer axial cooling tube is substantially tangential. As a result, the radially outer or upper tube end is able to “roll” in the seat in virtually any direction, thus accommodating relative shifting movement between the radially oriented tube and the axial tubes to which it is coupled while, at the same time resisting any radially outward movement which might otherwise occur due to centrifugal forces generated by rotation of the rotor. 
     The radially inner or lower end of the tube is formed as a “half-spoolie,” i.e., the lower free end of the tube is expanded to form a part toroid, formed by a part spherical surface. In other words, an annular groove is formed about the tube end, while the thickness of the tube wall remains substantially constant. This end of the tube is slidably received in a radially extending cylindrical bushing formed in the radially inner, axially extending tube. This arrangement results in tangential line contact at the interface of the tube and a cylindrical ID of the bushing. There is no restraint on any radial movement of the tube at this end, however, (i.e., other than friction) so that the tube can thermally expand in a radially inner direction relative to the rotor axis, even though the tube is constrained against thermal growth at the radially outer end thereof. 
     Accordingly, in its broader aspects, the invention relates to a tubular connector adapted to extend between two tubular components comprising a tubular body having an internal diameter, a first free end including an annular radial flange having a tapered surface adapted to engage a complementary seating surface on a first of the two tubular components, the internal diameter remaining constant through the first free end; and a second free end having an annular bulbous shape adapted to seat within a cylindrical end of a second of the two tubular components. 
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS 
     FIG. 1 is a partial side section of a gas turbine rotor assembly incorporating the connector tube of this invention; and 
     FIG. 2 is a side section of the connector tube in accordance with an exemplary embodiment of the invention. 
     FIG. 1 is a partial side section of a gas turbine rotor assembly incorporating the connector tube of this invention; 
     FIG. 2 is a side section of the connector tube in accordance with an exemplary embodiment of the invention; and 
     FIG. 3 is a cross-section taken along the line  3 — 3  of FIG. 2, but modified to show a coating on the exterior of the connector. 
    
    
     DETAILED DESCRIPTION OF THE INVENTION 
     Referring now to the drawings, there is illustrated a portion of a turbine, including a turbine rotor assembly, generally designated  10 , comprised of axially stacked components, for example, rotor wheels  12 ,  14 ,  16  and  18  which form portions of a four-stage exemplary turbine rotor with spacers  20 ,  22  and  24  alternating between the wheels. The wheel and spacer elements are held together on the rotor by a plurality of elongated, circumferentially extending bolts. only one of which is illustrated at  26 . The wheels  12 ,  14 ,  16  and  18  mount a plurality of circumferentially spaced turbine buckets  12   a ,  14   a ,  16   a  and  18   a , respectively. The combination of nozzles  30 ,  32 ,  34  and  36  and respective wheels  12 ,  14 ,  16  and  18  comprise the stages of the turbine. An aft shaft wheel  42  forms part of the rotor  10  and is bolted to the stacked wheels and spacers. 
     In an advanced gas turbine designed by the assignee hereof. the aft shaft  44  houses a bore tube assembly described and illustrated in detail in co-pending U.S. patent application Ser. No. 09/216363. Briefly, the bore tube assembly includes axially extending outer and inner tubes  48  and  50 , respectively, defining an annular steam-cooling supply passage  52  and a spent steam-cooling return passage  54 . The passages  52  and  54  communicate steam to and from the outer rim of the rotor through sets of radially extending conduits or tubes  56  and  58 , respectively, which in turn communicate with corresponding sets of axially extending tubes spaced circumferentially about the rim of the rotor. The steam supplied through the steam supply passage  52  and radial tubes  56  supply cooling steam to buckets  12   a  and  14   a  of the first and second stages, respectively, via axially extending tubes (not shown), while axial tubes (one shown at  57 ) and radial tubes  58  and return passage  54  receive the spent cooling steam from the buckets for return to a stationary or static pipe (not shown). It will be appreciated that the bore tubes  48  and  50  as well as axial tubes  57  are part of and rotate with the rotor assembly  10 . 
     With reference also to FIG. 2, the radial connector tubes  56 ,  58  in accordance with an exemplary embodiment of the invention are identical and only tube  58  will be described in detail. Connector tube  58  includes a tubular body with a conventional “B-nut”  60  at its radially outer end, and a “half-spoolie” connector  62  at its opposite, radially inner end. The “B-nut”  60  at the radially outer end includes a radial flange  64  and a spherically-shaped or tapered surface  66 . The latter is designed to engage a flat, annular tapered surface  68  of, in this case, an axially aligned end of an elbow  70  which is connected at its opposite end to the radially outer axial tube  57 . This is a conventional seal connection between adjacent tubular members, but is especially useful here, where the connector is subjected to centrifugal forces, tending to move the connector tube  58  in a radial outward direction. In other words, the spherical end of the tube  58  will maintain sealing contact with the mating surface  68  of the elbow  70 , adjusting as necessary to any relative movement between the parts. The B-nut itself may be welded to the end of the tube  58  opposite the half-spoolie  62 , or formed integrally therewith. 
     At the radially inner end, i.e., the half-spoolie end, the tube  58  is enlarged due to a radiused enlargement  72  (both inside and outside surfaces of the tube are increased in diameter), forming an annular, part spherical-shape (also referred to as a part or half-spoolie) which fits inside a straight or cylindrical end or tubular bushing  74  extending radially from the radially inner axial tube  54 . In this way, thermal growth of tube  58  is accommodated at the inner radial end of the tube, while any relative axial shifting motion between the inner and outer radial tubes is accommodated at the “B-nut” connection at the radially outer end of the tube. 
     In the exemplary embodiment, the spoolie surface is coated on its exterior with a wear resistant coating, e.g., a commercially available cobalt base coating  76  alloy known as Tribaloy (see FIG.  3 ). 
     At the radially inner end, i.e., the speolie end, the tube  56  has an enlarged end due to a radiused enlargement. forming an annular, part spherical-shaped end  72  (also referred Lo as a part or half-spoolie) which fits inside a straight or cylindrical end or tubular bushing  74  extending radially from the radially inner axial tube  54 . In this way, thermal growth of tube  58  is accommodated at the inner radial end of the tube, while any relative axial shifting motion between the inner and outer radial tubes is accommodated at the “B-nut” connection at the radially outer end of the tube. 
     In the exemplary embodiment, the spoolie surface is coated on its exterior with a wear resistant coating. e.g., a commercially available cobalt base coating alloy known as Tribaloy. 
     While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiment, it is to be understood that the invention is not to be limited to the disclosed embodiment, but on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.