Patent GB-1104025-A (GB)
Title: Flow control systems
Inventor: CUNDILL BRIAN RANDALL
IPC: G21C13/02
Filed: 1965-02-16
Abstract: 1,104,025. Valves. ENGLISH ELECTRIC CO. Ltd. 11 Feb., 1966 [16 Feb., 1965], No. 6620/65. Heading F2V. [Also in Division G6] A gas-cooled nuclear reactor has means for circulating the coolant successively through an inlet space and fuel channels between which are disposed gag valves, each of which is provided with flow control means, valve-operating means being operatively connected to the flow control means and controllable from a location remote from the gag valves so that the coolant flow can be varied while the reactor is in operation. With reference to Figs. 2A and 2B, each gag valve 23 has a cylindrical shell 50 supported from the core support plate 53 concentric with the corresponding fuel channel 12 and projecting below it into the coolant inlet space 13. A hollow cylindrical valve member 54, open at its upper end and arranged coaxially within the shell 50, has a triangular main flow port 55 formed in its side co-operating with a trapeziumshaped main flow port 56 in the shell 50 to allow gas to pass from the space 13 to the inside of the valve member 54. The parallel sides of the port 56 are axial, and the port 55 is in the form of an isosceles triangle with its base axial and its height equal to the perpendicular distance between the parallel sides of the port 56. The valve member 54 is rotatable and movable axially by means of two graphite bearings 60, 61 surrounding a shaft 59 and carried by a support spider 62 and a support plate 63, respectively, both of which are fixed in the shell 50. The lower end of shaft 59 carries a piston 64 slidable in an upper cylinder 65 carried by the support plate 63. A port 65A is provided in the upper portion of cylinder 65 so that the top of the piston 64 is always subjected to the gas pressure existing in the inlet space 13. The lower end of cylinder 65 is open and communicates with a lower cylinder 67 of larger internal diameter and having its bottom end closed by an end plate 68 penetrated by an inlet duct 69. A circular thrust plate 73, perforated by holes 74, is arranged within the lower cylinder 67 and is normally held by a compression spring 75 against the lower end of the upper cylinder 65. The valve member 54 has a lower portion 54A of smaller internal diameter and provided with an integral external annular ring 80 (Fig. 5, not shown), part of which is cut away to accommodate an end stop 82 fixed to the shell 50 while further portions, diametrically opposite the portion 81, are cut away to form radial teeth 83 of hexagonal section (Fig. 6, not shown). Adjacent the teeth 83 and fixed in an insert 50A in the shell 50 are three axiallyspaced tapered lugs 84, 85, 86. The teeth 83 and lugs 84 to 86 are so positioned and shaped as to constitute an indexing mechanism for rotating the valve member 54 by one tooth pitch at a time in response to axial movement of the valve member, the direction of rotation being dependent on the initial direction of axial movement of the valve member. Remote control means are described for connecting the space beneath the piston 64 to either a high pressure or a low pressure reservoir. Temperature-responsive devices such as thermocouples may be provided in the fuel channels and connected to temperature-indicating equipment by switch means when the corresponding gag valve is actuated.