56 TRANSACTIONS OF T H E A.S.M.E. JANUARY, 1941 Fio. 7 C r o s s S e c t i o n s T h r o u g h N o n c o n d e n s i n g T u r b i n e s f o r H i g h I n i t i a l P r e s s u r e s a n d T e m p e r a t u r e s ( A p p r o x im a te ly t o sc a le .)
WARREN—MODERN LARGE STEAM TURBINES FOR GENERATOR DRIVE 57 original designs, however, have been refined in certain ways as a result <strong>of</strong> this testing, and have been made much better from the mechanical standpoint as a result <strong>of</strong> operating experience with turbines in the interim. Some turbines have been built where condenser placement on the turbine operating level has perm itted a “stream flow” or “diffuser” type <strong>of</strong> exhaust hood. On these units vacuum measurements were obtained a t the last wheel which were greater than the vacuums existing in the condenser. <strong>The</strong>se hoods have been in service for a number <strong>of</strong> years on several turbines in the Chicago district with great success, but generally this type <strong>of</strong> condenser arrangement has not been favored by station designers on account <strong>of</strong> the extra space and unconventional arrangement required, although a gain somewhat in excess <strong>of</strong> one per cent results. N o n c o n d e n s i n g T u r b i n e s Fig. 7 shows three sizes <strong>of</strong> noncondensing turbines for high pressures and tem peratures. <strong>The</strong>se have been built in quite a number <strong>of</strong> cases to supply industrial process steam, or to operate as superposed turbines exhausting into existing lower-pressure condensing turbines. <strong>The</strong> first <strong>of</strong> these is for 10,000 kw to 15,000 kw capacity, 800 psi to 1200 psi pressure, and up to 900 F. This size machine generally requires no by-pass, and passes all <strong>of</strong> the steam through the first-stage wheel. <strong>The</strong> second is a recently designed machine for 15,000 kw to 20,000 kw capacity, for the same pressure range as the first, and up to 925 F. In this size a by-pass becomes advisable in order to secure the best possible light-load economy. <strong>The</strong> design shown is one <strong>of</strong> the latest involving an internal by-pass, which, as previously pointed out, perm its all <strong>of</strong> the steam to pass through the first-stage wheel at all loads. <strong>The</strong> third shows a type <strong>of</strong> machine which has been built for from 25,000 kw to 00,000 kw capacity, for a wide range <strong>of</strong> steam conditions up to 2300 psi pressure and up to 950 F. <strong>The</strong> first two <strong>of</strong> the foregoing machines are <strong>of</strong> the single-shell type. <strong>The</strong> third machine is <strong>of</strong> a type which was developed only a few years ago, and is known as the “double-shell” construction. I t has been successfully applied to a num ber <strong>of</strong> installations at high pressures and temperatures. Operating experience on seven <strong>of</strong> these turbines now in commercial service has been decidedly favorable. Trouble from steam leaks has not occurred. Shell distortions have been reduced to much less than ever previously experienced even in turbines at lower pressures and tem peratures. <strong>The</strong> dismantling <strong>of</strong> this type has been made easier owing to greater ease <strong>of</strong> handling the smaller shell bolts and the reduced shell distortions. Several other machines <strong>of</strong> this type are now being installed or manufactured. D e v e l o p m e n t o p D o u b l e S h e l l 10 Double-shell construction has had a rather interesting developm ent through four steps, the last <strong>of</strong> which is not yet in operation. <strong>The</strong> various steps in this design are shown in Fig. 8. Basically, the principle is to surround the working parts <strong>of</strong> the turbine with a steam tight inner shell carrying its own bolting flange, and to build around this a second shell. <strong>The</strong> space between the two shells is m aintained by communication with a lower stage in the turbine a t a pressure interm ediate between the intial pressure in the inner shell and the atmosphere. <strong>The</strong> total pressure drop is thus divided into two stages; neither shell 10 "Logan Double-Shell Turbine,” by G. B. Warren, Power, vol. 8 3 , 1937 p p . 3 0 2 -3 0 5 . ‘'53,000-Kw 3000-Iipm Superposed Turbine for Waterside Station,” by G. B. Warren, Combustion, vol. 9, 1938, pp. 27-32. F i o . 8 V a r i o u s D o u b l e - S h e l l D e s i g n s S h o w i n g S u c c e s s i v e D e v e l o p m e n t s
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