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162 Fbrging-Stamping - Heat Treating<br />

Impulse Blades.<br />

Fig. 7-c shows two typical examples of impulse<br />

blades. These are fabricated by either of two methods<br />

(a) milling from bar stock, whereby the port is<br />

milled out on revolving drum fixtures and (b) drop<br />

f<strong>org</strong>ing and hot swaging with suitable dies in a f<strong>org</strong>ing<br />

press concluding with milling operations for base<br />

and edges. Close limits of precision are required in<br />

either case and each blade is subjected to a V guage<br />

inspection to verify the pitch thickness. The finish is<br />

such that the curved surfaces nest together to proper<br />

pitch without milling or other machine finish. Individual<br />

blades of a set may depart from standard in<br />

thickness of pitch not to exceed .005-in., but in all<br />

cases blades guaging plus, must be compensated for<br />

pelative Displacement setweci<br />

JACENT SECTIONS MijsT NOT £,CEEE.<br />

the DiTEEPENCE BETWEEN THE ABOVE<br />

TOLERANCE'<br />

FIG. 8—Sketch of multiple exhaust blade, giving an idea of<br />

the precision required.<br />

by corresponding blades guaging minus, so that the<br />

algebraic sum of all departures from standard for a<br />

full circle or row shall be zero.<br />

Low Pressure Blades of Parallel Section.<br />

Where the necessities of design do not require extreme<br />

length for a low pressure blade out are beyond<br />

the range of physical qualities of manganese copper,<br />

standard practice employs a drop f<strong>org</strong>ed blade of<br />

straight parallel section, for moving rows usually of 5<br />

per cent nickel steel, of which Fig. 7-D shows a typical<br />

example. For stationary rows a parallel section in<br />

manganese copper is used. Although the latter blade<br />

is essentially of parallel section, its base is reinforced<br />

May, 1925<br />

by upset thickening to afford additional strength at<br />

and near the root.<br />

F<strong>org</strong>ed Low Pressure Reaction Blades of<br />

Special Types.<br />

In recent designs of Westinghouse turbines of<br />

large capacities, low pressure blades of 20 to 24 inch<br />

length and even longer have been used. Owing to<br />

the stresses due to high peripheral speeds, also owing:<br />

to radial angularity between the long blades, departure<br />

in certain instances from a straight parallel blade<br />

section has been effected in two particulars: A—the<br />

blade has been tapered to keep down the weight and<br />

stresses due to centrifugal force, and B—the blade has<br />

been twisted or warped for two reasons in order that:<br />

First—the inlet angle may permit the steam to be received<br />

tangentially at all points throughout the length<br />

of the blade, and, second—the passage between the<br />

blades may be of such shape throughout the length of<br />

the blade as to give the requisite nozzle effect in guiding<br />

the steam through the blades for best efficiency.<br />

Various stages in the course of manufacture of a<br />

multiple exhaust blade are shown in Fig. 7-E. On<br />

the bottom is shown the blank sheared to length from<br />

round bar stock. Next is shown the blank after being<br />

broken down under a Bradley hammer in preparation<br />

for the f<strong>org</strong>ing die. Next is the f<strong>org</strong>ing untrimmed<br />

after the first drop. Next is the finished f<strong>org</strong>ing with<br />

the flash trimmed off, and at the top is the blade fully<br />

machined. Not only is the f<strong>org</strong>ing of these blades an<br />

undertaking of unusual refinement, but the machining<br />

requires a high degree of precision in workmanship,<br />

as well as specially developed devices and fixtures.<br />

The sketch of a typical multiple exhaust blade. Fig.<br />

8, shows certain dimensions and characteristic tolerances<br />

from which the required standard of precision<br />

may be judged.<br />

Preparing Models of Dies.<br />

The Keller Mechanical Engineering Corporation<br />

of Brooklyn, New York, was instrumental in working<br />

out methods of preparing models and cutting drop<br />

f<strong>org</strong>e dies for blades for the multiple exhaust design,<br />

an undertaking of no small difficulty or magnitude.<br />

Each cross section of blade to be modeled has its<br />

appropriate contour gauge made of '^ in. sheet steel<br />

and fitted with extreme precision to lapped and<br />

ground steel templates or master pieces. Bottom<br />

halves of these contour guages are shown mounted in<br />

a plate. Fig. 9-A, so that each section bears its proper<br />

relation to its neighbors, vertically, horizontally and<br />

laterally, and these guages form the directing curves<br />

from which by the aid of straight edges, the warped<br />

surfaces are generated in modeling clay, Fig. 9-B.<br />

From this clay model a plaster cast is taken, Fig. 9-C.<br />

and around this plaster cast a cement model Fig. 9-D,<br />

was poured, which when thoroughly hard becomes<br />

available as the model for cutting the bottom die in<br />

an automatic engraving machine. A cast iron frame<br />

encloses the cement model to protect it from breakage<br />

or injury in use. Before being set to work in the<br />

engraving machine, the cement model bottom die is<br />

used in shaping a model for the upper die. Fig. 9-E<br />

shows the model partly prepared with modeling clay,<br />

accurately shaped templates of sheet zinc resting on<br />

the cement form and bedded in the modeling clay<br />

provide the directing curves for generating the sur-

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