Tables III. and IV. give the results obtained in a series of experiments on the transverse strengths and torsional resistance of unhammered, annealed steel castings, the specimens being cut from crank webs by the same authority as Tables I. and II.

Table V. gives further results, by different authorities and makers, of the physical properties of steel castings.

Table VI. has been supplied by Mr. James Riley, of the Steel Company of Scotland, and represents the quality of castings turned out by that firm. It is complete and needs no explanation, but the elongations on 8 inches deserve mention.

It may therefore be concluded that steel castings can be supplied very much superior to iron castings or forgings, and to rival those forgings made of hammered or wrought steel. It must be remembered that in a crank axle or any other forging, hammering makes a hard skin which never gets any hotter as the forging cools, consequently internal strains arc set up, and the centre metal is of little use from a physical point of view, and the cruciform shape taken by a pipe in an ingot is well known.

From the foregoing results, it would be reasonable to specify that the castings shall be made in close-grained steel of uniform quality, perfectly sound, free from honeycomb or other defects, and of 28 to 34 tons tenacity per square inch, with a minimum elongation of 15 per cent. on 2 inches; longer bars being difficult to obtain sound when attached to castings. The bending tests to be made upon bars 1¬ inches square, which should be capable of bending cold without fracture over a radius not greater than about one and a half times the thickness of the sample, and through an angle depending upon the ultimate strength; this angle to be not less than 90° at 28 tons, and 60§ at 34 tons per square inch, and in proportion for strengths between those limits. At the present time all locomotive castings are made to the above specification when nothing otherwise has been specified, and all the engine castings for the Admiralty are made to the same limits. The castings to he thoroughly annealed for reasons already stated.

Table I

Test mark

Analysis - per cent.

Section.

Stress.

Fracture

Remarks

Carbon

Silicon.

Managanese

Length

Diameter.

Original area In sq, Inches

First per, set induced

Tons per sq. inch

Breaking stress

Tons per sq. inch

Cohesive force.

Contraction of Area.

Per cent

Elongation per cent. on

2-inch length

SA19

.30

.22

.63

1.75

.533

.223

27'0

31.0

55.1

43-8

24

Annealed.

"

"

"

"

"

"

"

30.4

55.1

43-8

24

Do.

"

"

"

"

"

"

"

19.2

33.4

56.4

41.0

24

Do.

31.6

42.8

24

Average.

HA 13

"

"

"

"

"

"

336

46.6

26-84

16

Not annealed.

28.7 =

Percentage advantage.

SA18

.35

.23

.61

1.75

.533

.223

33.0

56.0

41.0

22.2

Annealed.

"

"

"

"

"

"

19-0

36.0

57.1

37.06

21.5

Do.

"

"

"

"

"

"

"

Spoiled in tooling

Do.

34.5

39.03

21.8

Average

ha 18

"

"

"

"

"

"

Spoiled in tooling

Not annealed.

Percentage advantage.

SA48

.50

-41

.66

175

.533

.223

44.0

52.9

16.8

12

Annealed

"

"

"

"

"

"

"

24

45.2

48.29

6.3

5

Do,

"

"

"

"

"

"

"

42.2

48.06

12.3

8

Do.

43.8

11.8

8.6

Average

HA 48

"

"

"

"

"

"

44.4

46.2

4.13

2

Not annealed.

27.1 =

Percentage advantage.

SA60

.77

.46

.67

1.76

.533

.223

39.8

40.34

1.35

10

Annealed,

"

"

"

"

"

"

39.0

40.34

3.3

1.9

Do.

"

"

"

"

"

"

32.4

33.6

34.21

1.8

1.5

Do.

"

37.4

2.15

11

Average

HA 60

"

"

"

"

"

"

36.4

36.61

0.8

Nil

Not annealed.

10.2 =

Percentage advantage.

SA82

.98

.62

'64

1.75

.533

.223

37.0

31-71

2-24

2

Annealed

"

"

"

"

"

"

"

38.0

38.3

0.80

1

Do.

"

"

"

"

"

"

"

35.6

36.2

1.80

1

Do.

"

34.8

1.61

1.3

Average

HA 82

"

"

"

"

"

"

37.0

37.3

0.8

Nil

Not annealed.

Table II

Test marks

Analysis.

Section.

Stress.

Fracture.

Elongation in percentage in a length of -

Remarks.

Carbon.

Silicon.

Manganese.

Length.

Diameter.

Area.

First per. set.

Tons per sq.

inch.

Breaking. Tons per sq.

inch.

Cohesive force

Reduced area.

Inches

Contraction

.of area.

Per cent.

5 in.

4 in.

3 in.

028

.41

.32

.47

5

.745

.4359

15.26

33.79

36.8

.4003

8.16

12

_

19

Not annealed

Taken from the git of a hydraulic riveter casting.

021

.26

-

-

"

.754

.4464

-

32.8

48.17

.2734

38.7

22

-

37

Annealed

024

.47

.30

.64

"

.741

.4310

15.5

32.1

33.10

.418

2.9

416

-

6

Not annealed

Taken from the git of a hydraulic cylinder

Casting.

025

.85

-

-

"

.710

.3959

13.26

36.6

50.66

.284

28.11

14.6

-

24

Annealed

151 8

.35

-

-

"

.754

.4464

11.7

32.3

50.27

.2734

38.7

15

-

28

Do.

027

.42

.33

.49

"

.768

.4512

19.8

24.01

24.80

.4382

2.8

1

1

-

Not annealed

Taken from the git of a hornblock.

020

.42

-

-

„"

.766

.4488

11.8

28.4

34.30

.375

15.9

18

-

16

Annealed

S 25

.47

.33

.47

"

.724

.4166

13.12

30.08

40.36

.3067

23.05

21.9

23.4

28

Do.

Taken from the gits of

059

.41

-

-

.757

.4500

19.54

38.19

43.05

.399

11.28

-

11.5

13

Do

060

.41

-

-

"

.757

.4500

19.04

37.69

42.37

.400

11.04

-

10

12

Do

0157

.35

-

-

"

.754

.4466

19.0

38.3

45.60

.375

16.01

14.6

14.5

16

Do.

Taken from the gits of horn-blocks & axle-boxes.

0158

.35

-

_

"

.754

.4465

18.69

38.5

48.85

.3462

22.46

19.25

20

22.5

Do.

0159

.35

-

-

"

.747

.4382

18.64

38.4

47.59

.3536

19.30

17.8

18

21.5

Do.

06567

-

-

-

"

.539

..2281

18.60

31.32

59-83

.1194

47.65

-

-

26.5

Do.

4 ft. 4 in. wheel centre.

06568

-

-

_

"

.548

.2358

15.19

30.24

56.77

.1256

46.78

-

-

28.0

Do.

2 ft. 6 in. wheel centre.

06883

-

-

_

.540

.2290

17.5

35.6

39.92

.2042

10.8

-

-

14.5

Do.

Trolley wheel.

06915

-

-

-

"

.540

.2290

13.62

28.4

34.10

.1907

16.7

-

-

32.0

Do.

Piston.

Table III

Test mark.

Section.

Stress.

Strain.

Remarks.

Length of the Bar.

Distance between Supports.

Size of Specimen.

B x D2.

Elastic limit.

Maximum

Stress in tons per sq. in.

Deflection.

Angle through which the Speci-men passed.

Δ 79

inches. 14

inches. 10

in. sq.

1.9531

tons per sq. in. 24.00

tons per sq. in. 45.25

5.73

deg. 127

Not broken.

" 84

"

"

"

"

27.77

56.53

3.55

87.5

Broken.

" 85

"

"

"

"

27.77

49.37

1.12

29.5

Do.

" 87

"

"

"

"

28.11

54.85

5.80

126

Not broken.

" 89

"

"

"

"

27.42

51.42

5.50

119.5

Do.

" 90

"

"

•»

"

27.42

51.42

5.40

119

Do.

" 96

"

"

"

"

28.11

51.43

5.84

125

Do.

" 97

"

"

"

"

27.42

51.77

5.71

124

Do.

The wheel centres are required by some users to be rough turned, leaving ⅛ inch for finishing where they have to be finished bright. One wheel in fifty to be supplied by the contractor free of cost, selected from the bulk and tested to destruction. From this sample the tensile and bending test will be taken, the results of which will be accepted as the average quality of the whole. It is further required by some users of wheel centres, that each be dropped in a running position, on the end of a spoke, from a height of 2 feet, and allowed to fall upon a rail secured to the top of an ingot of at least 2 tons weight, after which the wheel must be turned round through an angle of 90°, and dropped again in a similar manner. Each casting must be then slung up and hammered with a 7-lb. hammer to ascertain that it is sound. Clauses as to inspection and warranty are inserted to suit the purchaser; the latter is generally for twelve months from the date of commencing work.

Table IV

Test mark.

Length for torsion.

Diameter in inches

Original area in sq. in.

Elastic limit in tons per sq. in.

Maximum stress in tons per sq. in.

Angle through which piece twisted for two diameters long.

S 741

2.256

1.128

1.0

7.617

31.015

Deg.

274

S 742

"

"

"

8.161

30.470

275

S 741

"

"

"

9.794

32-647

2S2

S 742

"

"

9.794

29-926

213

013

"

..

"

7.6l0

30 400

278

014

"

"

"

9.790

31.010

271

015

"

"

"

7.610

31.550

285

016

"

"

"

8.700

32-640

316

Table V

Test mark.

Authority.

Maker.

Length of Specimen.

Section.

Stress.

Strain.

Fracture.

Remarks.

Dimensions. Inches.

Area. Square inches.

Elastic limit. Tons per sq. in.

Breaking weight.

Tons per sq. in.

Ultimate sets. Inches.

Per cent. of original length.

Area. Square inches.

Contraction per cent.

Appearance.

Bends.

C 337

Hadfield

Hadfield's Steel Foundry Co.

2

.7979

•5

-

32.5

-

29.0

-

40.4

deg.

C 2¬ B

"

"

"

-

32.5

-

27.9

-

33.4

C 147

"

"

"

-

34.5

-

27.7

-

352

C 2¬ A

"

"

"

-

32.0

-

26.8

-

30.9

C 111

"

"

"

-

40.0

-

19.0

-

20.0

C 117

"

"

"

-

45.0

-

15.0

-

18.0

C 1

"

"

"

-

52.0

-

4.0

-

6.3

C2

"

"

"

-

56.8

-

4.0

-

5.5

C3

"

"

"

-

64.0

-

6.0

-

8.0

"

-

-

-

26.0

-

36.5

-

40.4

1st centre arm

Loco, wheel centres.

"

-

-

-

26.0

-

37.6

-

50.0

" " rim

"

-

-

-

27.0

-

28.5

-

33.6

" " bal. weight

"

-

-

-

26.5

-

20.6

-

223

2nd „ arm

3223

"

.540

.229

-

31.1

•60

30.0

.1190

48.0

"

3224

"

.500

.196

-

32.6

•55

27.5

.1070

45.4

"

3435

"

.560

.246

-

32.5

•27

13.5

.2200

10.5

Granular & fibrous

3436

"

.565

.250

-

31.2

•34

17.0

.2000

20.0

" 30% "

3437

"

.565

.250

-

31.6

•60

30.0

.1350

46.0

Fibrous

3438

Snowdon

John Rogerson & Co., Wol-singham, Darlington.

2

-

.237

18.6

32.4

•64

32.0

.1194

49.6

100% fibrous

180

Not broken.

Size ⅝" and [¾" radius

3439

"

-

.216

18.5

32.9

•60

30.0

.1244

42.3

" " "

"

Do.

3441

"

-

.223

18.8

32.2

•62

31.0

.1152

48.3

" " "

"

Do.

3442

"

-

.227

17.3

31.7

•65

32.5

.1134

50.0

" " "

"

Do.

3443

"

-

.227

19.8

37.0

•45

22.5

.1661

26.8

20% fib., 80% gran.

"

Do.

3444

"

-

.225

18.3

31.6

•62

31.0

.1225

45.5

Fibrous " "

"

Do.

3445

"

-

.214

17.7

32.2

•60

30.0

.1134

46.9

" ....

"

Do.

3472

"

-

.223

20.1

35.2

•50

25.0

.1520

31.8

4% fib., 96% gran.

115

Broken. Size

⅝" and 7/16"

[radius

3473

"

-

.220

16.5

30.4

•65

32.5

.1134

48.0

100% fibrous

180

Not broken.

3474

"

-

.212

19.6

32.4

•60

30.0

.1134

46.5

" "

85

Broken.

3475

"

-

.220

17.8

32.3

•65

32.5

.1194

45.7

" "

180

Not broken.

3476

"

-

.220

18.5

34.6

•52

26.0

.1520

30.9

10% fib., 90% gran.

100

Broken.

3477

"

-

.224

18.4

32.0

•60

30.0

.1452

35.1

100% fibrous

180

Not broken.

3478

"

-

.233

18.5

35.0

•42

21.0

.1960

15.8

100% granular ..

180

Do.

3479

"

-

.220

18.6

31 4

•60

30.0

.1194

45.7

100% fibrous

180

Do.

Table VI

Test mark.

Length of Specimen.

Section.

Stress

Strain.

Fracture

Bends without

Fracture

Remarks.

Passed by inspector.

Diameter.

Area.

Square inches.

Elastic limit.

Tons per square inch.

Ultimate lead. Tons per square inch.

Extension.

inches.

Per cent.

Area

Square inches.

Contraction pet cent.

Appearance

in.

deg.

Y 272

2

.76

.463

20.5

34.9

.65

32.5

237

47.6

Silky

180

Engine coatings

Admiralty

Y 282

"

.75

.441

20.6

34.7

.65

32.5

.212

51.9

"

180

"

"

Z 683

"

.77

.465

19.7

35.2

.60

30.0

.220

52.7

"

180

"

"

Z 689

"

.77

.465

19.3

33.3

.65

32.5

.246

47.5

"

180

"

"

Z 696

"

.78

.477

19.4

32.7

.70

35.0

.220

53.8

"

180

"

"

Z 703

"

.75

.441

19.9

35.3

.75

37.5

.196

55.5

"

180

"

"

Z 716

"

.80

.502

19.1

31.4

.75

37.5

.255

49..2

"

180

"

"

Z 719

"

.79

.490

18.1

31.8

.70

35.0

.229

53.2

"

180

"

"

Z 739

"

.76

.453

17.0

29.3

.70

35.0

.237

47.6

"

180

"

"

No. 1

1.13

1.002

19.8

33.8

.75

37.5

.502

49.8

"

180

"

Russian Government

" 7

"

.89

.622

18.0

30.4

.75

37.5

.301

51.6

"

110

"

" "

.. 13

"

.88

.608

18.9

32.5

.70

35.0

.311

48.8

"

99

"

" "

" 15

"

1.11

.967

18.6

32.4

.72

36.0

.477

50.6

"

99

"

" "

" 10

"

.99

.769

18.3

32.5

.75

37.5

.390

50.7

"

100

Locomotive wheel

Railway

,. 11

"

.99

.769

18.3

31.4

.70

35.0

.385

50.0

"

100

centres

"

" 12

"

1.00

.785

17.9

31.5

.70

35.0

.410

52.2

"

100

"

"

" 330

8

.88

.608

17.0

29.4

2 .20

27.5

.311

48.8

"

90

Ship castings

Lloyds

„ 353

"

.85

.567

17 4

29.2

2.00

25.0

.284

50.0

"

94

"

"

" 373

"

.85

.567

18.4

30.3

1.84

23.0

.295

52.0

"

127

"

"

" 374

"

.84

.554

18.1

29.9

2.40

30.0

.290

52.5

"

127

"

"

As far as the analysis is concerned, probably it is best left in the hands of the steel maker, because so much depends upon the process. Sometimes a good analysis gives worse physical results than an interior one, owing to the working of the charge during the earlier or latter stages of the heat; however, castings having an analysis of C '18 to .28, Si .20 to .40, S .02 to .07, P .03 to .07, Mn .3 to . 75, would give similar results to those tabulated in Table V. under the second authority, providing that the heat had been worked to the best advantage. Finally, in a great number of observations made by the author for Mr. Aspinall, it was observed throughout, that the highest carbon with simultaneous high silicon gave the worst castings, and the best results were when the carbon was .28 per cent., or below, or when the content of carbon was from 10 to 26 per cent, less than that of silicon. Perhaps this does not quite coincide with a comparison of Tables I. and II., but it must be remembered that these tables are given for specific reasons. The first, to show the effect of annealing and also chemical composition, and therefore various percentages of elements may be expected; whereas Table II. shows chiefly the remarkable reduction of the content of combined carbon by annealing. The reliability of these tables is unimpeachable, they satisfy a specific purpose, but the author's personal experience of the physical and analytical results of some hundreds of castings, is summed up by low carbon in conjunction with high silicon or vice versa, these conditions being imperative, .26 per cent, carbon being the highest preferable amount for mild castings. High silicon with low carbon will work admirably in the forge, with as much as 1.5 per cent, of the former, providing the latter is very low, say about 15 per cent.

Table VI ConstructionOfModernLocomotive 80Table VI ConstructionOfModernLocomotive 81

Fig. 89.

Table VI ConstructionOfModernLocomotive 82

Fig. 90.

Table VI ConstructionOfModernLocomotive 83

Fig. 92.

Table VI ConstructionOfModernLocomotive 84Table VI ConstructionOfModernLocomotive 85

Fig. 93.

Table VI ConstructionOfModernLocomotive 86Table VI ConstructionOfModernLocomotive 87Table VI ConstructionOfModernLocomotive 88Table VI ConstructionOfModernLocomotive 89

Fig. 100.

Table VI ConstructionOfModernLocomotive 90

Fig. 101.

In Fig. 87 is seen one-half of the motion plate, from the centre line of the engine to the right frame, with its forked attachment for securing one end of the anchor link of Joy's motion, whilst an end view is shown in Fig. 88. Two views of the cross-head are given in Figs. 89 and 90, to which may be cast sufficient metal to be drawn down in the forge to the required dimensions of the piston rod. The driving wheel centre is given in Fig. 91, the leading and trailing being identical, with the exception of the balance weights, which are of course very much lighter; Fig. 92 being a half section through the crank pin boss. Figs. 93 and 94 are sections of the arms at the top and bottom. Reference has already been made to the designs of wheel centres, as well as the horn-block, which is shown in Fig. 98, with its keep, Fig. 99. This horn-block is of a useful design, but is frequently modified to suit the various types of locomotives built by different engineers. The Joy reversing shaft is shown in plan and elevation in Figs. 95, 96, and a cross-section, Fig. 97. Figs. 100 and 101 give two views of the brake hanger, which is swung from the frame at one end, coupled up to the brake cylinder by means of suitable connecting rods from the other, and having the cast-iron brake block attached in the centre, Figs. 105 and 106 being the tender brake shaft, The firebox foundation ring is given in cross-section in Fig. 102 and in isometric in Fig. 102a. The cross stay between the frames in front of the fire-box is shown in Fig. 103, and the safety-valve seating in Fig. 104. Similar designs to Fig. 104 are adopted for the mud collector in the barrel, just in front of the fire-box, and also where cast-steel domes are used they require a similar seating. Fig. 107 is the tender spring link, and the draw bar spring box is shown in section in Fig. 108.

Table VI ConstructionOfModernLocomotive 91

Fig. 102A.

Table VI ConstructionOfModernLocomotive 92

Fig. 104.

Table VI ConstructionOfModernLocomotive 93

Fig. 105.

Table VI ConstructionOfModernLocomotive 94

Fig. 108.

Table VI ConstructionOfModernLocomotive 95