US775376A - Tandem-compound-engine bushing. - Google Patents
Tandem-compound-engine bushing. Download PDFInfo
- Publication number
- US775376A US775376A US21994404A US1904219944A US775376A US 775376 A US775376 A US 775376A US 21994404 A US21994404 A US 21994404A US 1904219944 A US1904219944 A US 1904219944A US 775376 A US775376 A US 775376A
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- US
- United States
- Prior art keywords
- bushing
- piston
- tandem
- pressure
- compound
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/26—Sealings between relatively-moving surfaces with stuffing-boxes for rigid sealing rings
- F16J15/28—Sealings between relatively-moving surfaces with stuffing-boxes for rigid sealing rings with sealing rings made of metal
Definitions
- This invention relates to the bushing placed around the piston-rod between the high and low pressure cylinders in a tandem compound steam-engine, and has for its objects to increase the efficiency of the bushing by decreasing the leak of steam from the high to the low pressure cylinder and to increase the life of the bushing by making it self-adjusting and to decrease the wear of the pistonrod at the end near the high-pressure piston by decreasing the leak of steam as above stated.
- Figure 1 is a vertical longitudinal section of the high and low pressure cylinders of a tandem compound engine equipped with my improved bushing.
- Fig. 2 is an enlarged vertical longitudinal section of, the bushing, and
- Fig. 3 is an end view thereof looking from the low-pressure cylinder toward the high-pressure cylinder.
- my bushing is constructed in two parts, each part divided into three pieces.
- the part 15 of my bushing is nearest the low-pressure cylinder 2, and consists of a short cylindrical sleeve with a short flange 16 engaging in the recess 14: in the wall 11.
- This part 15 does not fit tightly in the passage 13, but fits the piston-rod except at the three points where it is cut, Fig. 3.
- the flange 16 fits tightly against the side of the recess 1& except where it is cut.
- the flange 16 is practically half as thick as the recess 1 L.
- the part 17 of the bushing is nearest the high-pressure cylinder 1 and consists of a short cylindrical sleeve practically of the same dimensions as the sleeve of the part and has a flange 18, which is adapted to fit exactly into the recess 14 between the wall 11 and the cone 12, but which is recessed to accurate lit over the flanges 16 of the part 15.
- the part 17 is also cut into three pieces, and when the parts 15 and 17 are assembled they are arranged as shown in Fig. 3, so that the open spaces between the pieces of the part 15 do not come near the similar open spaces between the pieces of the part 17, and they are retained in their proper relative positions by the dowelpin 19.
- Circular spiral springs 20 hold the pieces of the parts 15 and 17 together. I prefer to use two such springs placed in grooves on the outside of the sleeves of each of the parts and 17.
- a tandem-compound-engine bushing the combination with the wall between the high and low pressure cylinders having a pistonrod passage therein and with a recess in the end of said passage nearest the high-pressure cylinder, a casting within said high-pressure cylinder and constructed so as to continue the piston-rod passage and so as to form one side of said recess, a split bushing within said passage in said wall and having a circular flange engaging in said recess, a split bushing within said passage in said casting and having a flange of greater diameter than the flange on the first bushing and further having a recess in said flange adapted to fit over said flange on said first bushing and means for retaining said bushings from turning relatively to each other.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
Description
No. 775.376 PATENTED NOV. 22, 1904. J. METZGER.
TANDEM COMPOUND ENGINE BUSHING.
APPLICATION FILED AUG. 8, 1904.
N0 MODEL.
W/TNESES I INVENTOH W69, (/2950 fi/6/zyer W1 y VG/n H m k UNITED STATES Patented November 22, 1904:.
JOHN METZGER, OF TACOMA, IVASHINGTON.
TANDEM-COMPOUND-ENGINE BUSHING.
SPECIFICATION forming part of Letters Patent No. 775,376, dated November 22, 1904.
Application filed August 8, 1904.
T (ZZZ whmn it may concern.-
Be it known that 1, JOHN METZGER, a citizen of the United States of America, residing at Tacoma, in the county of Pierce and State of \Vashington, have invented certain new and useful Improvements in Tandem-Compound-Engine Bushings, of which the following is a specification,reference being had therein to the accompanying drawings.
This invention relates to the bushing placed around the piston-rod between the high and low pressure cylinders in a tandem compound steam-engine, and has for its objects to increase the efficiency of the bushing by decreasing the leak of steam from the high to the low pressure cylinder and to increase the life of the bushing by making it self-adjusting and to decrease the wear of the pistonrod at the end near the high-pressure piston by decreasing the leak of steam as above stated.
I attain these objects by the devices illustrated in the accompanying drawings, in which Figure 1 is a vertical longitudinal section of the high and low pressure cylinders of a tandem compound engine equipped with my improved bushing. Fig. 2 is an enlarged vertical longitudinal section of, the bushing, and Fig. 3 is an end view thereof looking from the low-pressure cylinder toward the high-pressure cylinder.
Similar numerals of reference refer to similar parts throughout the several views.
One of the principal obstacles to the successful working of tandem compound steamengines, especially locomotives, is found in the diiiiculty in keeping the highpressure steam from leaking through the bushing to the low-pressure cylinder when the pistons are on the inward stroke, as shown in Fig. 1, because the full boiler-pressure is applied to one side of the bushing, while the other side is connected to the condenser or to the atmosphere through the exhaust. This unequal pressure is greatest when at the beginning of the inward stroke. The usual construction As soon as this Serial No. 219,944. No modelfi rially wear the piston-rod near the high-pres-- sure piston and would thus reduce the efliciency of the engine every inward stroke.
In the drawings I have indicated the highpressure cylinder at 1, the low-pressure cylinder at 2, the high-pressure piston at 3, the low-pressure piston at 4, the piston'rod at 5, the steam-inlet passage at 6, the valve-chest and intermediate chamber at 7, the high-pressure Valve at 8, the low-pressure valve at 9, the exhaust-passage at 10, the wall between the high and low pressure cylinders at 11, the cone in the high-pressure cylinder at 12, the passage through the wall 11 and the cone 12 at 18, and the recess in the wall 11 from the passage 13 at 14.
In none of the above parts have I changed the usual method of constructing the engine.
Referring principally to Figs. 2 and 3, it will be seen that my bushing is constructed in two parts, each part divided into three pieces. The part 15 of my bushing is nearest the low-pressure cylinder 2, and consists of a short cylindrical sleeve with a short flange 16 engaging in the recess 14: in the wall 11. This part 15 does not fit tightly in the passage 13, but fits the piston-rod except at the three points where it is cut, Fig. 3. The flange 16 fits tightly against the side of the recess 1& except where it is cut. The flange 16 is practically half as thick as the recess 1 L.
The part 17 of the bushing is nearest the high-pressure cylinder 1 and consists of a short cylindrical sleeve practically of the same dimensions as the sleeve of the part and has a flange 18, which is adapted to fit exactly into the recess 14 between the wall 11 and the cone 12, but which is recessed to accurate lit over the flanges 16 of the part 15. The part 17 is also cut into three pieces, and when the parts 15 and 17 are assembled they are arranged as shown in Fig. 3, so that the open spaces between the pieces of the part 15 do not come near the similar open spaces between the pieces of the part 17, and they are retained in their proper relative positions by the dowelpin 19. Circular spiral springs 20 hold the pieces of the parts 15 and 17 together. I prefer to use two such springs placed in grooves on the outside of the sleeves of each of the parts and 17.
It is evident that as the piston-rod 5 or the bushings 15 and 17 wear the bushing will close around the piston-rod and will always keep a steam-tight joint along the rod between the two cylinders 1 and 2, and the flanges will always form a steam-tight joint around the bushings. Further, the flange 18 of the part 17 nearest the high-pressure cylinder incloses the flange 16 of the part 15. As the pressure of the steam around the part 17 is greater than the pressure around the part 15, the wear of the part 17 will tend to be greater than that of'the part 15; but as the flange 18 surrounds the flange 16 it immediately increases the pressure on the part 15, and thus distributes the pressure all along the bushing. This arrangement tends to stop the wear of the piston-rod 5 at the point Where at present it always shows the greatest wearnamely, near the I highpressure piston. The flanges 16 and 18 prevent the passage of steam around the outside of the bushing.
In practice I find that tandem compound locomotives fitted with my bushing have run for many months with no measurable wear to the piston-rod and but very little to the bushing, whereas the same locomotives needed a renewal of bushings every four weeks and the piston-rods needed returning every six months. The advantage, therefore, of my bushing is apparent.
Having now described my invention, what I claim, and desire to secure by Letters Patent, is
In a tandem-compound-engine bushing, the combination with the wall between the high and low pressure cylinders having a pistonrod passage therein and with a recess in the end of said passage nearest the high-pressure cylinder, a casting within said high-pressure cylinder and constructed so as to continue the piston-rod passage and so as to form one side of said recess, a split bushing within said passage in said wall and having a circular flange engaging in said recess, a split bushing within said passage in said casting and having a flange of greater diameter than the flange on the first bushing and further having a recess in said flange adapted to fit over said flange on said first bushing and means for retaining said bushings from turning relatively to each other.
In testimony whereof I afliX my signature in presence of two witnesses.
JOHN METZGER.
WVitnesses:
M. H. CoNY, WV. E. WVINDsoR.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US21994404A US775376A (en) | 1904-08-08 | 1904-08-08 | Tandem-compound-engine bushing. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US21994404A US775376A (en) | 1904-08-08 | 1904-08-08 | Tandem-compound-engine bushing. |
Publications (1)
Publication Number | Publication Date |
---|---|
US775376A true US775376A (en) | 1904-11-22 |
Family
ID=2843861
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US21994404A Expired - Lifetime US775376A (en) | 1904-08-08 | 1904-08-08 | Tandem-compound-engine bushing. |
Country Status (1)
Country | Link |
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US (1) | US775376A (en) |
-
1904
- 1904-08-08 US US21994404A patent/US775376A/en not_active Expired - Lifetime
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