US1292101A - Piston-ring. - Google Patents
Piston-ring. Download PDFInfo
- Publication number
- US1292101A US1292101A US20268717A US20268717A US1292101A US 1292101 A US1292101 A US 1292101A US 20268717 A US20268717 A US 20268717A US 20268717 A US20268717 A US 20268717A US 1292101 A US1292101 A US 1292101A
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- US
- United States
- Prior art keywords
- ring
- piston
- cylinder
- expansion
- formation
- 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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Classifications
-
- 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
- F16J9/00—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
- F16J9/12—Details
- F16J9/14—Joint-closures
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/49274—Piston ring or piston packing making
- Y10T29/49277—Piston ring or piston packing making including casting or molding
Definitions
- This invention relates to that type of single piece cast metal piston rings which rely upon the natural resiliency of the metal to maintain the ring in roper place and action after assemblage, and to Wh1ch end the ring is made of an open or split shape with the ends formed-for lapping interengagement, and the present improvement has for its object p
- Fig. 2 is a transverse sectional elevation, illustrating the piston ring in its normal contracted condition and in assembled relation to the piston and cylinder of an engine.
- Fig. 3 is a 'central sectional elevation iston and cylinder illustrating an engine lty of the present provided with a plura piston rings.
- Fig. 45 is a detail perspective view of the 7 joint between the ring ends at the split separation of said ring, the parts being shown in the interengaged condition assumed in actual use.
- Fig. 5 is a similar view, showing the parts in the disengaged condition of said parts lafter manufacture 'and previous to assemla e.
- . i 6 is an enlarged section on line X i", Fig. 2, of the piston, cylinder and the iston ring.
- 1 designates the piston ring having the usual rectangular form in cross-section and formed with a single split or opening 2.
- the material part of the present improvement consists in makthe side of the rin ing the aforesaid splitor open piston ring ment of the same inside the initially inner most end of the ring, the formation of the interengaging surfaces being such, that leakage of the motive fluid at such point is prevented, and preferably by a special formation of such ends or terminal portions as follows v
- the aforesaid interengaging members or portions 3 and 4 shown in Figs.
- the member or portion 3 is formed by a cavity 5 in the perimeter of the ring member 1 and at an outer corner of the same, said cavity being preferably of a curved form in cross-section as shown, while the other member or portion 4 is formed by a tongue 6, of reduced dimensions, also formed at the perimeter of the ring member 1 and at an outer corner of the same, said tongue 6 having a cross-sectional formation adapted to fit and have movement in the cavity 5 above described.
- member 1 into which the cavity 5 opens e arranged toward the directionof pressure stress in an engine cylinder, and where pressure stress prevails alternately in opposite directions in the engine cylinder, a plurality of piston ring members 1 arranged in reversed order will be employed, as illustrated in Fig. 3.
- An expansion piston ring comprising a circumferentially separated annulus having an initial flat spiral formation with an inherent resilient tendency to circumferential expansion when contracted, saidring the ring body to a circular form and impose circumferential expansion thereon under the inherent tendency of the ring body to return to its initial spiral form, substantially as set forth.
- An expansion piston ring comprising wearer a circumferentially separated annulus having an initial flat spiral formation With an inherent resilient tendency to circumferential expansion when contracted, said ring being provided With inter-engaging formations at the point of separation, which when the ring body is contracted to attain an inter-engagement of said formations and the placing in the bore of an engine cylinder, said inter-engaged formation in connection With the cylinder bore are adapted to hold the rin body to a circular form and impose circumferential expansion thereon under the inherent tendency of the ring body to re-- turn to its initial spiral form, said interengaging formations comprising a curved peripheral cavity' formed in an outer corner of the ring body and a reduced tongue of a size to fit said cavity, substantially as set forth.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
Description
J. SHAW.
PISTON RING.
APPLICATION FILED NOV. 19. 1917.
Patented Jan. 21,1919. 1
' JAMES SHAW, OF CHICAGO, ILLINOIS.
PISTON-RING.
Specification of Letters Patent.
Application filed November 19. 1917. Serial N 0. 202,687.
To all whom it may concern: Be it known that I, JAMES SHAW, a citi- I zen of the United States of America, and a resident of Chicago, in the county of Cook, State of Illinois, have invented certain new and useful Improvements in Piston-Rings, of which the following is a specification.
This invention relates to that type of single piece cast metal piston rings which rely upon the natural resiliency of the metal to maintain the ring in roper place and action after assemblage, and to Wh1ch end the ring is made of an open or split shape with the ends formed-for lapping interengagement, and the present improvement has for its object p To provide a simple and efiicient structural formation of a piston ring of the type above mentioned, whereby an even and uniform expanding resiliency of the ring is attained, and with which a true circularity of the ring, when contracted to fit an engine piston and c linder, is also attained,
all as will hereina er more fully appear.
In the accompanying drawing Figure 1, is an elevation of the present 7 ring structure in an uncontracted condition,
after -manufacture and before assemblage.
Fig. 2 is a transverse sectional elevation, illustrating the piston ring in its normal contracted condition and in assembled relation to the piston and cylinder of an engine.
Fig. 3, is a 'central sectional elevation iston and cylinder illustrating an engine lty of the present provided with a plura piston rings.
Fig. 45, is a detail perspective view of the 7 joint between the ring ends at the split separation of said ring, the parts being shown in the interengaged condition assumed in actual use.
Fig. 5, is a similar view, showing the parts in the disengaged condition of said parts lafter manufacture 'and previous to assemla e.
. i 6, is an enlarged section on line X i", Fig. 2, of the piston, cylinder and the iston ring.
Referring to the drawing, 1 designates the piston ring having the usual rectangular form in cross-section and formed with a single split or opening 2. The material part of the present improvement consists in makthe side of the rin ing the aforesaid splitor open piston ring ment of the same inside the initially inner most end of the ring, the formation of the interengaging surfaces being such, that leakage of the motive fluid at such point is prevented, and preferably by a special formation of such ends or terminal portions as follows v In the preferred construction of the aforesaid interengaging members or portions 3 and 4, shown in Figs. 4, 5 and 6 of the drawing, the member or portion 3 is formed by a cavity 5 in the perimeter of the ring member 1 and at an outer corner of the same, said cavity being preferably of a curved form in cross-section as shown, while the other member or portion 4 is formed by a tongue 6, of reduced dimensions, also formed at the perimeter of the ring member 1 and at an outer corner of the same, said tongue 6 having a cross-sectional formation adapted to fit and have movement in the cavity 5 above described. i
With the present piston ring structure, as the spiral ring member 1, shown in Fig.
Patented Jan. 21, 1919.
and 4 in the inter-engaged condition above described. During such operation the ring 1 assumes a true circular shape corresponding with'that of the bore of the engine cylinder 7, and owing to the described interengagement of the end or terminal portions of the piston ring, all expansion tendency of the ring is in a. circumferential manner. In practice it has been found that such circumferential expansion maintains the iston ring in proper circular shape during t e life of the ring, with an avoidance of undue fric tion and lrregular wear of the engine cylinder usual to the ordinary single piece split expansion rings now in general use.
For efiicientoperation it is advisable that member 1 into which the cavity 5 opens, e arranged toward the directionof pressure stress in an engine cylinder, and where pressure stress prevails alternately in opposite directions in the engine cylinder, a plurality of piston ring members 1 arranged in reversed order will be employed, as illustrated in Fig. 3.
Having thus fully described my said invention, What I claim as new and desire to secure by Letters Patent, is
1. An expansion piston ring, comprising a circumferentially separated annulus having an initial flat spiral formation with an inherent resilient tendency to circumferential expansion when contracted, saidring the ring body to a circular form and impose circumferential expansion thereon under the inherent tendency of the ring body to return to its initial spiral form, substantially as set forth.
' 2. An expansion piston ring, comprising wearer a circumferentially separated annulus having an initial flat spiral formation With an inherent resilient tendency to circumferential expansion when contracted, said ring being provided With inter-engaging formations at the point of separation, which when the ring body is contracted to attain an inter-engagement of said formations and the placing in the bore of an engine cylinder, said inter-engaged formation in connection With the cylinder bore are adapted to hold the rin body to a circular form and impose circumferential expansion thereon under the inherent tendency of the ring body to re-- turn to its initial spiral form, said interengaging formations comprising a curved peripheral cavity' formed in an outer corner of the ring body and a reduced tongue of a size to fit said cavity, substantially as set forth.
Signed at Chicago, Illinois, this14th day of November, 1917.
" JAMES SHAW.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US20268717A US1292101A (en) | 1917-11-19 | 1917-11-19 | Piston-ring. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US20268717A US1292101A (en) | 1917-11-19 | 1917-11-19 | Piston-ring. |
Publications (1)
Publication Number | Publication Date |
---|---|
US1292101A true US1292101A (en) | 1919-01-21 |
Family
ID=3359659
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US20268717A Expired - Lifetime US1292101A (en) | 1917-11-19 | 1917-11-19 | Piston-ring. |
Country Status (1)
Country | Link |
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US (1) | US1292101A (en) |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2670257A (en) * | 1950-06-21 | 1954-02-23 | Bergeron Alfred | Piston ring |
US4844487A (en) * | 1988-11-04 | 1989-07-04 | Kaydon Corporation | Lock-step duo step split sealing ring |
US5028055A (en) * | 1989-03-31 | 1991-07-02 | Leber Corp. | Substantially zero leakage path sealing assembly with additional line to line ring |
US5058904A (en) * | 1990-02-21 | 1991-10-22 | Eg&G Sealol Inc. | Self-contained sealing ring assembly |
US5071142A (en) * | 1989-03-31 | 1991-12-10 | Leber Corporation | Bi-directional substantially zero leakage path sealing assembly |
US5147094A (en) * | 1989-03-31 | 1992-09-15 | Leber Corporation | Substantially zero leakage path sealing assembly with insulating member |
US5193821A (en) * | 1989-03-31 | 1993-03-16 | Leber Corporation | Substantially zero leakage path sealing assembly with zero degree bias angle |
US5197746A (en) * | 1989-03-31 | 1993-03-30 | Leber Corporation | Substantially zero leakage path sealing assembly with expander void |
US5503405A (en) * | 1991-05-07 | 1996-04-02 | General Electric Co. | Apparatus for providing uniform radial clearance of seals between rotating and stationary components |
US5509780A (en) * | 1995-03-08 | 1996-04-23 | General Electric Co. | Apparatus and method for providing uniform radial clearance of seals between rotating and stationary components |
US5752705A (en) * | 1988-12-01 | 1998-05-19 | Ae Piston Products Limited | Piston rings |
US9423028B2 (en) | 2013-08-07 | 2016-08-23 | Federal-Mogul Corporation | Piston ring |
US11525515B2 (en) * | 2020-02-11 | 2022-12-13 | Raytheon Technologies Corporation | Radial seal segment joint |
US20240200659A1 (en) * | 2022-12-15 | 2024-06-20 | Raytheon Technologies Corporation | Gas turbine engine with split helical piston seal |
-
1917
- 1917-11-19 US US20268717A patent/US1292101A/en not_active Expired - Lifetime
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2670257A (en) * | 1950-06-21 | 1954-02-23 | Bergeron Alfred | Piston ring |
US4844487A (en) * | 1988-11-04 | 1989-07-04 | Kaydon Corporation | Lock-step duo step split sealing ring |
US5752705A (en) * | 1988-12-01 | 1998-05-19 | Ae Piston Products Limited | Piston rings |
US5028055A (en) * | 1989-03-31 | 1991-07-02 | Leber Corp. | Substantially zero leakage path sealing assembly with additional line to line ring |
US5071142A (en) * | 1989-03-31 | 1991-12-10 | Leber Corporation | Bi-directional substantially zero leakage path sealing assembly |
US5147094A (en) * | 1989-03-31 | 1992-09-15 | Leber Corporation | Substantially zero leakage path sealing assembly with insulating member |
US5193821A (en) * | 1989-03-31 | 1993-03-16 | Leber Corporation | Substantially zero leakage path sealing assembly with zero degree bias angle |
US5197746A (en) * | 1989-03-31 | 1993-03-30 | Leber Corporation | Substantially zero leakage path sealing assembly with expander void |
US5058904A (en) * | 1990-02-21 | 1991-10-22 | Eg&G Sealol Inc. | Self-contained sealing ring assembly |
US5503405A (en) * | 1991-05-07 | 1996-04-02 | General Electric Co. | Apparatus for providing uniform radial clearance of seals between rotating and stationary components |
US5509780A (en) * | 1995-03-08 | 1996-04-23 | General Electric Co. | Apparatus and method for providing uniform radial clearance of seals between rotating and stationary components |
US9423028B2 (en) | 2013-08-07 | 2016-08-23 | Federal-Mogul Corporation | Piston ring |
US11525515B2 (en) * | 2020-02-11 | 2022-12-13 | Raytheon Technologies Corporation | Radial seal segment joint |
US20240200659A1 (en) * | 2022-12-15 | 2024-06-20 | Raytheon Technologies Corporation | Gas turbine engine with split helical piston seal |
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