DE3336514C1 - Spring, in particular for piston rings - Google Patents
Spring, in particular for piston ringsInfo
- Publication number
- DE3336514C1 DE3336514C1 DE19833336514 DE3336514A DE3336514C1 DE 3336514 C1 DE3336514 C1 DE 3336514C1 DE 19833336514 DE19833336514 DE 19833336514 DE 3336514 A DE3336514 A DE 3336514A DE 3336514 C1 DE3336514 C1 DE 3336514C1
- Authority
- DE
- Germany
- Prior art keywords
- spring
- connecting pin
- diameter
- stops
- circumferential direction
- 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
Links
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
- F16J9/06—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction using separate springs or elastic elements expanding the rings; Springs therefor ; Expansion by wedging
- F16J9/061—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction using separate springs or elastic elements expanding the rings; Springs therefor ; Expansion by wedging using metallic coiled or blade springs
-
- 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
- F16J9/145—Joint-closures of spring expanders
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Springs (AREA)
Abstract
Description
Um dies zu umgehen, besteht die Möglichkeit, im Bereich beider Enden des Verbindungsstiftes mindestens eine Federwindung radial in Richtung auf den Verbindungsstift zu verformen. Dies kann durch Verquetschen, Stauchen oder dergleichen mechanische Verfahren durchgeführt werden. Da hier jedoch eine nicht erwünschte Längenänderung der Feder eintreten kann, wird eine andere bevorzugte Möglichkeit zur Bildung der erfindungsgemäßen Anschläge darin gesehen, daß jeweils mindestens eine Federwindung vom Durchmesser her kleiner gewickelt wird als der Durchmesser des Verbindungsstiftes. Somit wird das Wandern des Verbindungsstiftes in Umfangsrichtung mit Sicherheit ausgeschlossen. Mit heutigen NC-gesteuerten Federwikkelautomaten entstehen bei der Massenfertigung keine zusätzlichen Kosten durch Bildung der Anschläge. To get around this, there is the option of using the area at both ends of the connecting pin at least one spring turn radially in the direction of the connecting pin to deform. This can be done by squeezing, upsetting or similar mechanical processes be performed. Since here, however, an undesirable change in length of the spring can occur, is another preferred possibility for the formation of the invention Attacks seen in that each at least one spring turn of the diameter is wound here smaller than the diameter of the connecting pin. Thus becomes the wandering of the connecting pin in the circumferential direction is definitely excluded. With today's NC-controlled spring winding machines are produced in mass production no additional costs by forming the attacks.
Zwecks optischer Hervorhebung der Anschläge besteht die Möglichkeit, mehrere Windungen kleiner und zusätzlich auch ohne Abstand voneinander zu wickeln. In order to visually highlight the attacks, there is the possibility of to wind several turns smaller and also without any distance from each other.
Die Länge des Verbindungsstiftes sollte nominal dem Maß zwischen den Anschlägen - gemessen über den Federstoß - entsprechen, um die Montage sicherzustellen. Bevorzugt ist jedoch eine geringfügig kleinere Längenabmessung des Verbindungsstiftes, um die Bewegungsarbeit der Feder im Betriebszustand nicht zu beeinflussen. The length of the connecting pin should nominally be between correspond to the stops - measured across the spring joint - to ensure assembly. However, a slightly smaller length dimension of the connecting pin is preferred, so as not to influence the movement work of the spring in the operating state.
Eine weitere vorteilhafte Ausbildung des Erfindungsgedankens ist darin zu sehen, daß die Anschläge, ausgehend von beiden Stoßenden der Feder, in Umfangsrichtung gesehen, zwischen 90" und 1200 Drehwinkel angeordnet sind. Durch diese Maßnahme wird sichergestellt, daß der Verbindungsstift lang genug ist, um bei eventuellem Fallenlassen der Feder nicht aus einem Stoßende herauszuspringen. Another advantageous embodiment of the inventive concept is to see that the stops, starting from both butting ends of the spring, in Seen in the circumferential direction, between 90 "and 1200 angles of rotation are arranged this measure will ensure that the connecting pin is long enough to not to jump out of a joint end if the spring is dropped.
Die Stiftmontage und das Federschließen können ebenfalls automatisiert werden. The pin assembly and spring closing can also be automated will.
Die Erfindung ist in der Zeichnung dargestellt und wird im folgenden näher beschrieben. Es zeigen F i g. 1 und 2: Unterschiedliche Ausbildung von Anschlägen zur Arretierung eines Verbindungsstiftes innerhalb einer Schlauchfeder. The invention is illustrated in the drawing and will be described below described in more detail. It shows F i g. 1 and 2: Different training of attacks for locking a connecting pin inside a hose spring.
Die in den F i g. 1 und 2 abgebildete Druckfeder 1 ist schlauchförmig ausgebildet und in Kreisform gebogen. The in the F i g. 1 and 2 depicted compression spring 1 is tubular formed and bent in a circular shape.
Zwischen den Stoßenden 2, 3 erstreckt sich der Federstoß 4. In beide Stoßenden 2,3 ist ein dem Krümmungsradius der zu verbindenden Federbereiche 5,6 angepaßter Verbindungsstift 7 lose eingeführt. Der innere Windungsdurchmesser der Feder list hierbei geringfügig größer ausgebildet als der Durchmesser des Verbindungsstiftes 7, um so beim Einführen eine gewisse Leichtgängigkeit sicherzustellen. Um das Wandern des Verbindungsstiftes 7 in Umfangsrichtung zu vermeiden, sind beidseitig der Enden 8, 9 des Verbindungsstiftes 7 mit der Feder 1 zusammenwirkende Anschläge 10, 11 vorgesehen.The spring joint 4 extends between the joint ends 2, 3 into both Butt ends 2.3 is the radius of curvature of the spring areas 5.6 to be connected adapted connecting pin 7 inserted loosely. The inner coil diameter of the The spring list here is made slightly larger than the diameter of the connecting pin 7, so as to ensure a certain ease of movement during insertion. About hiking of the connecting pin 7 in the circumferential direction are to be avoided on both sides of the ends 8, 9 of the connecting pin 7, stops 10, 11 cooperating with the spring 1 intended.
Gemäß Fig. 1 bestehen die Anschläge 10, 11 aus mehreren, auf Block gewickelten Windungen 12, 13, deren Durchmesser kleiner ausgelegt ist als der Durchmesser des Verbindungsstiftes 7. According to Fig. 1, the stops 10, 11 consist of several, on block wound turns 12, 13, the diameter of which is designed to be smaller than the diameter of the connecting pin 7.
In F i g. 2 werden die Anschläge durch eine zwischen einzelnen Windungen 14, 15 und 16, 17 angebrachte, aushärtende und temperaturbeständige Kunststoffmasse 18, 19 gebildet. In Fig. 2 the stops are made by a between individual turns 14, 15 and 16, 17 attached, hardening and temperature-resistant plastic compound 18, 19 formed.
In beiden Fällen ist der Verbindungsstift 7 so lang ausgebildet, daß er sich etwa bis 1200 Drehwinkel der Feder 1 beidseitig der Stoßenden 2, 3 erstreckt, ohne jedoch die Anschläge 10, 11 unmittelbar zu berühren. In both cases, the connecting pin 7 is so long that that it extends to about 1200 angles of rotation of the spring 1 on both sides of the butt ends 2, 3, However, without touching the stops 10, 11 directly.
- Leerseite -- blank page -
Claims (5)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19833336514 DE3336514C1 (en) | 1983-10-07 | 1983-10-07 | Spring, in particular for piston rings |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19833336514 DE3336514C1 (en) | 1983-10-07 | 1983-10-07 | Spring, in particular for piston rings |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3336514C1 true DE3336514C1 (en) | 1984-08-16 |
Family
ID=6211244
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19833336514 Expired DE3336514C1 (en) | 1983-10-07 | 1983-10-07 | Spring, in particular for piston rings |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE3336514C1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102011014603A1 (en) | 2011-03-22 | 2012-09-27 | Federal-Mogul Burscheid Gmbh | Tubular spring for piston ring e.g. oil control ring, of internal combustion engine, has connector whose portion is provided with contour deviating from circumferential curvature that is provided in peripheral region of spring |
US20200232341A1 (en) * | 2019-01-21 | 2020-07-23 | Pratt & Whitney Canada Corp. | Anti-cavitation device for oil dampers |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3695622A (en) * | 1970-12-18 | 1972-10-03 | Sealed Power Corp | Piston ring construction |
DE2429390B1 (en) * | 1974-06-19 | 1975-05-07 | Sigmund Scherdel Kg, 8590 Marktredwitz | Annular coil spring |
US3955823A (en) * | 1974-11-19 | 1976-05-11 | Koppers Company, Inc. | Oil ring assembly |
DE2740125C3 (en) * | 1976-09-08 | 1981-12-10 | Sealed Power Corp., 49443 Muskegon, Mich. | Oil control ring with spreader and guide rod |
-
1983
- 1983-10-07 DE DE19833336514 patent/DE3336514C1/en not_active Expired
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3695622A (en) * | 1970-12-18 | 1972-10-03 | Sealed Power Corp | Piston ring construction |
DE2429390B1 (en) * | 1974-06-19 | 1975-05-07 | Sigmund Scherdel Kg, 8590 Marktredwitz | Annular coil spring |
US3955823A (en) * | 1974-11-19 | 1976-05-11 | Koppers Company, Inc. | Oil ring assembly |
DE2740125C3 (en) * | 1976-09-08 | 1981-12-10 | Sealed Power Corp., 49443 Muskegon, Mich. | Oil control ring with spreader and guide rod |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102011014603A1 (en) | 2011-03-22 | 2012-09-27 | Federal-Mogul Burscheid Gmbh | Tubular spring for piston ring e.g. oil control ring, of internal combustion engine, has connector whose portion is provided with contour deviating from circumferential curvature that is provided in peripheral region of spring |
US20200232341A1 (en) * | 2019-01-21 | 2020-07-23 | Pratt & Whitney Canada Corp. | Anti-cavitation device for oil dampers |
US10767511B2 (en) * | 2019-01-21 | 2020-09-08 | Pratt & Whitney Canada Corp. | Anti-cavitation device for oil dampers |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8100 | Publication of the examined application without publication of unexamined application | ||
D1 | Grant (no unexamined application published) patent law 81 | ||
8364 | No opposition during term of opposition | ||
8320 | Willingness to grant licences declared (paragraph 23) | ||
8339 | Ceased/non-payment of the annual fee |