US3785745A - Sealing bar for a rotary piston internal combustion engine - Google Patents

Sealing bar for a rotary piston internal combustion engine Download PDF

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Publication number
US3785745A
US3785745A US00109474A US3785745DA US3785745A US 3785745 A US3785745 A US 3785745A US 00109474 A US00109474 A US 00109474A US 3785745D A US3785745D A US 3785745DA US 3785745 A US3785745 A US 3785745A
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United States
Prior art keywords
sealing bar
width
wear
bar according
height
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Expired - Lifetime
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US00109474A
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English (en)
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H Lamm
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Daimler Benz AG
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Daimler Benz AG
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C19/00—Sealing arrangements in rotary-piston machines or engines
    • F01C19/10—Sealings for working fluids between radially and axially movable parts

Definitions

  • Vrablik [21] Appl' 109474 Attorney-Craig, Antonelli, Stewart & Hill [30] Foreign Application Priority Data [57] ABSTRACT Janv 24, 1970 Germany P 20 03 203.5 A Sealing bar for a rotary piston internal o u n [52] U S Cl 418/117 418/113 engine, particularly of trochoidal construction, which [51] 6 27/00 is arranged within a piston groove so as to be movable [58] Fie'ld 418/1 13 1 i 1 19424 in a radial direction, and which sealingly slides with its 7 1 277/81 head portion along a contact surface in the housing case of the internal combustion engine; the sealing bar is provided with a multi-partite, preferably two-partite, [56] References cued wear head portion subdivided substantially parallel to UNITED STATES PATENTS the longitudinal axis and having small-connecting sur- 3,l94,489 7/1965 Frenzel 4l8/l 17 faces with respect to the
  • FIG 2 FIG. 3
  • the present invention relates to a sealing bar for a rotary piston internal combustion engine, particularly of trochoidal type of construction, which is arranged within a piston groove movable in a radial direction and which with its dome or head portion sealingly slides along an engaging or running surface in the housing case of the internal combustion engine.
  • the sealing bar is provided with a multi-partite, preferably two-partite, wear head portion subdivided parallel to its longitudinal axis and having small connecting surfaces with respect to the support portion. The stresses leading to disturbances during operation are reduced in this manner.
  • the connecting surfaces may be arranged preferably only horizontally.
  • an elastic connecting layer of conventional material may be provided at the connecting surfaces.
  • the elastic connection may be formed, for example, by an elastic soldering (brazing) or adhesive connection as used for the installation of gas turbine blades.
  • the elastic connecting material may consist, for example,-of an elastic alloy to be meltedin customary in connections for metal to ceramic or glass or of an elastic metal adhesive, as long as these materials can be used within a temperature range of about 400 centigrade to 1,000 centigrade.
  • a very narrow gap may exist between the parts of the wear head portion made of customary wear material. This small gap assures freedom from stress of the parts with respect to one another.
  • Another object of the present invention resides in a sealing bar for a rotary piston internal combustion engine of trochoidal construction which at least greatly minimizes the stresses occurring on the inside thereof during manufacture and operation as a result of differences in the expansion conditions and moduli of elasticity.
  • a further object of the present invention resides in a sealing bar of the type described above which not only minimizes the operational stresses, but almost completely eliminates any residual stresses by extremely simple means.
  • FIGS. 1 to 3 illustrate cross-sectional views through three embodiments of a sealing bar in accordance with the present invention.
  • FIG. 4 illustrates a cross-sectional view of a portion of a rotary piston internal combustion engine of trochoidal construction.
  • a sealing bar generally designated by reference numeral 1 is illustrated in this figure which consists of a support portion 2 made of conventional support material and of a wear head portion 3 made of conventional wear material.
  • the sealing bar 1 is provided at its bottom side 4 with aslot 5 whose width corresponds to approximately one-fourth of the width of the sealing and whose height corresponds to approximately three-fourths of the height of the sealing bar 1.
  • the wear head portion 3 is subdivided along its longitudinal axis and is so se cured on the support portion 2 by means of an elastic connecting layer 6 of any conventional material,
  • the sealing bar generally designated by reference numeral 1 and illustrated in FIG. 2 consists of a support portion 2 and of a subdivided wear head portion 3 which is constructed exactly as the wear head portion 3 illustrated in FIG. I.
  • a slot 9 is arranged facing the wear portion 3 whose width corresponds to approximately a third of the width of the sealingbar l and whose height corresponds to approximately half the height of the sealing bar I.
  • a sealing bar generally designated by reference numeral 1 is illustrated in FIG. 3 in which an aperture 11 approximately V-shaped in cross-section is provided which starts from a lower edge 10 of the support portion 2; one side 12 of the V-shaped aperture 11 extends parallel to a flank 13 of the sealing bar 1 disposed opposite the edge 10 and the other side 14 of the V- shaped aperture 11 extends approximately in the diagonal direction of the cross-section of the sealing bar I.
  • the height of the aperture 11 corresponds to approximately three-fourths of the width of the sealing bar I.
  • Two parts of the wear head portion 3 with a thickness corresponding to about one-fifth of the width of the sealing bar 1 are arranged at the top side 15 of the support portion 2 with a web portion 16 of the support portion 2 having about the same thickness arranged therebetween.
  • the twoparts of the wear portion 3 are weardeterrninative for the entire top side 15. They are connected at its bottom side thereof by the elastic connecting layer 6 with the support part 2.
  • the sealing bar I is disposed in a slot 31 provided in a piston generally designated by the reference numeral 30 so as to enable the wear head portion 3 to engage the piston grooves 21 provided in the housing casing of the rotary piston internal combustion engine generally designated by the reference numeral 20.
  • a sealing bar for a rotary piston internal combustion engine which includes a housing casing and a piston provided with piston grooves, said sealing bar being movably arranged in a radial direction within a piston groove and sliding sealingly with a head portion thereof along engaging surface means provided in the housing case of the internal combustion engine, characterized in that the sealing bar is provided with a multi-partite wear head portion subdivided over its entire length in the longitudinal direction thereof, the wear head portion is supported on a support portion disposed therebelow by way of connecting surfaces of relatively small dimensions relative to the width of the sealing bar, and in that means are provided for avoiding stresses in the sealing bar which are caused by different thermal expansions of the utilized materials including an elastic layer means provided on the connecting surfaces for connecting the wear head portion to the support portion and a slot means provided in the support portion with at least a portion of the slot means extending substantially parallel to the longitudinal axis of the supportportion.
  • a sealing bar according to claim 1 characterized in that all parts of the multi-partite wear portion are made of wear material.
  • a sealing bar according to claim 1 characterized in that said connecting surfaces extend at substantially right angle to the vertical longitudinal center plane of the sealing bar.
  • a sealing bar according to claim 1 characterized in that said connecting surfaces extend only in plane at least approximately at right angle to the outer longitudinal surfaces of the bar.
  • a sealing bar according to claim 1 characterized in that the connecting surfaces are provided only substantially horizontally relative to the longitudinal direction.
  • a sealing bar according to claim 1 characterized in that the connecting surfaces extend over a distance smaller than the width of a sealing bar.
  • a sealing bar according to claim 1 characterized in that the individual parts of the multi-partite wear head portion are separate from one another by a small gap extending in said longitudinal direction over the entire length of the sealing bar.
  • a sealing bar according to claim 8 characterized in that said connecting surfaces are angularly disposed to the plane of separation of the individual parts of the multi-partite wear head portion, said plane of separation also containing said gap.
  • a sealing bar according to claim 9 characterized in that all parts of the multi-partite wear portion are made of wear material.
  • a sealing bar according to claim 10 characterized in that the connecting surfaces extend over a distance smaller than the width of a sealing bar.
  • a sealing bar according to claim 11 characterized in that said connecting surfaces are spaced from one another by a gap in the direction of the width of the sealing bar.
  • a sealing bar according to claim 13 characterized in that the slot means extends from the bottom side of the sealing bar substantially in the center of the sealing bar cross section, the width of said slot corresponding to about one-fourth to one-third of the width of the sealing bar and the height thereof corresponding to about one-half to three-quarters of the height of the sealing bar.
  • a sealing bar according to claim 13 characterized in that a narrow gap exists between the parts of the wear portion.
  • a sealing bar according to claim 1 characterized in that the slot means is arranged in the part of the support portion facing the wear portion, the width of said slot corresponding to about one-third of the width of the sealing bar and the height thereof corresponding to about one-half of the height of the sealing bar.
  • a sealing bar according to claim 13 characterized in that a narrow gap exists between the parts of the wear portion.
  • a sealing bar according to claim 1 characterized in that the slot aperture means includes an approximately V-shaped in cross section starting from a lower edge of the sealing bar, one side of said aperture being substantially parallel to a flank disposed opposite to one of the edges of the sealing bar and the other side extending approximately in the diagonal direction of the cross section of the sealing bar, the height of said aperture corresponding approximately to half the height of the sealing bar and the width thereof at the bottom side corresponding to about three-fourths of the width of the sealing bar.
  • a sealing bar according to claim 1 characterized in that the wear portion is subdivided substantially parallel to its longitudinal axis.
  • a sealing bar according to claim 19 characterized in that the connecting surfaces are provided only substantially horizontally relative to the longitudinal direction.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Sealing Devices (AREA)
US00109474A 1970-01-24 1971-01-25 Sealing bar for a rotary piston internal combustion engine Expired - Lifetime US3785745A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19702003203 DE2003203A1 (de) 1970-01-24 1970-01-24 Dichtleiste fuer eine Rotationskolben-Brennkraftmaschine

Publications (1)

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US3785745A true US3785745A (en) 1974-01-15

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US00109474A Expired - Lifetime US3785745A (en) 1970-01-24 1971-01-25 Sealing bar for a rotary piston internal combustion engine

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US (1) US3785745A (enExample)
DE (1) DE2003203A1 (enExample)
FR (1) FR2076896A5 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5039288A (en) * 1988-06-08 1991-08-13 Bando Kiko Co., Limited Rotary engine having an apex seal member

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1083041A (fr) * 1953-09-04 1955-01-04 Appareil rotatif, tel que compresseur, <<soufflante>>, pompe ou autre, provoquant outravaillant par le déplacement d'un fluide
US3120815A (en) * 1961-08-02 1964-02-11 Nsu Motorenwerke Ag Seal for rotary mechanisms
US3180564A (en) * 1962-07-02 1965-04-27 Goetzewerke Radial seal for rotary piston engines
US3194489A (en) * 1963-03-20 1965-07-13 Goetzewerke Radial piston for rotary engines
US3215340A (en) * 1962-03-20 1965-11-02 Daimler Benz Ag Rotary-piston engine construction
US3263912A (en) * 1963-07-23 1966-08-02 Goetzewerke Radial seal
US3270954A (en) * 1964-02-17 1966-09-06 Toyo Kogyo Company Ltd Sealing device for rotary piston engine
US3286912A (en) * 1965-03-11 1966-11-22 Yannar Diesel Engine Co Ltd Gas-tight sealing device for rotary piston engines
US3300124A (en) * 1966-04-14 1967-01-24 Curtiss Wright Corp Seal construction for rotry mechanisms

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1083041A (fr) * 1953-09-04 1955-01-04 Appareil rotatif, tel que compresseur, <<soufflante>>, pompe ou autre, provoquant outravaillant par le déplacement d'un fluide
US3120815A (en) * 1961-08-02 1964-02-11 Nsu Motorenwerke Ag Seal for rotary mechanisms
US3215340A (en) * 1962-03-20 1965-11-02 Daimler Benz Ag Rotary-piston engine construction
US3180564A (en) * 1962-07-02 1965-04-27 Goetzewerke Radial seal for rotary piston engines
US3194489A (en) * 1963-03-20 1965-07-13 Goetzewerke Radial piston for rotary engines
US3263912A (en) * 1963-07-23 1966-08-02 Goetzewerke Radial seal
US3270954A (en) * 1964-02-17 1966-09-06 Toyo Kogyo Company Ltd Sealing device for rotary piston engine
US3286912A (en) * 1965-03-11 1966-11-22 Yannar Diesel Engine Co Ltd Gas-tight sealing device for rotary piston engines
US3300124A (en) * 1966-04-14 1967-01-24 Curtiss Wright Corp Seal construction for rotry mechanisms

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5039288A (en) * 1988-06-08 1991-08-13 Bando Kiko Co., Limited Rotary engine having an apex seal member

Also Published As

Publication number Publication date
DE2003203A1 (de) 1971-07-29
FR2076896A5 (enExample) 1971-10-15

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