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US3881848A Expired / Lapsed US ⏱️ 0.0 years remaining

Packing strip arrangement for highly superheated gases in engines and other working machines

Assignee: Dornier System GmbH
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Filing: 1973-12-21
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Granted: 1975-05-06
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Expires: 1993-12-21
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Abstract

Abstract This invention relates to an improved sealing strip arrangement for sealing highly superheated gases in engines or other working machines having chambers under different pressures wherein the sealing strips are elastically mounted in a groove and bear against a coordinated bearing or rolling surface. The improvement comprises at least one sealing strip means guided in a gas-tight manner against the groove flanks, at least one bore means extending from the chamber of higher pressure to the groove at a point behind the sealing strip means, and valve means for closing-off said bore means.

Inventors

  • 👤 Franz Huf

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-06 08:27
CPC Classifications
F; F01; F01C; F01C19/00; F01C19/02; F01C19/04

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 312 words
In a sealing strip arrangement for a rotary piston engine of trochoidal construction with an inner or outer envelope curve and having a plurality of working chambers, radial grooves in the periphery of that one of the housing and piston of said engine which corresponds to said envelope curve, sealing strip means mounted in said grooves, smaller in radial dimension than said grooves to form a groove space beneath said sealing strip means and having arch-shaped domes on the edge thereof facing the other of said housing and piston, and a pair of bores connecting said groove space with first and second working chambers, respectively, of said engine, the improvement comprising, said domes having their center of curvature positioned on the exact point of intersection of the trochoid and said envelope curve, said sealing strip means having both sides thereof in sufficiently tight contact with the corresponding side walls of said grooves to prevent said sealing strip means from moving transvErsely in said grooves throughout operation of said engine and thereby maintain said center of curvature of said domes on said point of intersection at all times and maintain an essentially gas tight relation between both sides of said sealing strip means and said side walls of said grooves, a pair of second bores radially extending from said grooves and each connecting said groove space with a respective one of the first-mentioned bores, sealing element means mounted in said grooves at the base of said sealing strip means and resting against said side walls of said grooves, sealing cuff means mounted in said groove space and adapted to close off said second bores and spring means mounted in said groove space between said sealing element means and said sealing cuff means to simultaneously act against said sealing cuff means and said sealing element means and thereby urge said sealing strip means outwardly.
Claim 2
Dependent Claim 312 words
In a sealing strip arrangement for a rotary piston engine of trochoidal construction with an inner or outer envelope curve and having a plurality of working chambers, radial grooves in the periphery of that one of the housing and piston of said engine which corresponds to said envelope curve, sealing strip means mounted in said grooves, smaller in radial dimension than said grooves to form a groove space beneath said sealing strip means and having arch-shaped domes on the edge thereof facing the other of said housing and piston, and a pair of bores connecting said groove space with first and second working chambers, respectively, of said engine, the improvement comprising, said domes having their center of curvature positioned on the exact point of intersection of the trochoid and said envelope curve, said sealing strip means having both sides thereof in sufficiently tight contact with the corresponding side walls of said grooves to prevent said sealing strip means from moving transvErsely in said grooves throughout operation of said engine and thereby maintain said center of curvature of said domes on said point of intersection at all times and maintain an essentially gas tight relation between both sides of said sealing strip means and said side walls of said grooves, a pair of second bores radially extending from said grooves and each connecting said groove space with a respective one of the first-mentioned bores, sealing element means mounted in said grooves at the base of said sealing strip means and resting against said side walls of said grooves, sealing cuff means mounted in said groove space and adapted to close off said second bores and spring means mounted in said groove space between said sealing element means and said sealing cuff means to simultaneously act against said sealing cuff means and said sealing element means and thereby urge said sealing strip means outwardly.
Claim 3
Dependent Claim 25 words
A sealing strip arrangement in accordance with claim 1 wherein the first pair of bores are paraxially offset with respect to the engine working chambers.
Claim 4
Dependent Claim 39 words
A sealing strip arrangement in accordance with claim 1 wherein the engine has the sealing strips mounted in separate bodies in which the groove is machined and said bodies are radially mounted in corresponding recesses in the engine housing.
Claim 5
Dependent Claim 21 words
A sealing strip arrangement in accordance with claim 1 wherein the groove and the sealing strip means are in the piston.
Claim 6
Dependent Claim 25 words
A sealing strip arrangement in accordance with claim 1 wherein means are provided whereby the sealing strip means may be laterally inserted in the grooves.
Claim 7
Dependent Claim 41 words
A sealing strip arrangement in accordance with claim 5 wherein the sealing strip means are radially mounted in the housing of the engine and include closable openings and closure means in said housing wall at the point of sealing strip mounting.

References Cited (Backward Citations)

US619801A Cited
US2866417A Cited
US3193186A Cited
US3176909A Cited
US3193189A Cited
US3326454A Cited
US3369739A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1978-05-05 1978-11-04 1979-05-06 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1982-05-05 1982-11-04 1983-05-06 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1986-05-05 1986-11-04 1987-05-06 $7700.00 Window Closed / Lapsed

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