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US4877272A Expired / Lapsed US ⏱️ 0.0 years remaining

Metal static seal and assembly comprising such a seal

Assignee: Safran Aircraft Engines SAS
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Filing: 1987-03-31
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Granted: 1989-10-31
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Expires: 2007-03-31
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Abstract

Abstract The static seal comprises a semi-rigid annular part (11) shaped as a bead and first and second wings (12, 13) extending transversely with respect to the seal axis and laterally connected to the bead portion (11) in a gradual manner by means of concave surfaces with a large curvature radius. The seal has in its axial cross-section the shape of a V lying on its side, the tapered surfaces (16, 17) of the branches (12, 13) of the V being slightly inclined with respect to the planar surfaces (18, 19) of the bead (11) to which they are attached. The branches (12, 13) of the V forming the wings have an elasticity such that by flexure of said tapered surfaces (16, 17) of the V branches and slight flexure of the bead (11), the extremities of said surface may form with the planar surfaces (18, 19) of the bead (11) to which they are attached two sealing regions. Said seal is intended to be used in severe conditions of temperature, pressure, vibrations and chemical attack.

Inventors

  • 👤 Marc Chevallier
  • 👤 Guy Froger

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-28 21:38
CPC Classifications
F; F16; F16L; F16L41/00; F16L41/08; F16L41/10; F16J; F16J15/00; F16J15/02; F16J15/06; F16J15/08; F16J15/0887; Y; Y10; Y10S; Y10S285/00; Y10S285/917

Claims Analysis

Total Claims: 11
Claim 1
Independent Claim 226 words
A generally round static seal made of a material selected from the group consisting of metal and metal alloys, presenting a unitary load with the limit of remanent elongation Re at least equal to about 60 h bar, coated with a thin layer of coating for the assembly of the seal without the interposition of a washer, having a longitudinal axis, and comprising an annular-part-forming slightly flexible semi-rigid bead and first and second wings connected laterally to the bead and extending transversely therefrom with respect to the axis of the seal, the seal presenting in axial half-section the form of a V lying on its side, the bead having two oppositely disposed planar lateral surfaces perpendicular to the axis of the seal, each wing having an outer tapered surface slightly inclined to its respective planar lateral surface of the bead and connected thereto in a gradual and regular manner to form a concave surface with a large radius of curvature, the wings and bead having an elasticity such that when the wings are flexed said bead flexes displacing said planar lateral surfaces, said wings outer tapered surfaces provide with the displaced planar lateral surfaces of the bead two sealing regions, the flexural capabilities of the wings being determined exclusively by the characteristics of the seal and remaining independent from outer connecting pieces cooperating with the seal.
Claim 2
Dependent Claim 226 words
A generally round static seal made of a material selected from the group consisting of metal and metal alloys, presenting a unitary load with the limit of remanent elongation Re at least equal to about 60 h bar, coated with a thin layer of coating for the assembly of the seal without the interposition of a washer, having a longitudinal axis, and comprising an annular-part-forming slightly flexible semi-rigid bead and first and second wings connected laterally to the bead and extending transversely therefrom with respect to the axis of the seal, the seal presenting in axial half-section the form of a V lying on its side, the bead having two oppositely disposed planar lateral surfaces perpendicular to the axis of the seal, each wing having an outer tapered surface slightly inclined to its respective planar lateral surface of the bead and connected thereto in a gradual and regular manner to form a concave surface with a large radius of curvature, the wings and bead having an elasticity such that when the wings are flexed said bead flexes displacing said planar lateral surfaces, said wings outer tapered surfaces provide with the displaced planar lateral surfaces of the bead two sealing regions, the flexural capabilities of the wings being determined exclusively by the characteristics of the seal and remaining independent from outer connecting pieces cooperating with the seal.
Claim 3
Dependent Claim 32 words
The static seal of claim 1 in which the inclination of each outer tapered surface to its respective planar lateral surface to which it is attached is from 7 to 15 degrees.
Claim 4
Dependent Claim 30 words
The static seal of claim 1 in which the inclination of each outer tapered surface to its respective planar lateral surface to which it is attached is approximately 10 degrees.
Claim 5
Dependent Claim 38 words
The static seal of claim 1 having an outer diameter at most equal to about 14 millimeters in which the bead constitutes an inner annular part and the tapered wings point away from the axis of the seal.
Claim 6
Dependent Claim 37 words
The static seal of claim 1 having an outer diameter at least equal to about 14 millimeters in which the bead constitutes an outer annular part and the tapered wings point towards the axis of the seal.
Claim 7
Dependent Claim 16 words
The static seal of claim 1 in which it is made of a strongly alloyed steel.
Claim 8
Dependent Claim 14 words
The static seal of claim 6 in which the alloy is Z6 NCT 25-15.
Claim 9
Dependent Claim 18 words
The static seal of claim 6 in which the alloy comprises 50% nickel, 10% chromium, and 19% iron.
Claim 10
Dependent Claim 74 words
An assembly by screwed connection comprising an implantation piece provided with an inner thread, and a connecting piece composed of a connecting head and a threaded rod cooperating with the inner thread, in which the connecting head has a planar lower surface, the implantation piece has a countersink opposite the planar lower surface of the connecting head, and the static seal of claim 9 is interposed between the planar lower surface and the countersink.
Claim 11
Dependent Claim 63 words
An assembly by screwed connection in accordance with claim 9 having cylindrical surface defining therebetween an annular housing for receiving an O-ring made of elastomer, the cylindrical surfaces being formed on the connecting piece and the implantation piece respectively in a region located between the connecting head and the threaded rod and in a region located between the countersink and the inner thread.

References Cited (Backward Citations)

FR595332A Cited
US2852281A Cited
US3058750A Cited
US3142498A Cited
FR1356218A Cited
US3376053A Cited
FR1537146A Cited
FR1563153A Cited
US3759552A Cited
US4597596A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1992-10-30 1993-05-01 1993-10-31 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1996-10-30 1997-05-01 1997-10-31 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2000-10-30 2001-05-01 2001-10-31 $7700.00 Window Closed / Lapsed

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