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US4069576A Expired / Lapsed US ⏱️ 0.0 years remaining

Wound wire reinforcing bands and method

Assignee: Safran Aircraft Engines SAS
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Filing: 1975-10-07
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Granted: 1978-01-24
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Expires: 1995-10-07
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Abstract

Abstract A method and apparatus for fabricating reinforcing bands for strengtheningarts to be subjected to high centrifugal stresses. The reinforcing bands are made of coiled wire with a high modulus of elasticity and with a matrix of light metal or light-metal alloy. The coil, hoop or blank so formed is compacted in a direction parallel to its axis under high pressure and heat by an annular metal ram in a mold or die consisting of a bottom member, an inner ring, and an outer ring which are constructed so that the blank or coil does not undergo any radial stresses.

Inventors

  • 👤 Pierre Teysseyre
  • 👤 Joel Vigneau

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-25 11:54
CPC Classifications
C; C22; C22C; C22C47/00; C22C47/02; C22C47/06; C22C47/062; C22C47/064; B; B29; B29C; B29C53/00; B29C53/56; B29C53/564; B29C53/566; B65; B65H; B65H81/00; C22C47/16; C22C47/18; B22; B22F; B22F2998/00; Y; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/4998; Y10T29/49982; Y10T428/00; Y10T428/12; Y10T428/12465; Y10T428/12486

Claims Analysis

Total Claims: 10
Claim 1
Independent Claim 194 words
A process for fabricating a ring shaped member to be used in high speed rotating machinery which is subject to high centrifical stresses, the process comprising the steps of: a. winding wire helically on a mandrel to form a single cylindrical layer of wire, each wind being spaced between 0.3 and 2.0 d from the next adjacent wind, d being the diameter of the wire; b. depositing matrix material on the layer of wound wire after said winding step; c. repeating said winding and depositing steps n-1 times, where n is the number of layers of wire in the finished product, each repeated winding step providing a single layer of wire over the same axial length as the first layer of wire; said repeated winding and depositing steps forming an annular blank; d. applying heat and pressure to said blank, said pressure being applied parallel to the axis of rotation of the annular blank and being applied so that no radial stresses occur in the blank, said heat and pressure being selected so that the matrix creeps into and fills the interstices between the wires while the integrity of the wound wire is maintained.
Claim 2
Dependent Claim 194 words
A process for fabricating a ring shaped member to be used in high speed rotating machinery which is subject to high centrifical stresses, the process comprising the steps of: a. winding wire helically on a mandrel to form a single cylindrical layer of wire, each wind being spaced between 0.3 and 2.0 d from the next adjacent wind, d being the diameter of the wire; b. depositing matrix material on the layer of wound wire after said winding step; c. repeating said winding and depositing steps n-1 times, where n is the number of layers of wire in the finished product, each repeated winding step providing a single layer of wire over the same axial length as the first layer of wire; said repeated winding and depositing steps forming an annular blank; d. applying heat and pressure to said blank, said pressure being applied parallel to the axis of rotation of the annular blank and being applied so that no radial stresses occur in the blank, said heat and pressure being selected so that the matrix creeps into and fills the interstices between the wires while the integrity of the wound wire is maintained.
Claim 3
Dependent Claim 25 words
A process as defined in claim 1 wherein the inner diameter of the annular blank is substantially determined by the outer diameter of the mandrel.
Claim 4
Dependent Claim 36 words
A process as defined in claim 1 wherein the volume of matrix material deposited during said depositing step is approximately three times the volume of the layer of wire wound during the immediately preceding winding step.
Claim 5
Dependent Claim 57 words
A process as defined in claim 1 wherein said blank, prior to said step of applying heat and pressure, is placed in an annular space defined by a mold, and wherein said pressure applying step is carried out by an annular ram which cooperates with the annular space of the mold to apply pressure throughout the blank.
Claim 6
Dependent Claim 49 words
A process as defined in claim 4, wherein said mold includes an inner ring and an outer ring, the coefficient of expansion of the inner ring being greater than that of the blank and the coefficient of expansion of the outer ring being less than that of the blank.
Claim 7
Dependent Claim 28 words
A process as defined in claim 1, wherein the matrix material is deposited by a plasma torch and wherein the matrix surface is suitably finished after each deposit.
Claim 8
Dependent Claim 50 words
A process as defined in claim 1 wherein said wire is composed of tungsten coated with a material selected from a group consisting of boron carbide, silicon carbide, boron nitride, or combinations thereof, and wherein the diameter of the wire is in the range of 0.075 mm - 0.200 mm.
Claim 9
Dependent Claim 204 words
A ring-shaped reinforcing band for use in high speed rotating machinery which is subject to high centrifugal stresses, the band being produced by: a. winding wire helically on a mandrel to form a single cylindrical layer of wire, each wind being spaced apart between 0.3 and 2.0 d from the next adjacent wind, d being the diameter of the wire; b. depositing matrix material on the layer of wound wire after said depositing step; c. repeating said winding and depositing steps n-1 times, where n is the number of layers of wire in the finished product, each repeated winding step providing a single layer of wire over the same axial length as the first layer of wire; said repeated winding and depositing steps forming an annular blank; d. applying heat and pressure to said blank, said pressure being applied parallel to the axis of rotation of the annular blank, said heat and pressure being selected so that the matrix creeps into and fills the interstices between the wires while the integrity of the wound wire is maintained; e. whereby a reinforcing ring is produced wherein the reinforcing wires have been substantially free of any radial stresses at all times during production of the band.
Claim 10
Dependent Claim 204 words
A ring-shaped reinforcing band for use in high speed rotating machinery which is subject to high centrifugal stresses, the band being produced by: a. winding wire helically on a mandrel to form a single cylindrical layer of wire, each wind being spaced apart between 0.3 and 2.0 d from the next adjacent wind, d being the diameter of the wire; b. depositing matrix material on the layer of wound wire after said depositing step; c. repeating said winding and depositing steps n-1 times, where n is the number of layers of wire in the finished product, each repeated winding step providing a single layer of wire over the same axial length as the first layer of wire; said repeated winding and depositing steps forming an annular blank; d. applying heat and pressure to said blank, said pressure being applied parallel to the axis of rotation of the annular blank, said heat and pressure being selected so that the matrix creeps into and fills the interstices between the wires while the integrity of the wound wire is maintained; e. whereby a reinforcing ring is produced wherein the reinforcing wires have been substantially free of any radial stresses at all times during production of the band.

References Cited (Backward Citations)

US2166109A Cited
US2544455A Cited
US3006064A Cited
US3006065A Cited
US3007231A Cited
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USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1981-01-23 1981-07-25 1982-01-24 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1985-01-23 1985-07-25 1986-01-24 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1989-01-23 1989-07-25 1990-01-24 $7700.00 Window Closed / Lapsed

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