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US4010530A Expired / Lapsed US ⏱️ 0.0 years remaining

Method for making blade protective sheaths

Assignee: RTX Corp
•
Filing: 1975-07-24
•
Granted: 1977-03-08
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Expires: 1995-07-24
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Abstract

Abstract A method for producing a generally bifurcated metal protective sheath for the edge of an aerodynamic blade comprising the steps of (1) providing a metal sheath mid-section element having a top and bottom surface, (2) covering the top and bottom surface with an aluminum bonding material, (3) laying up separate metal top and bottom sheath cover elements on each of the top and bottom surfaces of the mid-section element to cover and overhang the same, the aluminum bonding material having a solidus temperature lower than the solidus temperatures of the mid-section element and the top and bottom cover elements, and (4) subjecting the layup to heat and pressure in a die for a time sufficient to bring the temperature of the bonding material to a temperature which is below but within approximately 20° F of its solidus temperature to solid state diffusion bond the mid-section and cover elements together without forming intermetallics.

Inventors

  • 👤 Eugene Joseph Delgrosso
  • 👤 Carl Edwin Carlson
  • 👤 James Augustus Jennings

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-30 06:14
CPC Classifications
B; B23; B23P; B23P15/00; B23P15/04; B23K; B23K20/00; B23K35/00; B23K35/22; B23K35/24; B23K35/28; B23K35/286; F; F01; F01D; F01D5/00; F01D5/12; F01D5/28; F04; F04D; F04D29/00; F04D29/26; F04D29/32; F04D29/321; F04D29/324; F05; F05D; F05D2240/00; F05D2240/20; F05D2240/30; F05D2240/303; Y; Y02; Y02T; Y02T50/00; Y02T50/60; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/49316; Y10T29/49336; Y10T29/49337; Y10T29/49826; Y10T29/49861

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 259 words
A method for protecting the edge of an aerodynamic blade comprising: providing a metal sheath mid-section element having a top and a bottom surface, said mid-section element being selected from the group consisting of titanium, nickel and alloys thereof; covering said top and bottom surface with an aluminum bonding material; laying up a metal top and bottom sheath cover element on each of said top and bottom surfaces of said mid-section element, said top and bottom cover elements being selected from the group consisting of titanium, nickel and alloys thereof and having contact surfaces wider than said top and bottom surfaces of said sheath mid-section element to overhang opposite sides of the same and thereby form channels adapted to receive the edge of said blade; said aluminum bonding material having a solidus temperature which is lower than the solidus temperature of each of said mid-section element and said top and bottom cover elements; subjecting the layup to heat and pressure in a die for a time sufficient to bring the temperature of said bonding material to a temperature which is below but within approximately 20° F of its solidus temperature to solid state diffusion bond said mid-section and cover elements together without forming intermetallics, said temperature being 900°-1075° F, said pressure being 1,000-10,000 psi and said time being 2-90 minutes; severing the bonded product through said top surface, said mid-section element and said bottom surface to form two U-shaped protective sheaths; finishing said U-shaped protective sheath to final shape; and bonding said U-shaped protective sheath to said blade edge.
Claim 2
Independent Claim 259 words
A method for protecting the edge of an aerodynamic blade comprising: providing a metal sheath mid-section element having a top and a bottom surface, said mid-section element being selected from the group consisting of titanium, nickel and alloys thereof; covering said top and bottom surface with an aluminum bonding material; laying up a metal top and bottom sheath cover element on each of said top and bottom surfaces of said mid-section element, said top and bottom cover elements being selected from the group consisting of titanium, nickel and alloys thereof and having contact surfaces wider than said top and bottom surfaces of said sheath mid-section element to overhang opposite sides of the same and thereby form channels adapted to receive the edge of said blade; said aluminum bonding material having a solidus temperature which is lower than the solidus temperature of each of said mid-section element and said top and bottom cover elements; subjecting the layup to heat and pressure in a die for a time sufficient to bring the temperature of said bonding material to a temperature which is below but within approximately 20° F of its solidus temperature to solid state diffusion bond said mid-section and cover elements together without forming intermetallics, said temperature being 900°-1075° F, said pressure being 1,000-10,000 psi and said time being 2-90 minutes; severing the bonded product through said top surface, said mid-section element and said bottom surface to form two U-shaped protective sheaths; finishing said U-shaped protective sheath to final shape; and bonding said U-shaped protective sheath to said blade edge.
Claim 3
Dependent Claim 35 words
The method of claim 1 including the step of inserting a spacer in said channel adjacent said mid-section element to support overhanging portions of said top and bottom cover elements during solid state diffusion bonding.
Claim 4
Dependent Claim 16 words
The method of claim 2 including the step of coating said spacer with a stop-off compound.
Claim 5
Dependent Claim 22 words
The method of claim 1 wherein said temperature is 990°-1,050° F, said pressure is 5,000-6,000 psi and said time is 10-40 minutes.
Claim 6
Dependent Claim 11 words
The method of claim 4 wherein said time is 12-35 minutes.
Claim 7
Dependent Claim 14 words
The method of claim 1 wherein said aluminum bonding alloy is 1-20 mils thick.

References Cited (Backward Citations)

US2615236A Cited
US2884077A Cited
US3002567A Cited
US2851770A Cited
US3478416A Cited
US3670397A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1980-03-07 1980-09-06 1981-03-08 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1984-03-07 1984-09-06 1985-03-08 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1988-03-07 1988-09-06 1989-03-08 $7700.00 Window Closed / Lapsed

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