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US3713752A Expired / Lapsed US ⏱️ 0.0 years remaining

Composite blade for a gas turbine engine

Assignee: RTX Corp
•
Filing: 1971-10-28
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Granted: 1973-01-30
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Expires: 1991-10-28
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Abstract

Abstract A composite fluid-directing element comprises a laminated, filament reinforced fluid-directing blade having a cambered airfoil portion and a sinusoid root portion and a foot member bonded to the root portion and configured for retention in the undercut slot of a turbomachine body. The blade is formed of a plurality of parallel laminations of sheets including sheets of high modulus, high strength reinforcing filaments embedded in a matrix material and aligned in a spanwise direction. The foot member has a radially extending oscillatory wave form opening conforming to the shape of the blade root portion in which the root portion is received in bonded relation.

Inventors

  • 👤 A Kurti

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-26 19:33
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/30

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 111 words
A composite fluid-directing element for mounting on a body of a turbomachine having undercut slots comprising a laminated, filament reinforced fluid-directing blade member having a cambered airfoil portion and a sinusoid root portion, said blade member being formed from a plurality of parallel laminations of sheets including sheets of high modulus, high strength reinforcing filaments embedded in a matrix material and aligned in a spanwise direction, said root portion having a radially extending oscillatory wave form and said blade being adapted for mounting on said body with the airfoil portion extending spanwise of the blade from the slot and the slot extending chordwise of the blade at the root portion thereof.
Claim 2
Dependent Claim 111 words
A composite fluid-directing element for mounting on a body of a turbomachine having undercut slots comprising a laminated, filament reinforced fluid-directing blade member having a cambered airfoil portion and a sinusoid root portion, said blade member being formed from a plurality of parallel laminations of sheets including sheets of high modulus, high strength reinforcing filaments embedded in a matrix material and aligned in a spanwise direction, said root portion having a radially extending oscillatory wave form and said blade being adapted for mounting on said body with the airfoil portion extending spanwise of the blade from the slot and the slot extending chordwise of the blade at the root portion thereof.
Claim 3
Dependent Claim 58 words
The invention of claim 1 wherein said element further includes a foot member bonded to said root portion and configured for retention in said undercut slot in the turbomachine body, saId foot member having a radially extending oscillatory wave form opening conforming to the shape of the root portion of said blade member receiving said root portion therein.
Claim 4
Dependent Claim 24 words
The invention of claim 2 wherein said filaments are selected from the group consisting of silicon carbide, carbon, boron and silicon carbide coated boron.
Claim 5
Dependent Claim 26 words
The invention of claim 3 wherein said sinusoid root portion is in the form of a succession of radially extending waves whose bending radii are equal.
Claim 6
Dependent Claim 28 words
The invention of claim 3 wherein said sinusoid root portion is in the form of a succession of radially inwardly extending waves whose bending radii are progressively diminished.

References Cited (Backward Citations)

US2487879A Cited
US3600103A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1976-01-30 1976-07-31 1977-01-30 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1980-01-30 1980-07-31 1981-01-30 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1984-01-30 1984-07-31 1985-01-30 $7700.00 Window Closed / Lapsed

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