US4343593A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Composite blade for turbofan engine fan
Assignee: United States Department of the Air Force
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Filing: 1980-01-25
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Granted: 1982-08-10
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Expires: 2000-01-25
Abstract
Abstract A turbofan engine fan blade made of composite material, and a method of making the fan, are taught. The fan blade essentially comprises an airfoil section having a root end and made of a plurality of bonded plies of composite material which are splayed and which are in a staggered condition at the root end; a two-piece platform section made of titanium or of aluminum, with one piece of the platform on each side of the airfoil section; and a steel outsert section which holds and secures the platform section to the airfoil section, with the outsert section having a triangular shaped cavity located at the root end of the airfoil section, between the splayed and staggered plies of the airfoil section. Among other advantages, the cavity eliminates the "insert plies" (or wedge) used in the prior art and the inherent disadvantages associated with such use.
Inventors
- 👤 David J. Harris
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 13:58
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/12; F01D5/28; F01D5/282; F01D5/30; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
186 words
A turbofan engine fan blade, comprising: a. an airfoil section having a tip end, a root end, and a first and a second surface therebetween, wherein said first surface is essentially convex and said second surface is essentially concave, and wherein said airfoil section comprises a plurality of bonded plies of composite material which are splayed and are in a staggered condition at said root end; b. a platform section which includes: (1) a first member complementary to, and disposed in abutting contact with, said convex first surface of said airfoil section at said root end thereof; and (2) a second member complementary to, and disposed in abutting contact with, said concave second surface of said airfoil section at said root end thereof; and c. a metal outsert section holding and securing said platform section of said airfoil section at said root end thereof, and means within said outsert section for defining a cavity therein, with said cavity located at said root end of said airfoil section and simultaneously also positioned between said splayed and staggered plies of said plurality of plies of said airfoil section.
Claim 2
Dependent Claim
186 words
A turbofan engine fan blade, comprising: a. an airfoil section having a tip end, a root end, and a first and a second surface therebetween, wherein said first surface is essentially convex and said second surface is essentially concave, and wherein said airfoil section comprises a plurality of bonded plies of composite material which are splayed and are in a staggered condition at said root end; b. a platform section which includes: (1) a first member complementary to, and disposed in abutting contact with, said convex first surface of said airfoil section at said root end thereof; and (2) a second member complementary to, and disposed in abutting contact with, said concave second surface of said airfoil section at said root end thereof; and c. a metal outsert section holding and securing said platform section of said airfoil section at said root end thereof, and means within said outsert section for defining a cavity therein, with said cavity located at said root end of said airfoil section and simultaneously also positioned between said splayed and staggered plies of said plurality of plies of said airfoil section.
Claim 3
Dependent Claim
34 words
A turbofan engine fan blade, as set forth in claim 1, wherein said plurality of plies of said airfoil section are made of composite material which includes reinforcing filaments embedded in a matrix material.
Claim 4
Dependent Claim
28 words
A turbofan engine fan blade, as set forth in claim 2, wherein said reinforcing filaments are made of graphite, and wherein said matrix material is an epoxy resin.
Claim 5
Dependent Claim
19 words
A turbofan engine fan blade, as set forth in claim 3, wherein said platform section is made of metal.
Claim 6
Dependent Claim
31 words
A turbofan engine fan blade, as set forth in claim 4, wherein said metal of which said platform section is made is selected from the group consisting of aluminum and titanium.
Claim 7
Dependent Claim
33 words
A turbofan engine fan blade, as set forth in claim 5, wherein said cavity in said outsert section has a cross sectioned shape that is essentially in the form of an upright triangle.
Claim 8
Dependent Claim
20 words
A turbofan engine fan blade, as set forth in claim 6, wherein said metal outsert section is made of steel.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1985-08-09 | 1986-02-08 | 1986-08-10 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-08-09 | 1990-02-08 | 1990-08-10 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-08-09 | 1994-02-08 | 1994-08-10 | $7700.00 | Window Closed / Lapsed |