US4664600A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Rotor aerofoil blade containment
Assignee: Rolls Royce PLC
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Filing: 1985-11-12
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Granted: 1987-05-12
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Expires: 2005-11-12
Abstract
Abstract A hollow prop-fan aerofoil blade is covered by a woven containment sheath which is bonded to the aerofoil surface of the blade and operationally anchored to the blade root. The sheath is arranged to be of sufficient strength to contain any of the aerofoil cross-section portion of the blade in the event of any structural failure thereof.
Inventors
- 👤 Derick A. Perry
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-01 21:56
CPC Classifications
B; B64; B64C; B64C11/00; B64C11/16; B64C11/20; B64C11/26; F; F01; F01D; F01D5/00; F01D5/12; F01D5/28; F01D5/282; F03; F03D; F03D1/00; F03D1/06; F03D1/065; F05; F05B; F05B2240/00; F05B2240/20; F05B2240/30; F05D; F05D2240/00; F05D2240/20; F05D2240/30; Y; Y02; Y02E; Y02E10/00; Y02E10/70; Y02E10/72; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
175 words
A rotor assembly comprising: a rotatable hub member; a plurality of hollow airfoil blades attached to said hub member, each of said hollow blades including an airfoil cross-section portion with an outer surface and having a tip portion at one end and a root portion at an opposite end thereof to said tip portion for attachment to said rotatable hub member; and containment means for each of said hollow blades, each of said containment means including a containment sheath formed from a fibrous material, said containment sheath having a closed end for enclosing said tip portion of said hollow blade, said containment sheath further enclosing and being bonded to said outer surface of said airfoil cross-section portion of said hollow blade and anchored to said root portion, said containment sheath having sufficient strength to contain any part of said airfoil cross-section portion enclosed thereby in the event of any structural failure of said airfoil cross-section portion, and said containment sheath being essentially a non-load bearing and passive member during normal operation of said rotor assembly.
Claim 2
Dependent Claim
175 words
A rotor assembly comprising: a rotatable hub member; a plurality of hollow airfoil blades attached to said hub member, each of said hollow blades including an airfoil cross-section portion with an outer surface and having a tip portion at one end and a root portion at an opposite end thereof to said tip portion for attachment to said rotatable hub member; and containment means for each of said hollow blades, each of said containment means including a containment sheath formed from a fibrous material, said containment sheath having a closed end for enclosing said tip portion of said hollow blade, said containment sheath further enclosing and being bonded to said outer surface of said airfoil cross-section portion of said hollow blade and anchored to said root portion, said containment sheath having sufficient strength to contain any part of said airfoil cross-section portion enclosed thereby in the event of any structural failure of said airfoil cross-section portion, and said containment sheath being essentially a non-load bearing and passive member during normal operation of said rotor assembly.
Claim 3
Dependent Claim
29 words
A hollow rotor assembly as claimed in claim 1 wherein said containment sheath is formed from fibrous material which is woven in the form of an open weave fabric.
Claim 4
Dependent Claim
57 words
A hollow rotor assembly as claimed in claim 1 wherein said containment sheath is operationally anchored to said root portion by arranging for a portion of said sheath to extend to said root portion and clamping said extended sheath portion between said root portion and the rotatable hub member to which said root portion is operationally attached.
Claim 5
Dependent Claim
44 words
A hollow rotor assembly as claimed in claim 1 wherein at least part of said aerofoil cross-section portion adjacent said root portion is constituted by a metal shield, at least a part of which shield is thermally insulated from the remainder of said blade.
Claim 6
Dependent Claim
29 words
A hollow rotor assembly as claimed in claim 4 wherein said at least part of said metal shield is thermally insulated from the remainder of said blade by air.
Claim 7
Dependent Claim
17 words
A hollow rotor assembly as claimed in claim 1 wherein said fibres are formed from an aramid.
Claim 8
Dependent Claim
34 words
A hollow rotor assembly as claimed in claim 1 wherein said containment sheath is bonded to the surface of said at least part of said aerofoil cross-section portion which it encloses by a resin.
Claim 9
Dependent Claim
15 words
A hollow rotor assembly as claimed in claim 7 wherein said resin is an epoxy.
Claim 10
Dependent Claim
16 words
A hollow rotor assembly as claimed in claim 1 wherein said blade is a prop-fan blade.
Claim 11
Dependent Claim
18 words
A hollow rotor assembly as claimed in claim 1 wherein said hollow blade contains a honeycomb support structure.
References Cited (Backward Citations)
US2929755A
Cited
US3330550A
Cited
GB1302857A
Cited
US3664764A
Cited
GB1437236A
Cited
US4037990A
Cited
GB1539634A
Cited
GB2082964A
Cited
US4302155A
Cited
US4407635A
Cited
US4524499A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1990-05-11 | 1990-11-10 | 1991-05-12 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-05-11 | 1994-11-10 | 1995-05-12 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-05-11 | 1998-11-10 | 1999-05-12 | $7700.00 | Window Closed / Lapsed |