Patent US5336044A successfully refreshed from Google Patents.
US5336044A
Expired / Lapsed
US
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Blade containment system and method
Assignee: General Electric Co
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Filing: 1993-08-06
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Granted: 1994-08-09
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Expires: 2013-08-06
Abstract
Abstract A blade containment system and method for use in a gas turbine engine having a plurality of blades mounted on a rotatable disk. The system comprises an annular casing in surrounding relationship with the blades and a plurality of panels, each having an interior noise absorbing structure and an outer containment structure, disposed about an interior surface of the casing so as to position the panels outward and forward of the blades. The panels are supported so as to fix the panels with respect to the casing during normal engine operation and to allow an impacted one of the panels to slide circumferentially when acted upon by a predetermined blade force caused by a released portion of one of the blades impacting the panel. Ramps formed in each end of the containment structure of each panel allow the impacted panel to slidingly engage at least a circumferentially adjacent one of the panels when acted upon by the predetermined blade force.
Inventors
- 👤 James M. Forrester
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-06 17:56
CPC Classifications
F; F01; F01D; F01D21/00; F01D21/04; F01D21/045; F05; F05D; F05D2220/00; F05D2220/30; F05D2220/32; F05D2220/327; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 12
Claim 1
Independent Claim
186 words
In a gas turbine engine having a plurality of radially extending blades mounted on an annular disk, the blades and disk being rotatable about a longitudinal axis of the engine, a blade containment system comprising: a) an annular casing positioned radially outward of the blades and in surrounding relationship with the blades; b) a plurality of circumferentially segmented panels disposed about an interior surface of said casing, said panels being radially outward of the blades; c) means for supporting said panels so as to fix each of said panels with respect to said forward portion of said casing during normal operation of the engine and so as to allow an impacted one of said panels to slide circumferentially when said impacted panel is acted upon by a predetermined blade force caused by a released portion of one of the blades impacting said impacted panel; d) ramp means for allowing said impacted panel to slidingly engage at least a circumferentially adjacent one of said panels when said impacted panel is impacted by the released blade portion so as to dissipate kinetic energy of the released blade portion.
Claim 2
Dependent Claim
186 words
In a gas turbine engine having a plurality of radially extending blades mounted on an annular disk, the blades and disk being rotatable about a longitudinal axis of the engine, a blade containment system comprising: a) an annular casing positioned radially outward of the blades and in surrounding relationship with the blades; b) a plurality of circumferentially segmented panels disposed about an interior surface of said casing, said panels being radially outward of the blades; c) means for supporting said panels so as to fix each of said panels with respect to said forward portion of said casing during normal operation of the engine and so as to allow an impacted one of said panels to slide circumferentially when said impacted panel is acted upon by a predetermined blade force caused by a released portion of one of the blades impacting said impacted panel; d) ramp means for allowing said impacted panel to slidingly engage at least a circumferentially adjacent one of said panels when said impacted panel is impacted by the released blade portion so as to dissipate kinetic energy of the released blade portion.
Claim 3
Dependent Claim
146 words
The blade containment system as recited in claim 1, wherein: a) said plurality of circumferentially segmented panels are disposed about a forward portion of said interior surface of said casing so as to position said panels axially forward of the blades; b) said ramp means comprises a radially outward facing ramp formed in a circumferentially facing end of each of said panels and a radially inward facing ramp formed in an opposite circumferentially facing end of each of said panels, said panels being disposed so as to position said radially outward facing ramp of each of said panels circumferentially adjacent to said radially inward facing ramp of an adjacent one of said panels; c) said ramp means causes said impacted panel to be forced radially inward of said circumferentially adjacent one of said panels when said impacted panel is acted upon by the predetermined blade force.
Claim 4
Dependent Claim
62 words
The blade containment system as recited in claim 2, wherein: a) each of said panels comprises a radially outer containment structure and a radially inner noise absorbing structure, said inner noise absorbing structure being bolted to said outer containment structure; said outer containment structure terminating on said radially outward facing ramp and said radially inward facing ramp of each of said panels.
Claim 5
Dependent Claim
43 words
The blade containment system as recited in claim 3, wherein said noise absorbing structure of each of said panels is sub-divided into a radially inner portion and a radially outer portion, said inner portion and said outer portion being separated by a septum.
Claim 6
Dependent Claim
20 words
The blade containment system as recited in claim 2, wherein said means for supporting comprises a plurality of shear bolts.
Claim 7
Dependent Claim
69 words
The blade containment system as recited in claim 5, wherein said means for supporting further comprises: a) a plurality of bushings bonded to each of said panels, each of said bushings including a hole for accepting one of said shear bolts; b) a plurality of nut plates fixedly attached to an exterior surface of said casing, each of said nut plates securing a corresponding one of said shear bolts.
Claim 8
Dependent Claim
66 words
The blade containment system as recited in claim 4, wherein said means for supporting comprises: a) a plurality of bushings bonded to each of said panels, each of said bushings including a hole for accepting a shear bolt; b) a plurality of nut plates fixedly attached to an exterior surface of said casing, each of said nut plates securing a corresponding one of said shear bolts.
Claim 9
Independent Claim
178 words
A method of containing rotating blades of a gas turbine engine, said method comprising the steps of: a) surrounding the rotating blades with an annular casing positioned radially outward of the blades; b) disposing a plurality of circumferentially segmented panels about a forward portion of an interior surface of said annular casing such that said panels are positioned radially outward and axially forward of the rotating blades; c) supporting said panels so as to fix each of said panels with respect to said casing during normal operation of the engine and so as to allow an impacted one of said panels to slide circumferentially when said impacted panel is acted upon by a predetermined blade force caused by a released portion of one of the blades impacting said impacted panel; d) providing ramp means on each of said panels to allow said impacted panel to slidingly engage at least a circumferentially adjacent one of said panels when said impacted panel is impacted by the released blade portion so as to dissipate kinetic energy of the released blade portion.
Claim 10
Independent Claim
178 words
A method of containing rotating blades of a gas turbine engine, said method comprising the steps of: a) surrounding the rotating blades with an annular casing positioned radially outward of the blades; b) disposing a plurality of circumferentially segmented panels about a forward portion of an interior surface of said annular casing such that said panels are positioned radially outward and axially forward of the rotating blades; c) supporting said panels so as to fix each of said panels with respect to said casing during normal operation of the engine and so as to allow an impacted one of said panels to slide circumferentially when said impacted panel is acted upon by a predetermined blade force caused by a released portion of one of the blades impacting said impacted panel; d) providing ramp means on each of said panels to allow said impacted panel to slidingly engage at least a circumferentially adjacent one of said panels when said impacted panel is impacted by the released blade portion so as to dissipate kinetic energy of the released blade portion.
Claim 11
Dependent Claim
121 words
The method as recited in claim 8, wherein: a) said step of supporting comprises the step of attaching each of said circumferentially segmented panels to a forward portion of said casing with a plurality of shear bolts; b) said step of providing comprises the steps of: i) forming a radially outward facing ramp in a circumferentially facing end of each of said panels; ii) forming a radially inward facing ramp in an opposite circumferentially facing end of each of said panels; c) said step of disposing comprises the step of positioning said panels such that said radially outward facing ramp of each of said panels is circumferentially adjacent to said radially inward facing ramp of an adjacent one of said panels.
Claim 12
Dependent Claim
122 words
The method as recited in claim 8, wherein said method further comprises the steps of: a) structuring each of said panels to include a radially outer containment structure and a radially inner noise absorbing structure; b) bonding said noise absorbing structure of each of said panels to said containment structure of a corresponding one of said panels; and c) wherein said step of providing further comprises the steps of: i) extending said radially outward facing ramp and said radially inward facing ramp through said outer containment structure of each of said panels; ii) causing said impacted panel to be forced radially inward of said circumferentially adjacent one of said panels when said impacted panel is acted upon by the predetermined blade force.
References Cited (Backward Citations)
US2987296A
Cited
US3241813A
Cited
US4149824A
Cited
US4377370A
Cited
US4534698A
Cited
US5160248A
Cited
US5188505A
Cited
US5273393A
Cited
US5267828A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1997-08-08 | 1998-02-07 | 1998-08-09 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2001-08-08 | 2002-02-07 | 2002-08-09 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2005-08-08 | 2006-02-07 | 2006-08-09 | $7700.00 | Window Closed / Lapsed |