CA2602319A1 - Blade containment system for a gas turbine engine - Google Patents

Blade containment system for a gas turbine engine Download PDF

Info

Publication number: CA2602319A1
Authority: CA; Canada
Prior art keywords: layer; containment system; blade containment; metal laminate; fiber metal
Prior art date: 2006-09-25
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.): Abandoned

Application number

CA002602319A

Other languages

English (en)

French (fr)

Inventor

David Lawrence Bedel

David William Crall

Stephen Craig Mitchell

Donald George Lachapelle

Ming Xie

Frank Worthoff

Leslie Louis Langenbrunner

Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)

General Electric Co

Original Assignee

General Electric Co

Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)

2006-09-25

Filing date

2007-09-13

Publication date

2008-03-25

2007-09-13 Application filed by General Electric Co filed Critical General Electric Co

2008-03-25 Publication of CA2602319A1 publication Critical patent/CA2602319A1/en

Status Abandoned legal-status Critical Current

Links

229910052751 metal Inorganic materials 0.000 claims abstract description 48
239000002184 metal Substances 0.000 claims abstract description 48
239000000835 fiber Substances 0.000 claims abstract description 40
229920000271 Kevlar® Polymers 0.000 claims abstract description 8
239000004761 kevlar Substances 0.000 claims abstract description 8
239000000463 material Substances 0.000 description 11
229910052782 aluminium Inorganic materials 0.000 description 6
XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 6
238000002485 combustion reaction Methods 0.000 description 4
238000011144 upstream manufacturing Methods 0.000 description 4
RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 3
239000003822 epoxy resin Substances 0.000 description 3
239000012634 fragment Substances 0.000 description 3
239000000446 fuel Substances 0.000 description 3
239000011521 glass Substances 0.000 description 3
229920000647 polyepoxide Polymers 0.000 description 3
239000010936 titanium Substances 0.000 description 3
229910052719 titanium Inorganic materials 0.000 description 3
OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
229910000831 Steel Inorganic materials 0.000 description 2
239000004760 aramid Substances 0.000 description 2
229920003235 aromatic polyamide Polymers 0.000 description 2
239000002131 composite material Substances 0.000 description 2
238000000034 method Methods 0.000 description 2
238000012986 modification Methods 0.000 description 2
230000004048 modification Effects 0.000 description 2
230000001141 propulsive effect Effects 0.000 description 2
239000010959 steel Substances 0.000 description 2
239000004593 Epoxy Substances 0.000 description 1
239000000853 adhesive Substances 0.000 description 1
230000001070 adhesive effect Effects 0.000 description 1
229910052799 carbon Inorganic materials 0.000 description 1
239000003733 fiber-reinforced composite Substances 0.000 description 1
RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 description 1
230000004313 glare Effects 0.000 description 1
229910002804 graphite Inorganic materials 0.000 description 1
239000010439 graphite Substances 0.000 description 1
210000001503 joint Anatomy 0.000 description 1
239000011159 matrix material Substances 0.000 description 1
229910001092 metal group alloy Inorganic materials 0.000 description 1
150000002739 metals Chemical class 0.000 description 1
239000000203 mixture Substances 0.000 description 1
230000002787 reinforcement Effects 0.000 description 1
238000005096 rolling process Methods 0.000 description 1
239000004576 sand Substances 0.000 description 1
238000000926 separation method Methods 0.000 description 1
239000007787 solid Substances 0.000 description 1
229920002994 synthetic fiber Polymers 0.000 description 1

Classifications

- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B1/00—Layered products having a non-planar shape
- B32B1/08—Tubular products
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
- F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/08—Sealings
- F04D29/16—Sealings between pressure and suction sides
- F04D29/161—Sealings between pressure and suction sides especially adapted for elastic fluid pumps
- F04D29/164—Sealings between pressure and suction sides especially adapted for elastic fluid pumps of an axial flow wheel
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/522—Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
- F04D29/526—Details of the casing section radially opposing blade tips
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

Engineering & Computer Science (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Structures Of Non-Positive Displacement Pumps (AREA)
Laminated Bodies (AREA)
Control Of Turbines (AREA)

CA002602319A 2006-09-25 2007-09-13 Blade containment system for a gas turbine engine Abandoned CA2602319A1 (en)

Applications Claiming Priority (2)

Application Number	Priority Date	Filing Date	Title
US52640106A	2006-09-25	2006-09-25
US11/526,401		2006-09-25

Publications (1)

Publication Number	Publication Date
CA2602319A1 true CA2602319A1 (en)	2008-03-25

Family

ID=38659004

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
CA002602319A Abandoned CA2602319A1 (en)	2006-09-25	2007-09-13	Blade containment system for a gas turbine engine

Country Status (4)

Country	Link
JP (1)	JP2008082332A (de)
CA (1)	CA2602319A1 (de)
DE (1)	DE102007045138A1 (de)
GB (1)	GB2442112A (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
CN108691582A (zh) *	2017-03-31	2018-10-23	波音公司	燃气涡轮发动机风扇叶片包容***
FR3097902A1 (fr) *	2019-06-27	2021-01-01	Safran Aircraft Engines	Turbomachine d’aeronef a enveloppe en materiau au moins partiellement composite

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
FR2935017B1 (fr) *	2008-08-13	2012-11-02	Snecma	Paroi interne d'une nacelle de turbomachine
EP2418387B1 (de)	2010-08-11	2015-04-01	Techspace Aero S.A.	Gehäusering eines Kompressors eines axialen Turbotriebwerks
GB2489673B (en) *	2011-03-29	2015-08-12	Rolls Royce Plc	A containment casing for a gas turbine engine
FR2977827B1 (fr) *	2011-07-13	2015-03-13	Snecma	Procede de fabrication d'un carter de soufflante de turbomachine muni de revetements abradable et acoustique
EP2594742B1 (de) *	2011-11-17	2017-01-04	Hamilton Sundstrand Corporation	Kostengünstige Berstschutzring
US9840936B2 (en)	2012-02-16	2017-12-12	United Technologies Corporation	Case with ballistic liner
SG11201404100TA (en)	2012-02-16	2014-10-30	United Technologies Corp	Composite fan containment case assembly
FR2991385B1 (fr)	2012-06-05	2017-04-28	Snecma	Contre-plaque, et turbomachine comprenant une contre-plaque
GB201401932D0 (en)	2014-02-05	2014-03-19	Rolls Royce Plc	A fan casing for a gas turbine engine
FR3031469B1 (fr) *	2015-01-14	2017-09-22	Snecma	Carter en materiau composite a matrice organique auto-raidi
AT516322B1 (de) *	2014-10-10	2017-04-15	Facc Ag	Fangehäuse für ein Flugzeugtriebwerk
US10472985B2 (en) *	2016-12-12	2019-11-12	Honeywell International Inc.	Engine case for fan blade out retention
US10662813B2 (en) *	2017-04-13	2020-05-26	General Electric Company	Turbine engine and containment assembly for use in a turbine engine
US10533450B2 (en)	2017-10-30	2020-01-14	United Technologies Corporation	Ballistic liner install methods
EP3702263A1 (de)	2019-02-28	2020-09-02	Airbus Operations GmbH	Flugzeugstruktur zur strömungsregelung

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US4534698A (en) *	1983-04-25	1985-08-13	General Electric Company	Blade containment structure
GB2159886B (en) *	1984-06-07	1988-01-27	Rolls Royce	Fan duct casing
GB2239214B (en) *	1989-12-23	1993-11-03	Rolls Royce Plc	A sandwich structure and a method of manufacturing a sandwich structure
US5344280A (en) *	1993-05-05	1994-09-06	General Electric Company	Impact resistant fan case liner
US6652222B1 (en) *	2002-09-03	2003-11-25	Pratt & Whitney Canada Corp.	Fan case design with metal foam between Kevlar
NL1024076C2 (nl) *	2003-08-08	2005-02-10	Stork Fokker Aesp Bv	Werkwijze voor het vormen van een laminaat met een uitsparing.
US20050175813A1 (en) *	2004-02-10	2005-08-11	Wingert A. L.	Aluminum-fiber laminate
TWI401160B (zh) *	2004-09-24	2013-07-11	Itochu Corp	複合材料、及包含該材料之產品和纖維-金屬複合材料
US20060093847A1 (en) *	2004-11-02	2006-05-04	United Technologies Corporation	Composite sandwich with improved ballistic toughness

2007
- 2007-09-13 CA CA002602319A patent/CA2602319A1/en not_active Abandoned
- 2007-09-14 GB GB0718002A patent/GB2442112A/en not_active Withdrawn
- 2007-09-20 DE DE102007045138A patent/DE102007045138A1/de not_active Withdrawn
- 2007-09-21 JP JP2007245123A patent/JP2008082332A/ja active Pending

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
CN108691582A (zh) *	2017-03-31	2018-10-23	波音公司	燃气涡轮发动机风扇叶片包容***
FR3097902A1 (fr) *	2019-06-27	2021-01-01	Safran Aircraft Engines	Turbomachine d’aeronef a enveloppe en materiau au moins partiellement composite

Also Published As

Publication number	Publication date
GB0718002D0 (en)	2007-10-24
GB2442112A (en)	2008-03-26
JP2008082332A (ja)	2008-04-10
DE102007045138A1 (de)	2008-03-27

Legal Events

Date	Code	Title	Description
2012-09-13	FZDE	Discontinued

Publication	Publication Date	Title
CA2602319A1 (en)	2008-03-25	Blade containment system for a gas turbine engine
CN107044445B (zh)	2021-04-06	易碎的燃气涡轮发动机翼型件
US8061966B2 (en)	2011-11-22	Composite containment casings
US8046915B2 (en)	2011-11-01	Methods for making composite containment casings
EP2932052B1 (de)	2019-07-24	Bläsergehäuse mit thermisch konformer auskleidung
US6382905B1 (en)	2002-05-07	Fan casing liner support
EP2952696B1 (de)	2021-05-26	Turbofantriebwerksanordnung mit fangehäuse-auskleidungseinsatz
EP2815084B1 (de)	2020-07-29	Gasturbinengehäuse mit ballistischer auskleidung
EP3779131A1 (de)	2021-02-17	Anordnung eines strömungspfadsbauteils und zugehöriger turbinenabschnitt für ein gasturbinentriebwerk
US8371009B2 (en)	2013-02-12	Methods for repairing composite containment casings
US8827629B2 (en)	2014-09-09	Case with ballistic liner
EP3447306B1 (de)	2020-07-22	Containmentgehäuse für den fan eines zweistromturbostrahltriebwerks
US10731662B2 (en)	2020-08-04	Apparatus and method of manufacturing a containment case with embedded containment core
US20160273550A1 (en)	2016-09-22	Layered ice liner
EP3719264A1 (de)	2020-10-07	Schaufelaussenluftdichtung aus cmc mit querhakenanordnung
EP3712382A2 (de)	2020-09-23	Verschleissauskleidung für eine äussere schaufelluftdichtung
US10907651B2 (en)	2021-02-02	Fan track liner subassembly angled upturn joint
EP3913190A1 (de)	2021-11-24	Schaufelbefestigung für gasturbinenmotoren

CA2602319A1 - Blade containment system for a gas turbine engine - Google Patents

Info

Links

Classifications

Landscapes

Applications Claiming Priority (2)

Publications (1)

Family

ID=38659004

Family Applications (1)

Country Status (4)

Cited By (2)

Families Citing this family (15)

Family Cites Families (9)

Cited By (2)

Also Published As

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Legal Events