SG11201404102PA - Case with ballistic liner - Google Patents

Case with ballistic liner

Info

Publication number
SG11201404102PA
SG11201404102PA SG11201404102PA SG11201404102PA SG11201404102PA SG 11201404102P A SG11201404102P A SG 11201404102PA SG 11201404102P A SG11201404102P A SG 11201404102PA SG 11201404102P A SG11201404102P A SG 11201404102PA SG 11201404102P A SG11201404102P A SG 11201404102PA
Authority
SG
Singapore
Prior art keywords
case
ballistic liner
ballistic
liner
Prior art date
Application number
SG11201404102PA
Inventor
Darin S Lussier
Sreenivasa R Voleti
Jr Thomas J Robertson
Christopher M Quinn
Original Assignee
United Technologies Corp
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.)
Filing date
Publication date
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of SG11201404102PA publication Critical patent/SG11201404102PA/en

Links

Classifications

    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
    • B29C70/226—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure the structure comprising mainly parallel filaments interconnected by a small number of cross threads
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
    • B29C70/228—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure the structure being stacked in parallel layers with fibres of adjacent layers crossing at substantial angles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/32—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core on a rotating mould, former or core
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/006—Producing casings, e.g. accumulator cases
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/20—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres
    • B29C70/202—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres arranged in parallel planes or structures of fibres crossing at substantial angles, e.g. cross-moulding compound [XMC]
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/748—Machines or parts thereof not otherwise provided for
    • B29L2031/7504—Turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/601—Fabrics
    • F05D2300/6012—Woven fabrics
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
SG11201404102PA 2012-02-16 2013-02-14 Case with ballistic liner SG11201404102PA (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/397,772 US9840936B2 (en) 2012-02-16 2012-02-16 Case with ballistic liner
PCT/US2013/026148 WO2013123195A1 (en) 2012-02-16 2013-02-14 Case with ballistic liner

Publications (1)

Publication Number Publication Date
SG11201404102PA true SG11201404102PA (en) 2014-10-30

Family

ID=48982386

Family Applications (1)

Application Number Title Priority Date Filing Date
SG11201404102PA SG11201404102PA (en) 2012-02-16 2013-02-14 Case with ballistic liner

Country Status (4)

Country Link
US (2) US9840936B2 (en)
EP (1) EP2815084B1 (en)
SG (1) SG11201404102PA (en)
WO (1) WO2013123195A1 (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140003923A1 (en) 2012-07-02 2014-01-02 Peter Finnigan Functionally graded composite fan containment case
FR2995038B1 (en) * 2012-08-30 2014-09-19 Snecma GAS TURBINE BLOWER HOUSING HAVING EQUIPMENT FASTENING BELT
US20150345320A1 (en) * 2013-03-13 2015-12-03 United Technologies Corporation Fan case with auxetic liner
WO2015094421A1 (en) * 2013-12-19 2015-06-25 United Technologies Corporation Gas turbine engine having energy dissipating gap and containment layer
EP2940251B1 (en) 2014-04-28 2019-06-12 Rolls-Royce Corporation Fan containment case
US9915168B2 (en) 2014-06-03 2018-03-13 United Technologies Corporation Flowpath cartridge liner and gas turbine engine including same
US9714583B2 (en) * 2014-08-21 2017-07-25 Honeywell International Inc. Fan containment cases for fan casings in gas turbine engines, fan blade containment systems, and methods for producing the same
AT515539B1 (en) * 2014-09-04 2015-10-15 Facc Ag Jacket for an aircraft engine and method for producing such a jacket
US10458433B2 (en) * 2015-06-17 2019-10-29 United Technologies Corporation Co-molded metallic fan case containment ring
US10731662B2 (en) 2016-01-12 2020-08-04 Rolls-Royce Corporation Apparatus and method of manufacturing a containment case with embedded containment core
US20170234160A1 (en) * 2016-02-11 2017-08-17 General Electric Company Aircraft engine with an impact panel
US20180347585A1 (en) * 2017-06-01 2018-12-06 Rolls-Royce Corporation Fan track liner assembly
US20190085856A1 (en) * 2017-09-18 2019-03-21 United Technologies Corporation Laminated hybrid composite-metallic containment system for gas turbine engines
US10533450B2 (en) 2017-10-30 2020-01-14 United Technologies Corporation Ballistic liner install methods
US11040512B2 (en) * 2017-11-08 2021-06-22 Northrop Grumman Systems Corporation Composite structures, forming apparatuses and related systems and methods
US11156126B2 (en) 2018-04-13 2021-10-26 Raytheon Technologies Corporation Fan case with interleaved layers
GB201811549D0 (en) 2018-07-13 2018-08-29 Rolls Royce Plc Fan blade containment
FR3100561B1 (en) * 2019-09-10 2023-01-20 Safran Aircraft Engines ATTACHING AN ACOUSTIC SHELL TO A CRANKCASE SHELL FOR AN AIRCRAFT TURBOMACHINE
US11319833B2 (en) * 2020-04-24 2022-05-03 General Electric Company Fan case with crack-arresting backsheet structure and removable containment cartridge
US11549391B2 (en) * 2021-03-22 2023-01-10 General Electric Company Component formed from hybrid material

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FR2497726A1 (en) 1981-01-12 1982-07-16 Brochier Fils J MULTILAYER TEXTILE ARTICLE FOR REINFORCING LAMINATED MATERIALS AND PROCESS FOR OBTAINING THE SAME
US4748064A (en) 1985-01-14 1988-05-31 Allied Corporation Ballistic-resistant composite article
CA2042198A1 (en) 1990-06-18 1991-12-19 Stephen C. Mitchell Projectile shield
US5516257A (en) * 1994-04-28 1996-05-14 United Technologies Corporation Aircraft fan containment structure restraint
US5809805A (en) 1996-09-03 1998-09-22 Mcdonnell Douglas Corporation Warp/knit reinforced structural fabric
US5724670A (en) 1996-10-03 1998-03-10 Safariland Ltd., Inc. Multi-component ballistic vest
US6637186B1 (en) * 1997-11-11 2003-10-28 United Technologies Corporation Fan case liner
US6053696A (en) 1998-05-29 2000-04-25 Pratt & Whitney Canada Inc. Impact resistant composite shell for gas turbine engine fan case
US6814541B2 (en) * 2002-10-07 2004-11-09 General Electric Company Jet aircraft fan case containment design
US20040219855A1 (en) 2003-05-02 2004-11-04 Tsotsis Thomas K. Highly porous interlayers to toughen liquid-molded fabric-based composites
EP1621323A1 (en) 2004-07-27 2006-02-01 Hexcel Composites GmbH Continuous pultrusion process for producing high performance structural profiles
US20060093847A1 (en) 2004-11-02 2006-05-04 United Technologies Corporation Composite sandwich with improved ballistic toughness
US7246990B2 (en) 2004-12-23 2007-07-24 General Electric Company Composite fan containment case for turbine engines
US7435693B2 (en) 2005-01-07 2008-10-14 The Boeing Company Toughened, non-crimped unidirectional fabric apparatus and method of making same
GB0510538D0 (en) * 2005-05-24 2005-06-29 Rolls Royce Plc A rotor blade containment assembly for a gas turbine engine
CA2602319A1 (en) 2006-09-25 2008-03-25 General Electric Company Blade containment system for a gas turbine engine
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US9017814B2 (en) 2007-10-16 2015-04-28 General Electric Company Substantially cylindrical composite articles and fan casings
US8403624B2 (en) * 2007-12-12 2013-03-26 General Electric Company Composite containment casings having an integral fragment catcher
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JP5551411B2 (en) 2009-11-06 2014-07-16 株式会社Ｉｈｉ Case manufacturing method and case

Also Published As

Publication number Publication date
US20180100408A1 (en) 2018-04-12
EP2815084A1 (en) 2014-12-24
US20130216367A1 (en) 2013-08-22
US9840936B2 (en) 2017-12-12
WO2013123195A1 (en) 2013-08-22
EP2815084B1 (en) 2020-07-29
US10724397B2 (en) 2020-07-28
EP2815084A4 (en) 2015-12-16

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