CA2973385A1 - Structures auxetiques presentant des fentes de saillie deformees dans des motifs obtenus par ingenierie afin de fournir un comportement npr et des performances ameliorees a la contrainte - Google Patents

Structures auxetiques presentant des fentes de saillie deformees dans des motifs obtenus par ingenierie afin de fournir un comportement npr et des performances ameliorees a la contrainte

Info

Publication number
CA2973385A1
CA2973385A1 CA2973385A CA2973385A CA2973385A1 CA 2973385 A1 CA2973385 A1 CA 2973385A1 CA 2973385 A CA2973385 A CA 2973385A CA 2973385 A CA2973385 A CA 2973385A CA 2973385 A1 CA2973385 A1 CA 2973385A1
Authority
CA
Canada
Prior art keywords
elongated apertures
rigid body
apertures
npr
elastically rigid
Prior art date
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
CA2973385A
Other languages
English (en)
Inventor
Christopher Booth-Morrison
Mehran FARHANGI
Minh Quan Pham
Farhad JAVID
Katia Bertoldi
Michael James Taylor
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.)
Harvard College
Original Assignee
Harvard College
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 Harvard College filed Critical Harvard College
Publication of CA2973385A1 publication Critical patent/CA2973385A1/fr
Abandoned legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002Wall structures
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/186Film cooling
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P2700/00Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
    • B23P2700/13Parts of turbine combustion chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/70Shape
    • F05D2250/71Shape curved
    • F05D2250/713Shape curved inflexed
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/70Shape
    • F05D2250/75Shape given by its similarity to a letter, e.g. T-shaped
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/202Heat transfer, e.g. cooling by film cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/50Intrinsic material properties or characteristics
    • F05D2300/501Elasticity
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/605Crystalline
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00018Manufacturing combustion chamber liners or subparts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03041Effusion cooled combustion chamber walls or domes

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Laminated Bodies (AREA)
  • Fuel Cell (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)

Abstract

L'invention concerne des structures auxétiques, des feuilles auxétiques à refroidissement par effusion, des systèmes et des dispositifs dotés de structures auxétiques, et des procédés d'utilisation et des procédés de fabrication de structures auxétiques. Une structure auxétique comporte un corps élastiquement rigide avec des surfaces supérieure et inférieure opposées. Des première et seconde pluralités d'ouvertures allongées s'étendent à travers le corps élastiquement rigide à partir de la surface supérieure vers la surface inférieure. La première pluralité d'ouvertures allongées s'étend transversalement par rapport à la seconde pluralité d'ouvertures allongées. La première et/ou la seconde pluralité d'ouvertures allongées ont des formes déformées saillantes à travers le corps élastiquement rigide selon un angle oblique. Les ouvertures allongées sont configurées de manière coopérative pour conférer des performances à la contrainte souhaitées tout en présentant un comportement à rapport de Poisson négatif (NPR) dans des conditions de chargement plan macroscopique. À titre d'exemple, la structure auxétique peut présenter une réduction de la concentration de contraintes à proximité des ouvertures allongées et un rapport de Poisson d'environ -0,0001 à -0,9 %.
CA2973385A 2015-01-09 2016-01-09 Structures auxetiques presentant des fentes de saillie deformees dans des motifs obtenus par ingenierie afin de fournir un comportement npr et des performances ameliorees a la contrainte Abandoned CA2973385A1 (fr)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US201562101852P 2015-01-09 2015-01-09
US62/101,852 2015-01-09
US201562118830P 2015-02-20 2015-02-20
US62/118,830 2015-02-20
PCT/US2016/012770 WO2016112369A1 (fr) 2015-01-09 2016-01-09 Structures auxétiques présentant des fentes de saillie déformées dans des motifs obtenus par ingénierie afin de fournir un comportement npr et des performances améliorées à la contrainte

Publications (1)

Publication Number Publication Date
CA2973385A1 true CA2973385A1 (fr) 2016-07-14

Family

ID=56356522

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2973385A Abandoned CA2973385A1 (fr) 2015-01-09 2016-01-09 Structures auxetiques presentant des fentes de saillie deformees dans des motifs obtenus par ingenierie afin de fournir un comportement npr et des performances ameliorees a la contrainte

Country Status (7)

Country Link
US (1) US20170370581A1 (fr)
EP (1) EP3242759A4 (fr)
JP (1) JP2018504557A (fr)
CN (1) CN108290198A (fr)
CA (1) CA2973385A1 (fr)
RU (1) RU2017126609A (fr)
WO (1) WO2016112369A1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102016206022A1 (de) * 2016-04-12 2017-10-12 Siemens Aktiengesellschaft Dichtung für Strömungsmaschinen
CN109344443A (zh) * 2018-09-04 2019-02-15 谢亿民工程科技南京有限公司 一种设计三维负泊松比超材料的方法
US11771183B2 (en) 2021-12-16 2023-10-03 Joon Bu Park Negative Poisson's ratio materials for fasteners
US11988095B2 (en) 2022-03-03 2024-05-21 General Electric Company Seals for managing thermal distortion in a turbomachine and methods for building the same

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6427446B1 (en) * 2000-09-19 2002-08-06 Power Systems Mfg., Llc Low NOx emission combustion liner with circumferentially angled film cooling holes
JP2004257335A (ja) * 2003-02-27 2004-09-16 Kawasaki Heavy Ind Ltd ポーラス金属を用いたガスタービン部品及びその製造方法
US7631502B2 (en) * 2005-12-14 2009-12-15 United Technologies Corporation Local cooling hole pattern
US7546737B2 (en) * 2006-01-24 2009-06-16 Honeywell International Inc. Segmented effusion cooled gas turbine engine combustor
US8652602B1 (en) * 2007-02-28 2014-02-18 William Jacob Spenner Dolla Rotational expansion auxetic structures
US20110059291A1 (en) * 2009-09-07 2011-03-10 Boyce Christopher M Structured materials with tailored isotropic and anisotropic poisson's ratios including negative and zero poisson's ratios
JP5923936B2 (ja) * 2011-11-09 2016-05-25 株式会社Ihi フィルム冷却構造及びタービン翼
US9629397B2 (en) * 2012-08-31 2017-04-25 Under Armour, Inc. Articles of apparel including auxetic materials
US9709274B2 (en) * 2013-03-15 2017-07-18 Rolls-Royce Plc Auxetic structure with stress-relief features
US9353783B2 (en) * 2013-03-15 2016-05-31 Rolls-Royce Canada, Ltd. Auxetic locking pin
EP2969740B1 (fr) * 2013-03-15 2020-05-06 President and Fellows of Harvard College Structures vides à motif répétitif d'ouvertures allongées
WO2014151045A1 (fr) * 2013-03-15 2014-09-25 President And Fellows Of Harvard College Feuille auxétique à faible porosité
JP2018508738A (ja) * 2015-01-09 2018-03-29 プレジデント アンド フェローズ オブ ハーバード カレッジ 特注のnpr挙動および向上された冷却性能のための特別設計されたパターンに位置する傾斜したスロットを有するオーゼティック構造体

Also Published As

Publication number Publication date
EP3242759A1 (fr) 2017-11-15
JP2018504557A (ja) 2018-02-15
RU2017126609A (ru) 2019-02-12
CN108290198A (zh) 2018-07-17
RU2017126609A3 (fr) 2019-07-17
EP3242759A4 (fr) 2018-09-26
US20170370581A1 (en) 2017-12-28
WO2016112369A1 (fr) 2016-07-14

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Legal Events

Date Code Title Description
FZDE Discontinued

Effective date: 20210831

FZDE Discontinued

Effective date: 20210831