SG11201506186PA - Repair of surface damage at edges of cellular panels - Google Patents

Repair of surface damage at edges of cellular panels

Info

Publication number
SG11201506186PA
SG11201506186PA SG11201506186PA SG11201506186PA SG11201506186PA SG 11201506186P A SG11201506186P A SG 11201506186PA SG 11201506186P A SG11201506186P A SG 11201506186PA SG 11201506186P A SG11201506186P A SG 11201506186PA SG 11201506186P A SG11201506186P A SG 11201506186PA
Authority
SG
Singapore
Prior art keywords
repair
edges
surface damage
cellular panels
panels
Prior art date
Application number
SG11201506186PA
Inventor
Brian Kenneth Holland
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 SG11201506186PA publication Critical patent/SG11201506186PA/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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30—Exhaust heads, chambers, or the like
    • 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
    • B29C73/00—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
    • B29C73/04—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements
    • B29C73/14—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements using elements composed of two parts joined together after having been placed one on each side of the article
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/40—Maintaining or repairing aircraft
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/46—Nozzles having means for adding air to the jet or for augmenting the mixing region between the jet and the ambient air, e.g. for silencing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/827—Sound absorbing structures or liners
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/80—Repairing, retrofitting or upgrading methods
    • 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
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/14—Casings or housings protecting or supporting assemblies within
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Connection Of Plates (AREA)
SG11201506186PA 2013-03-01 2014-02-27 Repair of surface damage at edges of cellular panels SG11201506186PA (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201361771419P 2013-03-01 2013-03-01
US201361832389P 2013-06-07 2013-06-07
PCT/US2014/018897 WO2014134262A1 (en) 2013-03-01 2014-02-27 Repair of surface damage at edges of cellular panels

Publications (1)

Publication Number Publication Date
SG11201506186PA true SG11201506186PA (en) 2015-09-29

Family

ID=51428791

Family Applications (1)

Application Number Title Priority Date Filing Date
SG11201506186PA SG11201506186PA (en) 2013-03-01 2014-02-27 Repair of surface damage at edges of cellular panels

Country Status (4)

Country Link
US (1) US10060295B2 (en)
EP (1) EP2961967B1 (en)
SG (1) SG11201506186PA (en)
WO (1) WO2014134262A1 (en)

Family Cites Families (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4820564A (en) * 1984-10-29 1989-04-11 The Boeing Company Blind-side repair patch kit
US4759812A (en) 1985-07-11 1988-07-26 Miller Robert W Method and apparatus for effecting field repairs in stress carrying structures
US5239823A (en) * 1991-02-26 1993-08-31 United Technologies Corporation Multiple layer cooled nozzle liner
US5682678A (en) 1995-11-13 1997-11-04 The Nordam Group, Inc. Mechanical repair for a honeycomb panel
US5927647A (en) * 1997-09-24 1999-07-27 Rohr, Inc. Blocker door frame pressure structure for translating cowl of cascade thrust reverser for aircraft jet engine
US6656299B1 (en) * 2001-12-19 2003-12-02 Lockheed Martin Corporation Method and apparatus for structural repair
US6718752B2 (en) * 2002-05-29 2004-04-13 The Boeing Company Deployable segmented exhaust nozzle for a jet engine
US7546684B2 (en) 2004-07-27 2009-06-16 General Electric Company Method for repair and replacement of combustor liner panel
US20060059828A1 (en) 2004-07-29 2006-03-23 Stevenson James F Repair method for noise suppression structure
EP3305465B1 (en) * 2005-12-14 2021-11-24 Hontek Corporation Method and coating for protecting and repairing an airfoil surface
US7740028B1 (en) * 2006-01-24 2010-06-22 The University Of Tulsa Composite plug system and process for high pressure pipeline leaks
EP2015889B1 (en) 2006-05-11 2014-07-09 Bell Helicopter Textron Inc. Device and method for repairing structural components
US7572347B2 (en) 2006-05-26 2009-08-11 United Technologies Corporation Repair of composite sandwich structures with uneven bond surfaces
US7935205B2 (en) 2006-06-19 2011-05-03 United Technologies Corporation Repair of composite sandwich structures
US7722318B2 (en) 2007-02-13 2010-05-25 United Technologies Corporation Hole liners for repair of vane counterbore holes
US7837437B2 (en) 2007-03-07 2010-11-23 General Electric Company Turbine nozzle segment and repair method
US20080233346A1 (en) 2007-03-23 2008-09-25 United Technologies Corporation Repair of a composite sandwich structure having a perforated skin
US20090165926A1 (en) * 2007-10-24 2009-07-02 United Technologies Corporation Method and assembly for bonding metal layers in a gas turbine engine using a polyimide adhesive
US8043690B2 (en) * 2008-04-21 2011-10-25 The Boeing Company Exhaust washed structure and associated composite structure and method of fabrication
DE102008021788A1 (en) 2008-04-30 2009-11-12 Deutsches Zentrum für Luft- und Raumfahrt e.V. Method for repairing an aircraft component
US8015820B2 (en) * 2008-06-03 2011-09-13 United Technologies Corporation Gas turbine engine exhaust component and manufacturing method of same
FR2933224B1 (en) 2008-06-25 2010-10-29 Aircelle Sa ACCOUSTIC PANEL FOR EJECTION TUBE
US8617694B1 (en) * 2009-03-09 2013-12-31 The Boeing Company Discretely tailored multi-zone bondline for fail-safe structural repair
US8434293B2 (en) * 2009-08-06 2013-05-07 The Boeing Company High stiffness shape memory alloy actuated aerostructure
DE102010051842A1 (en) * 2010-11-18 2012-05-24 Rolls-Royce Deutschland Ltd & Co Kg Repair method of a sandwich-type component
FR2970238B1 (en) * 2011-01-07 2013-01-25 Airbus Operations Sas PIECE AND METHOD FOR REPAIRING A DAMAGED STRUCTURE, ESPECIALLY AIRCRAFT SKIN, AND A REPAIR KIT FOR IMPLEMENTING THE SAME
FR2970433B1 (en) 2011-01-13 2013-01-04 Aircelle Sa PROCESS FOR REPAIRING AT LEAST ONE PART OF AN ACOUSTIC PANEL FOR A NACELLE
FR2971613B1 (en) * 2011-02-10 2013-03-15 Airbus Operations Sas PANEL FOR ACOUSTIC PROCESSING COMPRISING JOINT BETWEEN TWO PARTS AND METHOD OF REPAIRING A PANEL FOR ACOUSTIC TREATMENT
US9539798B2 (en) * 2014-02-17 2017-01-10 The Boeing Company Verifiable quick patch repair for composite structures

Also Published As

Publication number Publication date
EP2961967A4 (en) 2016-11-23
EP2961967B1 (en) 2021-03-31
EP2961967A1 (en) 2016-01-06
US20150377072A1 (en) 2015-12-31
US10060295B2 (en) 2018-08-28
WO2014134262A1 (en) 2014-09-04

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