US20080041842A1 - Connector for heater - Google Patents

Connector for heater Download PDF

Info

Publication number
US20080041842A1
US20080041842A1 US11/221,195 US22119505A US2008041842A1 US 20080041842 A1 US20080041842 A1 US 20080041842A1 US 22119505 A US22119505 A US 22119505A US 2008041842 A1 US2008041842 A1 US 2008041842A1
Authority
US
United States
Prior art keywords
connector
heater
terminals
strut
electrical
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
US11/221,195
Inventor
Phillip Emerson Alexander
David R. Lyders
John Vontell
George Alan Salisbury
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.)
RTX Corp
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
Assigned to UNITED TECHNOLOGIES CORPORATION reassignment UNITED TECHNOLOGIES CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: ALEXANDER, PHILLIP EMERSON, LYDERS, DAVID R., SALISBURY, GEORGE ALAN, VONTELL, JOHN
Priority to US11/221,195 priority Critical patent/US20080041842A1/en
Application filed by United Technologies Corp filed Critical United Technologies Corp
Priority to CA002553300A priority patent/CA2553300A1/en
Priority to IL177029A priority patent/IL177029A0/en
Priority to JP2006200710A priority patent/JP2007071199A/en
Priority to AU2006203145A priority patent/AU2006203145A1/en
Priority to CNA2006101513490A priority patent/CN1933243A/en
Priority to BRPI0602901-9A priority patent/BRPI0602901A/en
Priority to EP06253970A priority patent/EP1762714B1/en
Priority to SG200605273-2A priority patent/SG131009A1/en
Priority to KR1020060074025A priority patent/KR20070028219A/en
Publication of US20080041842A1 publication Critical patent/US20080041842A1/en
Priority to US12/605,652 priority patent/US8247746B2/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047Heating to prevent icing
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R13/00Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
    • H01R13/02Contact members
    • H01R13/04Pins or blades for co-operation with sockets
    • 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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/02De-icing means for engines having icing phenomena
    • 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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162Bearing supports
    • 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
    • F01D9/00Stators
    • F01D9/06Fluid supply conduits to nozzles or the like
    • F01D9/065Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R13/00Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
    • H01R13/02Contact members
    • H01R13/22Contacts for co-operating by abutting
    • H01R13/24Contacts for co-operating by abutting resilient; resiliently-mounted
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R31/00Coupling parts supported only by co-operation with counterpart
    • H01R31/06Intermediate parts for linking two coupling parts, e.g. adapter
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R4/00Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation
    • H01R4/28Clamped connections, spring connections
    • H01R4/50Clamped connections, spring connections utilising a cam, wedge, cone or ball also combined with a screw
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B3/00Ohmic-resistance heating
    • H05B3/02Details
    • H05B3/06Heater elements structurally combined with coupling elements or holders
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B3/00Ohmic-resistance heating
    • H05B3/20Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater
    • H05B3/22Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater non-flexible
    • H05B3/28Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater non-flexible heating conductor embedded in insulating material
    • H05B3/30Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater non-flexible heating conductor embedded in insulating material on or between metallic plates
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R4/00Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation
    • H01R4/10Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation effected solely by twisting, wrapping, bending, crimping, or other permanent deformation
    • H01R4/18Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation effected solely by twisting, wrapping, bending, crimping, or other permanent deformation by crimping
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R4/00Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation
    • H01R4/10Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation effected solely by twisting, wrapping, bending, crimping, or other permanent deformation
    • H01R4/18Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation effected solely by twisting, wrapping, bending, crimping, or other permanent deformation by crimping
    • H01R4/20Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation effected solely by twisting, wrapping, bending, crimping, or other permanent deformation by crimping using a crimping sleeve
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B2203/00Aspects relating to Ohmic resistive heating covered by group H05B3/00
    • H05B2203/002Heaters using a particular layout for the resistive material or resistive elements
    • H05B2203/003Heaters using a particular layout for the resistive material or resistive elements using serpentine layout
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B2203/00Aspects relating to Ohmic resistive heating covered by group H05B3/00
    • H05B2203/002Heaters using a particular layout for the resistive material or resistive elements
    • H05B2203/005Heaters using a particular layout for the resistive material or resistive elements using multiple resistive elements or resistive zones isolated from each other
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B2203/00Aspects relating to Ohmic resistive heating covered by group H05B3/00
    • H05B2203/013Heaters using resistive films or coatings
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B2203/00Aspects relating to Ohmic resistive heating covered by group H05B3/00
    • H05B2203/017Manufacturing methods or apparatus for heaters
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B2214/00Aspects relating to resistive heating, induction heating and heating using microwaves, covered by groups H05B3/00, H05B6/00
    • H05B2214/02Heaters specially designed for de-icing or protection against icing
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49002Electrical device making
    • Y10T29/49082Resistor making
    • Y10T29/49083Heater type

Definitions

  • the present invention relates generally to turbine engines and more particularly to a connector for a heater for an inner strut of an inlet case of a turbine engine.
  • Some gas turbine engines particularly gas turbine engines for military aircraft, include inlet struts in the inlet case in front of the fan. It is possible for snow and ice to accumulate on the inlet struts and to interfere with operation of the gas turbine engine. Accordingly, the assignee of the present invention has developed a heater system for the inlet struts.
  • the heater system includes a flexible polymer mat having a plurality of metal electrical traces or heating elements formed therein. The mat is installed around the inlet strut. Electrical current through the heating elements generates heat in the mat, which melts away any snow and ice that have accumulated on the inlet strut.
  • the present invention provides a connector for incorporation into the heater system for inlet struts.
  • the connector includes a body having a tapered forward end and an opposite rear end.
  • a plurality of forward electrical terminals are formed on the outer surface of the tapered end.
  • a plurality of rearward electrical terminals are formed on the rear end of the body. The rearward electrical terminals are in electrical connection with the forward electrical terminals.
  • the forward electrical terminals on the tapered end are in electrical contact with a plurality of electrical contacts connected to heating elements formed in a heating mat.
  • the heating mat entirely envelops the connector.
  • the heater mat is formed within a substantially rigid outer shell.
  • the rearward electrical terminals of the connector make electrical contact with a socket formed on the inlet strut when the shell and heater mat are inserted onto the inlet strut. Electrical power to the heater mat is thus provided from the socket on the inlet strut through the connector to the heating elements in the heater mat.
  • FIG. 1 is a sectional view of a gas turbine engine in which the present invention could be used.
  • FIG. 2 is a perspective view of a section of the inlet case and inlet strut with the heater system exploded away.
  • FIG. 3 is a sectional view through the shell, heater mat, connector and inlet strut of FIG. 2 in an assembled position.
  • FIG. 4 is a rear perspective view of the connector.
  • FIG. 5 is a perspective view of the heater mat in a partially unfolded position.
  • FIG. 6 is an enlarged rear perspective view of the tab and contacts on the heater mat of FIG. 5 .
  • FIG. 7 is an enlarged sectional view of the connector inside the heater mat and shell.
  • FIG. 8 is a sectional view through the heating system of FIG. 2 during manufacture on a mold.
  • FIG. 9 is a perspective view of the socket of FIG. 7 .
  • FIG. 10 is a perspective view of an alternate heater mat.
  • FIG. 11 illustrates the heater mat of FIG. 10 connected to an alternate connector.
  • FIG. 12 is a sectional view through the connector and heater mat of FIG. 11 .
  • FIG. 1 shows a gas turbine engine 10 , such as a gas turbine used for power generation or propulsion, circumferentially disposed about an engine centerline or axial center line axis 12 .
  • the engine 10 includes a fan 14 , a compressor 16 , a combustion section 18 and a turbine 11 .
  • air compressed in the compressor 16 is mixed with fuel that is burned in the combustion section 18 and expands in the turbine 11 .
  • the turbine 11 includes rotors 13 and 15 that rotate in response to the expansion, driving the compressor 16 and fan 14 .
  • the turbine 11 includes alternating rows of turbine blades 20 and vanes 19 .
  • FIG. 1 is a somewhat schematic presentation for illustrative purposes only and is not a limitation on the instant invention, which may be employed on gas turbine engines for electrical power generation, aircraft, etc. Additionally, there are various types of gas turbine engines, many of which could benefit from the present invention, which is not noted to the design shown.
  • FIG. 2 is an exploded perspective view of one inlet strut 26 and heating system 28 .
  • the heating system 28 generally includes a heater mat 30 having a plurality of electrical heating elements 32 formed therein.
  • the heater mat 30 is a flexible polymer, such as Kapton, while the heating elements 32 may be a foil which may be attached to the heater mat 30 by adhesive or insert molded into the Kapton. Alternatively, the heating elements 32 may be formed by sputter deposits onto the heater mat 30 .
  • the heating elements 32 may be titanium, copper or other suitable materials.
  • the heater mat 30 is folded to form a folded forward end 34 and an open rear end 36 .
  • An electrical connector 38 is electrically connected to the heating elements 32 and positioned in the forward end 34 of the heater mat 30 .
  • a composite outer shell 40 is formed over the heater mat 30 in the electrical heating elements 32 .
  • the outer shell 40 may be a composite structure formed of numerous plies, where the heater mat 30 is one of the plies.
  • a forward end of the inlet strut includes a socket 46 or other electrical connector complimentary to the electrical connector 38 in the heating system 28 .
  • Power is supplied to the socket 46 and the electrical connector 38 by a power cable 48 passing through inlet case 24 into the inlet strut 26 in connecting to the socket 46 .
  • the heating system 28 is shipped and installed with the outer shell 40 attached to the heater mat 30 .
  • the heating system 28 is slid onto the inlet strut 26 by inserting the inlet strut 26 into the open rear end 36 of the heater mat 30 until the electrical connector 38 makes electrical connection with the socket 46 on the inlet strut 26 as shown in FIG. 3 .
  • Filler 50 in the forward end of the outer shell 40 may abut the inlet strut 26 , thereby improving the stability of the heating system 28 .
  • the heating system 28 may be further fastened to the inlet strut 26 by fasteners or adhesive.
  • the heating system 28 i.e. the outer shell 40 , heater mat 30 with heating elements 32 and the electrical connector 38
  • FIG. 4 is a rear perspective view of the connector 38 of FIGS. 2-3 .
  • the connector 38 includes a body 56 , which is preferably formed of a non-conductive polymer or composite.
  • the body 56 includes a tapered forward end 58 having curved and angled outer surfaces 60 .
  • a plurality of forward terminals 62 are formed on one of the outer surfaces 60 .
  • Each of the forward terminals 62 is in electrical connection with one of a plurality of rearward terminals 64 formed on a rear end 66 of the body 56 of the electrical connector 38 .
  • the forward terminal 62 and the rearward terminal 64 are formed on opposite ends of a plurality of conductive metal sockets 68 (one shown) insert molded in the body 56 of the electrical connector 38 .
  • FIG. 5 is a perspective view showing the heater mat 30 in a partially unfolded position.
  • the heater mat 30 includes a connection tab 74 projecting upward from the remainder of the heater mat 30 .
  • the heating elements 32 are not shown in FIG. 5
  • FIG. 6 is an enlarged rear perspective view of the connection tab 74 of the heater mat 30 of FIG. 5 .
  • the electrical heating elements 32 lead to the connection tab 74 and are electrically connected to a plurality of electrically conductive contacts 76 on the connection tab 74 . There need not be a one-to-one relationship between heating elements 32 and electrical contacts 76 .
  • FIGS. 6 , 7 and 8 illustrate how the connector 38 of FIG. 4 and the heater mat 30 of FIGS. 5-6 are used to make the heating system 28 of FIGS. 2-3 .
  • the connection tab 74 of the heater mat 30 is first folded inwardly into the interior of the heater mat 30 as indicated by the arrow in FIG. 6 , such that the contacts 76 are exposed to the interior of the heater mat 30 , as shown in FIG. 7 .
  • the connector 38 is placed in a recess at an upper corner of the mold 49 and the heater mat 30 is wrapped around the connector 38 and mold 49 .
  • the connector 38 is thereby inserted into the forward end 34 of the interior of the heater mat 30 until the forward terminals 62 of the connector 38 make electrical contact with the contacts 76 .
  • the tapered forward end 58 of the connector 38 with curved and angled outer surfaces 60 , fits snugly within the forward end 34 of the heater mat 30 .
  • the connector 38 may be joined to the heater mat 30 by welding, brazing, soldering, mechanical crimping/stapling or conductive adhesive.
  • the outer shell 40 is then formed over the heater mat 30 as a series of plies in a known manner for making composite components.
  • the heater mat 30 is shown as the innermost ply in the outer shell 40 , but could be one of the middle plies.
  • the mold 49 is then removed from the outer shell 40 , heater mat 30 and connector 38 to leave a formed heating system 28 .
  • the volume below the electrical connector 38 and between the outer shell 40 and inlet strut 26 may be filled with the filler 50 , which may be a polymer, composite, polymer foam or other material as shown in FIG. 3 .
  • the filler 50 increases the strength and durability of the heating system 28 .
  • the electrical connector 38 and socket 46 is shown located at an upper end of the inlet strut 26 and heating system 28 but could be located at any point along the inlet strut 26 .
  • the socket 68 is generally a metal conductive tube that is flattened at one end to form the forward terminal 62 and left open and round at the opposite end to form the rearward terminal 64 .
  • the socket 68 may also be bent or formed to properly locate the forward terminal 62 and rearward terminal 64 .
  • the forward terminal 62 and rearward terminal 64 could be provided in other ways.
  • FIGS. 10 through 12 illustrate an alternate way of making an electrical connection to a heater mat 30 .
  • the electrical heating elements are not shown for simplicity.
  • the alternate heater mat 30 ′ includes an alternate connection tab 74 ′ projecting upward from the remainder of the heater mat 30 ′.
  • a plurality of electrical contacts 76 ′ are formed at one end of the connection tab 74 ′.
  • the connection tab 74 ′ is flexible.
  • the connector 38 ′ is not shown, but the connection tab 74 ′ is shown folded twice as it would be to fit inside the connector 38 ′ as shown in FIG. 11 .
  • the alternate connector 38 ′ includes a removable mid-portion 61 ′ that is opposite a mid-portion 60 ′ and behind a forward portion 59 ′.
  • the removable mid-portion 61 ′ is first removed from the connector 38 ′.
  • the connection tab 74 ′ is then folded down over the mid-portion 60 ′ of the connector 38 ′, and the portion of the connection tab 74 ′ with the electrical contacts 76 ′ is folded back.
  • the removable mid-portion 61 ′ is then returned to the connector 38 ′ on top of the connection tab 74 ′, thereby retaining the connection tab 74 ′ within the connector 38 ′.
  • the mid-portion 61 ′ may be snap fit or friction fit, or even somewhat loosely retained in the connector 38 ′.
  • FIG. 12 is a sectional view taken along Line 12 - 12 of FIG. 11 after the mid-portion 61 ′ is inserted.
  • the electrical contact 76 ′ makes electrical contact with sockets 68 ′ insert-molded in the connector 38 ′.
  • the connector 38 ′ may be joined to the heater mat 30 ′ by welding, brazing, soldering, mechanical crimping/stapling or conductive adhesive.
  • the assembly shown in FIG. 12 would then be placed on the mold 49 and wrapped with the outer shell 40 as shown with respect to the first embodiment in FIGS. 7 and 8 .
  • the connector 38 ′ and heater mat 30 ′ of FIGS. 10-12 could be used in place of the connector 38 and heater mat 30 of FIGS. 1-9 .

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Resistance Heating (AREA)

Abstract

A connector for incorporation into a heater system for inlet struts includes a body having a tapered forward end and an opposite rear end. A plurality of forward electrical terminals are formed on the outer surface of the tapered end. A plurality of rearward electrical terminals are formed on the rear end of the body. The rearward electrical terminals are in electrical connection with the forward electrical terminals. The forward electrical terminals on the tapered end are in electrical contact with a plurality of electrical contacts connected to heating elements formed in a heating mat. The heating mat entirely envelops the connector. The heater mat is formed within a substantially rigid outer shell.

Description

  • This invention was made with Government support under N00019-02-C-3003 awarded by the United States Navy. The Government has certain rights in this invention.
  • BACKGROUND OF THE INVENTION
  • The present invention relates generally to turbine engines and more particularly to a connector for a heater for an inner strut of an inlet case of a turbine engine.
  • Some gas turbine engines, particularly gas turbine engines for military aircraft, include inlet struts in the inlet case in front of the fan. It is possible for snow and ice to accumulate on the inlet struts and to interfere with operation of the gas turbine engine. Accordingly, the assignee of the present invention has developed a heater system for the inlet struts. The heater system includes a flexible polymer mat having a plurality of metal electrical traces or heating elements formed therein. The mat is installed around the inlet strut. Electrical current through the heating elements generates heat in the mat, which melts away any snow and ice that have accumulated on the inlet strut.
  • SUMMARY OF THE INVENTION
  • The present invention provides a connector for incorporation into the heater system for inlet struts. The connector includes a body having a tapered forward end and an opposite rear end. A plurality of forward electrical terminals are formed on the outer surface of the tapered end. A plurality of rearward electrical terminals are formed on the rear end of the body. The rearward electrical terminals are in electrical connection with the forward electrical terminals.
  • The forward electrical terminals on the tapered end are in electrical contact with a plurality of electrical contacts connected to heating elements formed in a heating mat. The heating mat entirely envelops the connector. The heater mat is formed within a substantially rigid outer shell.
  • The rearward electrical terminals of the connector make electrical contact with a socket formed on the inlet strut when the shell and heater mat are inserted onto the inlet strut. Electrical power to the heater mat is thus provided from the socket on the inlet strut through the connector to the heating elements in the heater mat.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • Other advantages of the present invention can be understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein:
  • FIG. 1 is a sectional view of a gas turbine engine in which the present invention could be used.
  • FIG. 2 is a perspective view of a section of the inlet case and inlet strut with the heater system exploded away.
  • FIG. 3 is a sectional view through the shell, heater mat, connector and inlet strut of FIG. 2 in an assembled position.
  • FIG. 4 is a rear perspective view of the connector.
  • FIG. 5 is a perspective view of the heater mat in a partially unfolded position.
  • FIG. 6 is an enlarged rear perspective view of the tab and contacts on the heater mat of FIG. 5.
  • FIG. 7 is an enlarged sectional view of the connector inside the heater mat and shell.
  • FIG. 8 is a sectional view through the heating system of FIG. 2 during manufacture on a mold.
  • FIG. 9 is a perspective view of the socket of FIG. 7.
  • FIG. 10 is a perspective view of an alternate heater mat.
  • FIG. 11 illustrates the heater mat of FIG. 10 connected to an alternate connector.
  • FIG. 12 is a sectional view through the connector and heater mat of FIG. 11.
  • DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
  • FIG. 1 shows a gas turbine engine 10, such as a gas turbine used for power generation or propulsion, circumferentially disposed about an engine centerline or axial center line axis 12. The engine 10 includes a fan 14, a compressor 16, a combustion section 18 and a turbine 11. As is well known, air compressed in the compressor 16 is mixed with fuel that is burned in the combustion section 18 and expands in the turbine 11. The turbine 11 includes rotors 13 and 15 that rotate in response to the expansion, driving the compressor 16 and fan 14. The turbine 11 includes alternating rows of turbine blades 20 and vanes 19. The fan 14 is surrounded by an inlet case 24, which is supported by a plurality of inlet struts 26, which are positioned inside the inlet case 24 in front of the fan 14. Each of the inlet struts 26 is wrapped by a heating system 28. FIG. 1 is a somewhat schematic presentation for illustrative purposes only and is not a limitation on the instant invention, which may be employed on gas turbine engines for electrical power generation, aircraft, etc. Additionally, there are various types of gas turbine engines, many of which could benefit from the present invention, which is not noted to the design shown.
  • FIG. 2 is an exploded perspective view of one inlet strut 26 and heating system 28. The heating system 28 generally includes a heater mat 30 having a plurality of electrical heating elements 32 formed therein. Generally, the heater mat 30 is a flexible polymer, such as Kapton, while the heating elements 32 may be a foil which may be attached to the heater mat 30 by adhesive or insert molded into the Kapton. Alternatively, the heating elements 32 may be formed by sputter deposits onto the heater mat 30. The heating elements 32 may be titanium, copper or other suitable materials. The heater mat 30 is folded to form a folded forward end 34 and an open rear end 36. An electrical connector 38 is electrically connected to the heating elements 32 and positioned in the forward end 34 of the heater mat 30. A composite outer shell 40 is formed over the heater mat 30 in the electrical heating elements 32. The outer shell 40 may be a composite structure formed of numerous plies, where the heater mat 30 is one of the plies.
  • A forward end of the inlet strut includes a socket 46 or other electrical connector complimentary to the electrical connector 38 in the heating system 28. Power is supplied to the socket 46 and the electrical connector 38 by a power cable 48 passing through inlet case 24 into the inlet strut 26 in connecting to the socket 46.
  • Although illustrated in an exploded view in FIG. 2, the heating system 28 is shipped and installed with the outer shell 40 attached to the heater mat 30. For assembly, the heating system 28 is slid onto the inlet strut 26 by inserting the inlet strut 26 into the open rear end 36 of the heater mat 30 until the electrical connector 38 makes electrical connection with the socket 46 on the inlet strut 26 as shown in FIG. 3. Filler 50 in the forward end of the outer shell 40 may abut the inlet strut 26, thereby improving the stability of the heating system 28. The heating system 28 may be further fastened to the inlet strut 26 by fasteners or adhesive. The heating system 28 (i.e. the outer shell 40, heater mat 30 with heating elements 32 and the electrical connector 38) can be installed, removed and replaced on the inlet strut 26.
  • FIG. 4 is a rear perspective view of the connector 38 of FIGS. 2-3. The connector 38 includes a body 56, which is preferably formed of a non-conductive polymer or composite. The body 56 includes a tapered forward end 58 having curved and angled outer surfaces 60. A plurality of forward terminals 62 are formed on one of the outer surfaces 60. Each of the forward terminals 62 is in electrical connection with one of a plurality of rearward terminals 64 formed on a rear end 66 of the body 56 of the electrical connector 38. In the embodiment shown, the forward terminal 62 and the rearward terminal 64 are formed on opposite ends of a plurality of conductive metal sockets 68 (one shown) insert molded in the body 56 of the electrical connector 38.
  • FIG. 5 is a perspective view showing the heater mat 30 in a partially unfolded position. As shown, the heater mat 30 includes a connection tab 74 projecting upward from the remainder of the heater mat 30. For simplicity, the heating elements 32 are not shown in FIG. 5, but FIG. 6 is an enlarged rear perspective view of the connection tab 74 of the heater mat 30 of FIG. 5. As shown, the electrical heating elements 32 lead to the connection tab 74 and are electrically connected to a plurality of electrically conductive contacts 76 on the connection tab 74. There need not be a one-to-one relationship between heating elements 32 and electrical contacts 76.
  • FIGS. 6, 7 and 8 illustrate how the connector 38 of FIG. 4 and the heater mat 30 of FIGS. 5-6 are used to make the heating system 28 of FIGS. 2-3. Referring first to FIG. 6, the connection tab 74 of the heater mat 30 is first folded inwardly into the interior of the heater mat 30 as indicated by the arrow in FIG. 6, such that the contacts 76 are exposed to the interior of the heater mat 30, as shown in FIG. 7.
  • Referring to FIGS. 7 and 8, the connector 38 is placed in a recess at an upper corner of the mold 49 and the heater mat 30 is wrapped around the connector 38 and mold 49. The connector 38 is thereby inserted into the forward end 34 of the interior of the heater mat 30 until the forward terminals 62 of the connector 38 make electrical contact with the contacts 76. The tapered forward end 58 of the connector 38, with curved and angled outer surfaces 60, fits snugly within the forward end 34 of the heater mat 30. The connector 38 may be joined to the heater mat 30 by welding, brazing, soldering, mechanical crimping/stapling or conductive adhesive. The outer shell 40 is then formed over the heater mat 30 as a series of plies in a known manner for making composite components. The heater mat 30 is shown as the innermost ply in the outer shell 40, but could be one of the middle plies. The mold 49 is then removed from the outer shell 40, heater mat 30 and connector 38 to leave a formed heating system 28.
  • After removal of the mold 49, the volume below the electrical connector 38 and between the outer shell 40 and inlet strut 26 (previously occupied by the mold) may be filled with the filler 50, which may be a polymer, composite, polymer foam or other material as shown in FIG. 3. The filler 50 increases the strength and durability of the heating system 28. The electrical connector 38 and socket 46 is shown located at an upper end of the inlet strut 26 and heating system 28 but could be located at any point along the inlet strut 26.
  • One of the sockets 68 from inside the connector 38 of FIG. 4 is shown in FIG. 9. The socket 68 is generally a metal conductive tube that is flattened at one end to form the forward terminal 62 and left open and round at the opposite end to form the rearward terminal 64. The socket 68 may also be bent or formed to properly locate the forward terminal 62 and rearward terminal 64. The forward terminal 62 and rearward terminal 64 could be provided in other ways.
  • FIGS. 10 through 12 illustrate an alternate way of making an electrical connection to a heater mat 30. The electrical heating elements are not shown for simplicity.
  • Referring to FIG. 10, the alternate heater mat 30′ includes an alternate connection tab 74′ projecting upward from the remainder of the heater mat 30′. A plurality of electrical contacts 76′ are formed at one end of the connection tab 74′. The connection tab 74′ is flexible. In FIG. 10, the connector 38′ is not shown, but the connection tab 74′ is shown folded twice as it would be to fit inside the connector 38′ as shown in FIG. 11. Referring to FIG. 11, the alternate connector 38′ includes a removable mid-portion 61′ that is opposite a mid-portion 60′ and behind a forward portion 59′.
  • To connect the electrical connector 38′ to the electrical contacts 76′, the removable mid-portion 61′ is first removed from the connector 38′. The connection tab 74′ is then folded down over the mid-portion 60′ of the connector 38′, and the portion of the connection tab 74′ with the electrical contacts 76′ is folded back. The removable mid-portion 61′ is then returned to the connector 38′ on top of the connection tab 74′, thereby retaining the connection tab 74′ within the connector 38′. The mid-portion 61′ may be snap fit or friction fit, or even somewhat loosely retained in the connector 38′.
  • FIG. 12 is a sectional view taken along Line 12-12 of FIG. 11 after the mid-portion 61′ is inserted. As shown in FIG. 12, the electrical contact 76′ makes electrical contact with sockets 68′ insert-molded in the connector 38′. Again, the connector 38′ may be joined to the heater mat 30′ by welding, brazing, soldering, mechanical crimping/stapling or conductive adhesive. The assembly shown in FIG. 12 would then be placed on the mold 49 and wrapped with the outer shell 40 as shown with respect to the first embodiment in FIGS. 7 and 8. The connector 38′ and heater mat 30′ of FIGS. 10-12 could be used in place of the connector 38 and heater mat 30 of FIGS. 1-9.
  • In accordance with the provisions of the patent statutes and jurisprudence, exemplary configurations described above are considered to represent a preferred embodiment of the invention. However, it should be noted that the invention can be practiced otherwise than as specifically illustrated and described without departing from its spirit or scope. Alphanumeric identifiers in method steps are for convenient reference in dependent claims and do not indicate a required order of performance of the method steps unless otherwise specified in the claims.

Claims (21)

1) A connector comprising:
a body having a forward tapered end and a rear end, the tapered end including an outer surface;
a plurality of forward terminals on the tapered end; and
a plurality of rearward terminals on the rear end of the body, the rearward terminals in electrical connection with the forward terminals.
2) The connector of claim 1 wherein the outer surface of the tapered end includes a pair of angled surfaces.
3) The connector of claim 2 wherein the plurality of forward terminals are formed on one of the pair of angled surfaces.
4) The connector of claim 3 wherein the pair of angled surfaces are convex.
5) The connector of claim 1 wherein the tapered end includes a removable portion removably secured over the forward terminals.
6) The connector of claim 1 and a heater electrically connected to the plurality of forward terminals on the connector.
7) The connector and heater of claim 6 wherein the heater fully envelops the connector.
8) The connector and heater of claim 7 wherein the heater includes a plurality of electrical heating elements, each connected to at least one of the plurality of forward terminals.
9) The connector and heater of claim 8 wherein the plurality of electrical heating elements includes a plurality of contacts in direct contact with the plurality of forward terminals of the connector.
10) The connector and heater of claim 6 wherein the heater includes a shell in which the connector is mounted.
11) The connector and heater of claim 10 wherein the shell includes a pair of spaced apart walls joined by a forward end, the connector mounted in the forward end of the shell.
12) The connector and heater of claim 11 wherein the shell is a composite shell and the heater includes a heater mat that is a layer in the shell.
13) The connector and heater of claim 6 mounted to a turbine engine structure.
14) The connector, heater and turbine engine structure of claim 13 wherein the turbine engine structure is a strut.
15) A turbine engine including the connector, heater and strut of claim 14, wherein the strut is an inner strut of an inlet case.
16) A heater for a turbine engine strut comprising:
a heating element; and
a connector in connection with the heating element, the connector having a contact at a rearward end for mating with a complementary connector on a turbine engine strut.
17) The heater of claim 16 wherein the heating element is one of a plurality of heating elements formed in a pair of spaced-apart walls joined at a forward end.
18) The heater of claim 17 wherein the connector is mounted in the forward end of the pair of walls.
19) The heater of claim 18 wherein the heating element is an electrical heating element.
20) A method of forming a heating system for a strut in a turbine engine including the steps of:
a) placing a connector adjacent a mold;
b) placing a plurality of heating elements over the mold;
c) connecting the plurality of heating elements to the connector;
d) forming an outer shell over the connector and the mold; and
e) removing the mold from the outer shell.
21) The method of claim 20 wherein at least a portion of the outer shell is formed over the plurality of heating elements in said step d).
US11/221,195 2005-09-07 2005-09-07 Connector for heater Abandoned US20080041842A1 (en)

Priority Applications (11)

Application Number Priority Date Filing Date Title
US11/221,195 US20080041842A1 (en) 2005-09-07 2005-09-07 Connector for heater
CA002553300A CA2553300A1 (en) 2005-09-07 2006-07-21 Connector for heater
IL177029A IL177029A0 (en) 2005-09-07 2006-07-23 Connector for heater
JP2006200710A JP2007071199A (en) 2005-09-07 2006-07-24 Heater for turbine engine strut, electrical connector and method for forming heating device
AU2006203145A AU2006203145A1 (en) 2005-09-07 2006-07-24 Connector for Heater
CNA2006101513490A CN1933243A (en) 2005-09-07 2006-07-25 Connector for heater
BRPI0602901-9A BRPI0602901A (en) 2005-09-07 2006-07-26 connector, turbine engine, heater for a turbine engine holder, and method for forming a heating system for a holder in a turbine engine
EP06253970A EP1762714B1 (en) 2005-09-07 2006-07-28 Heater for a gas turbine engine strut, electrical connector for this heater and corresponding manufacturing method
SG200605273-2A SG131009A1 (en) 2005-09-07 2006-08-04 Connector for heater
KR1020060074025A KR20070028219A (en) 2005-09-07 2006-08-07 Connector for heater
US12/605,652 US8247746B2 (en) 2005-09-07 2009-10-26 Connector for heater

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/221,195 US20080041842A1 (en) 2005-09-07 2005-09-07 Connector for heater

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US12/605,652 Continuation US8247746B2 (en) 2005-09-07 2009-10-26 Connector for heater

Publications (1)

Publication Number Publication Date
US20080041842A1 true US20080041842A1 (en) 2008-02-21

Family

ID=37067631

Family Applications (2)

Application Number Title Priority Date Filing Date
US11/221,195 Abandoned US20080041842A1 (en) 2005-09-07 2005-09-07 Connector for heater
US12/605,652 Expired - Fee Related US8247746B2 (en) 2005-09-07 2009-10-26 Connector for heater

Family Applications After (1)

Application Number Title Priority Date Filing Date
US12/605,652 Expired - Fee Related US8247746B2 (en) 2005-09-07 2009-10-26 Connector for heater

Country Status (10)

Country Link
US (2) US20080041842A1 (en)
EP (1) EP1762714B1 (en)
JP (1) JP2007071199A (en)
KR (1) KR20070028219A (en)
CN (1) CN1933243A (en)
AU (1) AU2006203145A1 (en)
BR (1) BRPI0602901A (en)
CA (1) CA2553300A1 (en)
IL (1) IL177029A0 (en)
SG (1) SG131009A1 (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100015455A1 (en) * 2008-07-21 2010-01-21 United Technologies Corporation Method and assembly for validating bond line
US20100024612A1 (en) * 2008-07-30 2010-02-04 United Technologies Corporation Installation tool for use with u-shaped component
US20100108661A1 (en) * 2008-10-31 2010-05-06 United Technologies Corporation Multi-layer heating assembly and method
US20100322782A1 (en) * 2008-04-02 2010-12-23 United Technologies Corporation Nosecone bolt access and aerodynamic leakage baffle
US20110053468A1 (en) * 2009-08-31 2011-03-03 United Technologies Corporation Thermal mechanical skive for composite machining
US20140366552A1 (en) * 2013-06-18 2014-12-18 Alstom Technology Ltd Method and device for suppressing the formation of ice on structures at the air intake of a turbomachine
EP3228834A1 (en) * 2016-04-08 2017-10-11 Safran Aero Boosters SA Turbomachine blade, corresponding compressor, turbomachine and production method
US10815885B2 (en) * 2018-07-26 2020-10-27 Raytheon Technologies Corporation Anti-ice systems for engine airfoils
US11325548B2 (en) 2017-06-09 2022-05-10 Gentherm Gmbh Heating mat with electric control unit integrated connector
US20230128806A1 (en) * 2021-10-27 2023-04-27 General Electric Company Airfoils for a fan section of a turbine engine
US20240003294A1 (en) * 2021-08-23 2024-01-04 General Electric Company Ice reduction mechanism for turbofan engine
US12108498B2 (en) 2020-10-16 2024-10-01 Ngk Insulators, Ltd. Wafer placement table

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9133714B2 (en) 2006-11-01 2015-09-15 United Technologies Corporation Titanium foil as a structural heater element
GB2497807B (en) 2011-12-22 2014-09-10 Rolls Royce Plc Electrical harness
US9478896B2 (en) 2011-12-22 2016-10-25 Rolls-Royce Plc Electrical connectors
GB2497809B (en) 2011-12-22 2014-03-12 Rolls Royce Plc Method of servicing a gas turbine engine
GB2498006B (en) 2011-12-22 2014-07-09 Rolls Royce Plc Gas turbine engine systems
EP2685565B1 (en) * 2012-07-10 2016-09-07 Rolls-Royce plc Electrical connectors
FR2995949B1 (en) * 2012-09-25 2018-05-25 Safran Aircraft Engines TURBOMACHINE HOUSING
US9297307B2 (en) * 2012-09-28 2016-03-29 United Technologies Corporation Power cable and connector arrangement for a gas turbine engine
EP2943657B1 (en) 2013-01-14 2019-08-14 United Technologies Corporation Organic matrix composite structural inlet guide vane for a turbine engine
GB201308025D0 (en) 2013-05-03 2013-06-12 Rolls Royce Plc Electrical connectors
WO2015076960A1 (en) * 2013-11-21 2015-05-28 United Technologies Corporation Method to integrate multiple electric circuits into organic matrix composite
DE102016215030A1 (en) * 2016-08-11 2018-02-15 Rolls-Royce Deutschland Ltd & Co Kg Turbofan engine with a lying in the secondary flow channel and a separate end element panel
GB2599691A (en) * 2020-10-09 2022-04-13 Rolls Royce Plc A heat exchanger
GB2599693B (en) * 2020-10-09 2022-12-14 Rolls Royce Plc A heat exchanger

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2742248A (en) * 1952-02-16 1956-04-17 Curtiss Wright Corp Propeller blade de-icing
US2744992A (en) * 1951-03-30 1956-05-08 Gen Motors Corp Deicing control
US4659161A (en) * 1984-04-06 1987-04-21 Holcomb Kenneth L Adapter plug for personal computers
US6024588A (en) * 1998-05-26 2000-02-15 Hsu; I-Ching Multi-socket computer adapter having a reversible plug
US20020162222A1 (en) * 2001-05-02 2002-11-07 Williams Charles G. Overmolding insert for heat exchanger, process for manufacturing a heat exchanger, and heat exchanger produced thereby
US6481965B2 (en) * 2000-12-08 2002-11-19 Eurocopter Rotary-wing aircraft rotors with manually folding blades and electrical connection installation
US20020182905A1 (en) * 2000-08-22 2002-12-05 Paul Hedrick Locking electrical receptacle
US20050008482A1 (en) * 2003-07-11 2005-01-13 Rolls-Royce Plc Inlet guide vane

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5123852A (en) * 1991-05-17 1992-06-23 International Business Machines Corporation Modular electrical connector
CN1049090C (en) 1995-08-21 2000-02-09 山东农业大学 Agricultural chemical composite
GB9703248D0 (en) 1997-02-17 1997-04-09 Singh Steven S Remote control adapter
JPH10294157A (en) 1997-04-21 1998-11-04 Harness Sogo Gijutsu Kenkyusho:Kk Relay connector structure of portable telephone
JPH11121123A (en) 1997-10-15 1999-04-30 Churi:Kk Transformer

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2744992A (en) * 1951-03-30 1956-05-08 Gen Motors Corp Deicing control
US2742248A (en) * 1952-02-16 1956-04-17 Curtiss Wright Corp Propeller blade de-icing
US4659161A (en) * 1984-04-06 1987-04-21 Holcomb Kenneth L Adapter plug for personal computers
US6024588A (en) * 1998-05-26 2000-02-15 Hsu; I-Ching Multi-socket computer adapter having a reversible plug
US20020182905A1 (en) * 2000-08-22 2002-12-05 Paul Hedrick Locking electrical receptacle
US6481965B2 (en) * 2000-12-08 2002-11-19 Eurocopter Rotary-wing aircraft rotors with manually folding blades and electrical connection installation
US20020162222A1 (en) * 2001-05-02 2002-11-07 Williams Charles G. Overmolding insert for heat exchanger, process for manufacturing a heat exchanger, and heat exchanger produced thereby
US20050008482A1 (en) * 2003-07-11 2005-01-13 Rolls-Royce Plc Inlet guide vane

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100322782A1 (en) * 2008-04-02 2010-12-23 United Technologies Corporation Nosecone bolt access and aerodynamic leakage baffle
US8292592B2 (en) 2008-04-02 2012-10-23 United Technologies Corporation Nosecone bolt access and aerodynamic leakage baffle
US8349104B2 (en) 2008-07-21 2013-01-08 United Technologies Corporation Method and assembly for validating bond line
US20100015455A1 (en) * 2008-07-21 2010-01-21 United Technologies Corporation Method and assembly for validating bond line
US20100024612A1 (en) * 2008-07-30 2010-02-04 United Technologies Corporation Installation tool for use with u-shaped component
US8875374B2 (en) 2008-07-30 2014-11-04 United Technologies Corporation Method of installing a flexible component in a U-shaped component
US20100108661A1 (en) * 2008-10-31 2010-05-06 United Technologies Corporation Multi-layer heating assembly and method
US20110053468A1 (en) * 2009-08-31 2011-03-03 United Technologies Corporation Thermal mechanical skive for composite machining
US8342908B2 (en) 2009-08-31 2013-01-01 United Technologies Corporation Thermal mechanical skive for composite machining
US20140366552A1 (en) * 2013-06-18 2014-12-18 Alstom Technology Ltd Method and device for suppressing the formation of ice on structures at the air intake of a turbomachine
US9708929B2 (en) * 2013-06-18 2017-07-18 Ansaldo Energia Switzerland AG Method and device for suppressing the formation of ice on structures at the air intake of a turbomachine
EP3228834A1 (en) * 2016-04-08 2017-10-11 Safran Aero Boosters SA Turbomachine blade, corresponding compressor, turbomachine and production method
US20170298760A1 (en) * 2016-04-08 2017-10-19 Safran Aero Boosters Sa Axial Turbine Engine Compressor De-Icing Blade
US11325548B2 (en) 2017-06-09 2022-05-10 Gentherm Gmbh Heating mat with electric control unit integrated connector
US10815885B2 (en) * 2018-07-26 2020-10-27 Raytheon Technologies Corporation Anti-ice systems for engine airfoils
US12108498B2 (en) 2020-10-16 2024-10-01 Ngk Insulators, Ltd. Wafer placement table
US20240003294A1 (en) * 2021-08-23 2024-01-04 General Electric Company Ice reduction mechanism for turbofan engine
US20230128806A1 (en) * 2021-10-27 2023-04-27 General Electric Company Airfoils for a fan section of a turbine engine
US11988103B2 (en) * 2021-10-27 2024-05-21 General Electric Company Airfoils for a fan section of a turbine engine

Also Published As

Publication number Publication date
CA2553300A1 (en) 2007-03-07
EP1762714B1 (en) 2011-11-09
CN1933243A (en) 2007-03-21
EP1762714A2 (en) 2007-03-14
AU2006203145A1 (en) 2007-03-22
US8247746B2 (en) 2012-08-21
US20100170887A1 (en) 2010-07-08
KR20070028219A (en) 2007-03-12
SG131009A1 (en) 2007-04-26
EP1762714A3 (en) 2009-11-04
JP2007071199A (en) 2007-03-22
BRPI0602901A (en) 2007-04-27
IL177029A0 (en) 2006-12-10

Similar Documents

Publication Publication Date Title
US8247746B2 (en) Connector for heater
US8033790B2 (en) Multiple piece turbine engine airfoil with a structural spar
US8434292B2 (en) Ceramic-encased hot surface igniter system for jet engines
RU2448258C2 (en) Gas turbine engine blade assembly and gas turbine stator with said assembly
JP6765873B2 (en) Electric circuit breaker
EP3033510A2 (en) Fuel igniter assembly having heat-dissipating element and methods of using same
CN110169599A (en) Monolithic plane and its manufacturing method with electrical contact
CN114583369A (en) Battery pack
JP2003014234A (en) Mounting of cmc combustion chamber in turbo machine using brazed tub
US7055306B2 (en) Combined stage single shaft turbofan engine
JP6684170B2 (en) Electrical circuit breaker
US10724438B2 (en) Apparatus and method for heating pre-combustor air in a gas turbine engine
US10811850B2 (en) Spark plug of internal combustion engine
US20090148280A1 (en) Turbine Vane for a Gas Turbine Engine
JP3604143B2 (en) Igniter plug guide used in gas turbine engine combustor
US20110048111A1 (en) Method of leak testing aerospace components
CN111379593A (en) Hybrid rotor blade for a turbine engine
EP3857042B1 (en) Hybrid jet engine
US6691660B2 (en) Glow plug energizing device
EP2119893A2 (en) Recuperators for gas turbine engines
JP6962752B2 (en) Electric circuit breaker
EP1669554A1 (en) Thrust bearing assembly for a gas turbine engine
CN110806275A (en) Exhaust gas temperature sensor
US11591096B1 (en) Artificial ice for an aircraft component
CN219679785U (en) Central heating structure and electronic cigarette

Legal Events

Date Code Title Description
AS Assignment

Owner name: UNITED TECHNOLOGIES CORPORATION, CONNECTICUT

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:ALEXANDER, PHILLIP EMERSON;LYDERS, DAVID R.;VONTELL, JOHN;AND OTHERS;REEL/FRAME:016968/0302

Effective date: 20050907

STCB Information on status: application discontinuation

Free format text: EXPRESSLY ABANDONED -- DURING PUBLICATION PROCESS