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公开(公告)号:JP2001289122A
公开(公告)日:2001-10-19
申请号:JP2001057733
申请日:2001-03-02
Applicant: UNITED TECHNOLOGIES CORP
Inventor: REY NANCY M , ROBIN MIHEKUN MILLER , TILLMAN THOMAS G , RUKUS ROBERT M , KETTLE JOHN L , DUNPHY JAMES R , CHAUDHRY ZAFFIR A , PEARSON DAVID D , DREITLEIN KENNETH C , LOFFREDO CONSTANTINO V , WYNOSKY THOMAS A
Abstract: PROBLEM TO BE SOLVED: To provide a gas turbine engine with a variable area nozzle requiring no large-scale maintenance without largely increasing the total weight of the gas turbine engine. SOLUTION: The gas turbine engine 10 includes a variable area nozzle 30 having a plurality of flaps 38. The flaps 38 are actuated by a plurality of actuating mechanisms 40 to be driven by a shape memory alloy(SMA) actuator 68. The SMA actuator 68 has a deformed shape in a martensitic state and a basic shape in an austenitic state. The SMA actuator 68 is heated to transform from the martensitic state into the austenitic state generating a force to actuate the flaps 38. The variable area nozzle 30 also contains a plurality of return mechanisms 42 for deforming the SMA actuator 68 when in the martensitic state.
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公开(公告)号:JP2001304095A
公开(公告)日:2001-10-31
申请号:JP2001059797
申请日:2001-03-05
Applicant: UNITED TECHNOLOGIES CORP
Inventor: REY NANCY M , ROBIN MIHEKUN MILLER , TILLMAN THOMAS G , RUKUS ROBERT M , KETTLE JOHN L
Abstract: PROBLEM TO BE SOLVED: To increase force generated from an SMA material. SOLUTION: An SMA bundle 10 is formed of an individual SMA wire 12. This SMA bundle 10 has a base phase shape and a deformation shape, and outputs large force by returning to the base phase state by being heated in a deformation state. The SMA wire 12 for constituting the SMA bundle 10 can be constituted as a strand, a rope, a row or the other shape.
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公开(公告)号:DK0862729T3
公开(公告)日:2002-05-13
申请号:DK96940596
申请日:1996-11-21
Applicant: UNITED TECHNOLOGIES CORP
Inventor: DUNPHY JAMES R , RUKUS ROBERT M , HA JONG-MIN
IPC: B29C35/02 , B29C70/54 , G01B11/16 , G01C19/56 , G01D5/353 , G01H11/06 , G01M11/08 , G01N11/00 , G01N33/44 , G01P15/125 , G01K11/32 , G01L1/24
Abstract: Resin curing of a composite laminated structure is monitored using an optical fiber 20 having a grating sensor 28 embedded therein. The fiber 20 is surrounded by upper and lower buffer regions 12,14 having a predetermined minimum number of layers 30 (or thickness) with uni-directional reinforcing filaments 32 and resin 34 therebetween. When the filaments 32 are oriented perpendicular to the longitudinal axis of the fiber 20, the buffer regions 12,14 allow the sensor 28 to exhibit maximum sensitivity to detection of the minimum resin viscosity and the gelation point (i.e., the onset of a rapid crosslinking rate) of the resin 34. The buffer regions 12,14 also have a minimum thickness which serve to isolate the sensor 28 from interfering stresses from arbitrarily angled filaments 32 in layers 30 of outer regions 10,16 which surround the buffer regions 12,14.
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公开(公告)号:DE60112150D1
公开(公告)日:2005-09-01
申请号:DE60112150
申请日:2001-03-02
Applicant: UNITED TECHNOLOGIES CORP
Inventor: REY NANCY M , MILLER ROBIN MIHEKUN , TILLMAN THOMAS G , RUKUS ROBERT M , KETTLE JOHN L , DUNPHY JAMES R , CHAUDHRY ZAFFIR A , PEARSON DAVID D , DREITLEIN KENNETH C , LOFFREDO CONSTANTINO V , WYNOSKY THOMAS A
Abstract: A gas turbine engine (10) includes a variable area nozzle (30) having a plurality of flaps (38). The flaps (38) are actuated by a plurality of actuating mechanisms (40) driven by shape memory alloy (SMA) actuators (68) to vary fan exist nozzle area (36). The SMA actuator (68) has a deformed shape in its martensitic state and a parent shape in its austenitic state. The SMA actuator (68) is heated to transform from martensitic state to austenitic state generating a force output to actuate the flaps (38). The variable area nozzle (30) also includes a plurality of return mechanisms (42) deforming the SMA actuator (68) when the SMA actuator (68) is in its martensitic state.
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公开(公告)号:DE60134347D1
公开(公告)日:2008-07-17
申请号:DE60134347
申请日:2001-03-02
Applicant: UNITED TECHNOLOGIES CORP
Inventor: REY NANCY M , DUNPHY JAMES R , MILLER ROBIN MIHEKUN , CHAUDRY ZAFFIR A , TILMAN THOMAS G , PEARSON DAVID D , RUKUS ROBERT M , DREITLEIN KENNETH C , KETTLE JOHN L , LOFFREDO CONSTANTINTO , WYNOSKY THOMAS A
Abstract: A gas turbine engine (10) includes a variable area nozzle (30) having a plurality of flaps (38). The flaps (38) are actuated by a plurality of actuating mechanisms (40) driven by shape memory alloy (SMA) actuators (68) to vary fan exist nozzle area (36). The SMA actuator (68) has a deformed shape in its martensitic state and a parent shape in its austenitic state. The SMA actuator (68) is heated to transform from martensitic state to austenitic state generating a force output to actuate the flaps (38). The variable area nozzle (30) also includes a plurality of return mechanisms (42) deforming the SMA actuator (68) when the SMA actuator (68) is in its martensitic state.
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公开(公告)号:GR3031366T3
公开(公告)日:2000-01-31
申请号:GR990402460
申请日:1999-09-29
Applicant: UNITED TECHNOLOGIES CORP
Inventor: DUNPHY JAMES R , RUKUS ROBERT M , HA JONG-MIN
Abstract: An optical fiber entry strain relief interface includes a composite structure (lay-up) 10 having an optical fiber 20 embedded therein. The optical fiber 20 enters (or exits) the lay-up 10 at at least one point 24 and passes through transition layers 47 comprising an adhesive film 42, a thin rubber sealing layer 44, and a thick rubber strain relief layer 46, and through a polymer plug 48 located above the layer 46. The lay-up is consolidated by heating the lay-up over a temperature profile and applying pressure through mostly closed compression molding tools 30,32. The adhesive film 42 bonds the adjacent layer 44 to the upper surface of the lay-up 10, the sealing layer 44 becomes soft enough to seal around the fiber 20 at a temperature lower than the temperature at which the resin 16 exhibits a low enough viscosity to leak out of the lay-up 10, thereby preventing the resin from leaking out of the lay-up 10 during lay-up consolidation, the strain relief layer 46 provides a rubber strain relief for the optical fiber 20, and the plug 48 supports the layers 47 during consolidation.
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公开(公告)号:DE60112150T2
公开(公告)日:2006-03-30
申请号:DE60112150
申请日:2001-03-02
Applicant: UNITED TECHNOLOGIES CORP
Inventor: REY NANCY M , MILLER ROBIN MIHEKUN , TILLMAN THOMAS G , RUKUS ROBERT M , KETTLE JOHN L , DUNPHY JAMES R , CHAUDHRY ZAFFIR A , PEARSON DAVID D , DREITLEIN KENNETH C , LOFFREDO CONSTANTINO V , WYNOSKY THOMAS A
Abstract: A gas turbine engine (10) includes a variable area nozzle (30) having a plurality of flaps (38). The flaps (38) are actuated by a plurality of actuating mechanisms (40) driven by shape memory alloy (SMA) actuators (68) to vary fan exist nozzle area (36). The SMA actuator (68) has a deformed shape in its martensitic state and a parent shape in its austenitic state. The SMA actuator (68) is heated to transform from martensitic state to austenitic state generating a force output to actuate the flaps (38). The variable area nozzle (30) also includes a plurality of return mechanisms (42) deforming the SMA actuator (68) when the SMA actuator (68) is in its martensitic state.
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公开(公告)号:DE60111095T2
公开(公告)日:2005-10-27
申请号:DE60111095
申请日:2001-03-02
Applicant: UNITED TECHNOLOGIES CORP HARTF
Inventor: REY NANCY M , RUKUS ROBERT M , MILLER ROBIN MIHEKUN , KETTLE JOHN L , TILLMAN THOMAS G
Abstract: A self contained shape memory alloy (SMA) mechanism (50) is presented comprising a first anchor (52) and a second anchor (54) with a SMA actuator (56) and a return member (58) disposed therebetween. The SMA actuator (56) is a SMA bundle formed of single wires. The return member (58) is a linear spring surrounding the SMA actuator (56). Each mechanism (50) also includes a heating means. In operation, with the SMA actuator (56) in a martensitic state, the spring (58) of the mechanism (50) stretches the SMA actuator (56). When the SMA actuator (56) is heated to achieve its austenitic state, the force of the SMA actuator overcomes the force of the spring and pulls the anchors (52,54) thereby actuating at least one of the anchors (52,54). One major benefit of the mechanisms (50) is the ability to repeatably generate high active force in a compact package.
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公开(公告)号:DE60111095D1
公开(公告)日:2005-07-07
申请号:DE60111095
申请日:2001-03-02
Applicant: UNITED TECHNOLOGIES CORP HARTF
Inventor: REY NANCY M , RUKUS ROBERT M , MILLER ROBIN MIHEKUN , KETTLE JOHN L , TILLMAN THOMAS G
Abstract: A self contained shape memory alloy (SMA) mechanism (50) is presented comprising a first anchor (52) and a second anchor (54) with a SMA actuator (56) and a return member (58) disposed therebetween. The SMA actuator (56) is a SMA bundle formed of single wires. The return member (58) is a linear spring surrounding the SMA actuator (56). Each mechanism (50) also includes a heating means. In operation, with the SMA actuator (56) in a martensitic state, the spring (58) of the mechanism (50) stretches the SMA actuator (56). When the SMA actuator (56) is heated to achieve its austenitic state, the force of the SMA actuator overcomes the force of the spring and pulls the anchors (52,54) thereby actuating at least one of the anchors (52,54). One major benefit of the mechanisms (50) is the ability to repeatably generate high active force in a compact package.
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公开(公告)号:DK0866991T3
公开(公告)日:2000-01-17
申请号:DK96942153
申请日:1996-12-09
Applicant: UNITED TECHNOLOGIES CORP
Inventor: DUNPHY JAMES R , RUKUS ROBERT M , HA JONG-MIN
IPC: G02B6/44
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