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1.发明申请公开(公告)号：US20190193863A1
公开(公告)日：2019-06-27
申请号：US16301969
申请日：2017-09-25
发明人： Mohammadmahdi ABDOLLAHZADEHSANGROUDI , Jose Carlos PASCOA MARQUES , Frederico Miguel FREIRE RODRIGUES
CPC分类号： B64D15/22 , B64C23/005 , B64C23/04 , B64C2230/12 , B64D15/12 , B64D15/20 , H05B1/0236 , H05B6/62 , H05B2214/02 , H05H1/2406 , H05H2001/2412
摘要： The present invention relates to an ice detection/protection and flow control system based on printing of dielectric barrier discharge sliding plasma actuators. This invention has advantages such as: reduced weight, low maintenance cost, no environmental impact, fully electric operation and combination of functionalities (ice detection, deicing, anti-icing and flow control).The system comprises the following components: exposed AC electrode (1), dielectric layer (2), embedded electrode (3), sliding/nanosecond electrode (4), ground plane (5), AC power supply (6), DC power supply (7), nanosecond range pulse generator (8), monitoring capacitor (9), high voltage probe (10), control module (11), temperature sensor (12), control signal input module (13) and monitoring system (14). The system senses ice formation and generates extensive surface heating to prevent ice accumulation.
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公开(公告)号：US20190186360A1
公开(公告)日：2019-06-20
申请号：US16211360
申请日：2018-12-06
申请人： ROLLS-ROYCE plc
发明人： Benjamin J. SELLERS
CPC分类号： F02C7/057 , B64D15/12 , B64D27/10 , B64D31/00 , B64D2221/00 , B64F5/60 , F01D15/10 , F01D25/02 , F02C7/047 , F02C7/32 , F02C9/00 , F05D2220/76 , F05D2270/101 , F05D2270/309 , F05D2270/335
摘要： A method of controlling electrical power supplied to a component of a vehicle, the method comprising: receiving a signal comprising information associated with an operating condition of a gas turbine engine; determining whether a parameter exceeds a predetermined threshold value using the information in the received signal; and controlling a reduction in electrical power supplied to a component of a vehicle from a generator of the gas turbine engine if the parameter exceeds the predetermined threshold value.
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公开(公告)号：US20190006840A1
公开(公告)日：2019-01-03
申请号：US16107169
申请日：2018-08-21
CPC分类号： H02H9/02 , B64C1/1476 , B64D15/12 , H05B1/0236 , H05B3/86 , H05B2203/016 , H05B2203/035
摘要： A system for monitoring performance of an aircraft windshield includes a sensor comprising a sensory contact and an evaluation unit. The sensory contact is in physical contact with one or more components of the windshield, and generates a signal representative of the performance of the component(s) of the windshield. An electrical connector is secured to the surface of the windshield facing the interior of the aircraft. The signal from the sensory contact passes through the connector to the evaluation unit. The evaluation unit acts on the signal to determine the performance of the component(s) of the windshield, wherein the evaluation unit is spaced from and out of physical contact with the windshield and the electrical connector, and is in electrical contact with the electrical connector.
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公开(公告)号：US20180332666A1
公开(公告)日：2018-11-15
申请号：US15830799
申请日：2017-12-04
发明人： Seth S. Kessler , Ajay Raghavan , Brian L. Wardle
IPC分类号： H05B3/14 , H01B1/02 , B64D15/12 , B64D15/20 , G01N25/00 , G01N25/72 , C08K3/04 , B82Y99/00 , B64D45/00 , B64C1/00
CPC分类号： H05B3/145 , B64C2001/0072 , B64D15/12 , B64D15/20 , B64D2045/0085 , B82Y99/00 , C08K3/04 , C08K3/041 , G01N25/00 , G01N25/72 , H01B1/02 , H05B2203/003 , H05B2203/021 , H05B2214/02 , H05B2214/04 , Y02T50/43 , Y10S977/742
摘要： Various applications for structured CNT-engineered materials are disclosed herein. In one application, systems are disclosed, wherein a structured CNT-engineered material forms at least part of an object capable of providing its own structural feedback. In another application, systems are disclosed, wherein a structured CNT-engineered material forms at least part of an object capable of generating heat. In yet another application, systems are disclosed, wherein a structured CNT-engineered material forms at least part of an object capable of functioning as an antenna, for example, for receiving, transmitting, absorbing and/or dissipating a signal. In still another application, systems are disclosed, wherein a structured CNT-engineered material forms at least part of an object capable of serving as a conduit for thermal or electrical energy.
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公开(公告)号：US20180327100A1
公开(公告)日：2018-11-15
申请号：US15594360
申请日：2017-05-12
发明人： Gary S. Froman
CPC分类号： B64D15/12 , B64C11/20 , B64C29/0033 , B64D15/20 , H05B1/0236 , H05B3/34 , H05B2214/02
摘要： In one embodiment, a system may comprise an electro-thermal heating element and a controller. The electro-thermal heating element may be configured to heat a structure, and the controller may be configured to: identify a target temperature for the structure; identify a target rate of temperature change for the structure; identify a target voltage for heating the structure at the target rate of temperature change; and apply the target voltage to the electro-thermal heating element.
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公开(公告)号：US10035603B2
公开(公告)日：2018-07-31
申请号：US15221170
申请日：2016-07-27
申请人： THALES
发明人： Claude Sarno , Romain Hodot
IPC分类号： B33Y50/02 , B33Y80/00 , B64D33/08 , F28D21/00 , B64D15/06 , B64D15/12 , B64D43/02 , G01P5/165 , F28D15/02 , B33Y10/00 , G01F1/46
CPC分类号： B64D15/06 , B33Y10/00 , B33Y50/02 , B33Y80/00 , B64D15/12 , B64D33/08 , B64D43/02 , F28D15/0266 , F28D2021/0021 , G01F1/46 , G01P5/165
摘要： An aircraft provided with at least one piece of aeronautic equipment, the equipment (25) including a part intended to be arranged at a skin (27) of the aircraft and elements for heating the part, characterized in that the heating elements include a thermodynamic loop including a closed circuit in which a heat transfer fluid circulates, the closed circuit including an evaporator (14) associated with functional elements (70) of the aircraft forming a heat source giving off heat during their operation and a zone in which a condensation of the heat transfer fluid can occur in the appendage to heat it, and in that outside the evaporator, the circuit in which the fluid circulates is formed by a tubular channel with an empty section.
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公开(公告)号：US20180162077A1
公开(公告)日：2018-06-14
申请号：US15373371
申请日：2016-12-08
申请人： Goodrich Corporation
发明人： Jin Hu , Galdemir Cezar Botura , Casey Slane , Nathaniel Ching
IPC分类号： B29C71/00
CPC分类号： B29C71/0072 , B29C35/0272 , B29C71/02 , B29C2035/0211 , B29K2105/167 , B29K2105/18 , B64D15/12 , C08J7/08 , C08J2300/22 , H05B3/145 , H05B3/36 , H05B2214/04 , B29C71/0081
摘要： A method for reducing the resistivity of a thermoplastic film containing carbon nanotubes includes connecting an electric power supply to the thermoplastic film containing carbon nanotubes and passing electric current through the thermoplastic film containing carbon nanotubes to heat the thermoplastic film to an elevated temperature and align carbon nanotubes within the thermoplastic film. The thermoplastic film is solid at room temperature.
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公开(公告)号：US20180160482A1
公开(公告)日：2018-06-07
申请号：US15368271
申请日：2016-12-02
申请人： Goodrich Corporation
发明人： Brad Hartzler , Tommy M. Wilson, JR. , Galdemir Cezar Botura , Wenping Zhao , Zaffir A. Chaudhry
IPC分类号： H05B3/14 , B05D7/00 , B05D7/02 , B05D3/00 , B05D1/02 , B05D1/38 , B05D1/32 , H05B3/16 , H05B3/18 , B64D15/12
CPC分类号： H05B3/145 , B05D1/02 , B05D1/32 , B05D1/38 , B05D3/007 , B05D7/02 , B05D7/52 , B64D15/12 , B82Y30/00 , B82Y40/00 , C01B32/168 , C01B2202/22 , C01B2202/24 , H05B3/16 , H05B3/18 , H05B3/34 , H05B2203/013 , H05B2214/02 , H05B2214/04 , Y10S977/742 , Y10S977/842 , Y10S977/932
摘要： A method for creating a carbon nanotube heater assembly includes creating a carbon nanotube heater with varying resistances and attaching the carbon nanotube heater to both carrier and encapsulating materials. Creating the carbon nanotube heater with varying resistances is accomplished by applying a carbon nanotube mixture to a substrate, adjusting the thickness or width of the carbon nanotube mixture, and drying the nanotube mixture.
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公开(公告)号：US09957034B2
公开(公告)日：2018-05-01
申请号：US14977941
申请日：2015-12-22
CPC分类号： B64C1/1492 , B64C1/14 , B64C1/1476 , B64D15/12 , B64D45/02 , H05B3/84 , H05B2203/002 , H05B2203/013
摘要： The present invention provides a windshield of an aircraft, including a plurality of conductive members that are disposed along an in-plane direction of the windshield, and are wire-connected together, wherein the plurality of conductive members are heaters that generate heat when supplied with an alternating current, and the conductive members are wire-connected such that induced currents induced in the respective conductive members by a magnetic field in association with a lightning current are circulated between the conductive members.
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公开(公告)号：US20180093785A1
公开(公告)日：2018-04-05
申请号：US15284052
申请日：2016-10-03
申请人： ROHR, INC.
发明人： Keith T. Brown
CPC分类号： F02C7/047 , B64D15/12 , B64D2033/0233 , B64F5/40 , F01D25/02 , F05D2230/80 , F05D2270/54
摘要： An ice protection system for an aircraft may comprise an electric heater embedded within a composite aircraft component. In the event of malfunction of the embedded heater, a secondary heater may be attached to an interior surface of the composite aircraft component. The wiring may be detached from the embedded heater and attached to the secondary heater. The secondary heater may be used to provide ice protection to the composite aircraft component.
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