专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明公开

EP3422805A1 PROCEDE DE FABRICATION D'UN EQUIPEMENT TOURNANT DE VOILURE TOURNANTE MUNI D'UN DEGIVREUR, LEDIT EQUIPEMENT TOURNANT, ET UN DRONE MUNI DUDIT EQUIPEMENT TOURNANT 有权
公开(公告)号：EP3422805A1
公开(公告)日：2019-01-02
申请号：EP18172703.3
申请日：2018-05-16
申请人： Airbus Helicopters
发明人： GIBERT, Gauthier , IMBERT, Nicolas
IPC分类号： H05B3/26
CPC分类号： B64D15/12 , B64C27/32 , B64C39/024 , B64C2201/024 , H05B3/26 , H05B2203/013 , H05B2214/02 , H05K3/0026 , H05K3/18
摘要： La présente invention concerne un équipement tournant de drone muni d'un ensemble tournant (10) qui comporte au moins une pale (11). L'ensemble tournant (10) comporte au moins un sillon (20) qui s'étend sur ladite enveloppe (13) d'une première extrémité (21) vers une deuxième extrémité (22), ledit au moins un sillon (20) étant au moins ménagé sur ladite pale (11), ledit au moins un sillon (20) présentant au moins un changement de direction (23) sur ladite pale (11), ledit ensemble tournant (10) comprenant au moins un dégivreur (30) muni d'une piste électriquement conductrice (31) qui s'étend dans ledit au moins un sillon (20), ladite piste électriquement conductrice (31) s'étendant d'une première borne (32) jusqu'à une deuxième borne (33), la première borne (32) étant présente dans la première extrémité (21), la deuxième borne (33) étant présente dans la deuxième extrémité (22), ledit dégivreur (30) comprenant une couche de protection recouvrant ladite piste électriquement conductrice (31).

2. 发明公开

EP3419381A2 ELECTROMECHANICAL ICE PROTECTION SYSTEMS WITH CARBON ADDITIVE LOADED THERMOPLASTIC HEATING ELEMENTS 审中-公开
公开(公告)号：EP3419381A2
公开(公告)日：2018-12-26
申请号：EP18179102.1
申请日：2018-06-21
申请人： Goodrich Corporation
发明人： HU, Jin , BOTURA, Galdemir Cezar , SLANE, Casey
IPC分类号： H05B3/28 , H05B3/36 , H05B3/14 , B64D15/12
CPC分类号： H05B3/286 , B64D15/12 , H05B3/146 , H05B3/36 , H05B2203/013 , H05B2203/017 , H05B2203/037 , H05B2214/02 , H05B2214/04
摘要： Pre-fabric, flexible and thermally stable plastic sheets (12) are loaded with carbon additives (14) such as carbon nanotubes (CNTs), graphene, nano carbon fibers, graphite powders, or other carbon allotropes to adjust the resistivity of the sheets as desired for ice protection. These sheets (12) are both conformable to desired surfaces and prevent the carbon debris migration issues in traditional CNT heaters.

3. 发明授权

EP3231252B1 DEICING OF STRUCTURES USING MICROWAWES GENERATED BY TRANSISTORS 有权
公开(公告)号：EP3231252B1
公开(公告)日：2018-12-05
申请号：EP15812994.0
申请日：2015-12-08
申请人： Icesolution AS
发明人： KARTHÄUSER, Joachim
IPC分类号： H05B6/64 , B64D15/00 , H05B6/68 , H05B6/80
CPC分类号： H05B6/80 , B64D15/12 , H05B6/6491 , H05B6/686 , H05B2206/044 , H05B2214/02 , H05B2214/04
摘要： This invention concerns a novel method to deice structures such as blades of wind power turbines, wings of airplanes and other structures prone to ice accretion including power cables, marine structures and the like. Essentially, solid state radio frequency (RF) power transistors are used to generate microwaves which are absorbed by a microwave-absorbing material. The heat generated by microwave absorption is used to shed ice from affected structures. Various embodiments and associated advantages are disclosed.

4. 发明授权

EP3032153B1 HEATED VALVE 有权
公开(公告)号：EP3032153B1
公开(公告)日：2018-11-14
申请号：EP15195997.0
申请日：2015-11-24
申请人： Goodrich Corporation
发明人： FAHRNER, Alan J. , PUDOKA, Rick
IPC分类号： F16K49/00 , B64D15/12 , B64D15/04 , B64D13/06
CPC分类号： F16K49/002 , B64D15/04 , B64D15/12 , B64D2013/0607 , Y10T137/6606
摘要： A valve (10; 36) includes a body (12) with an inlet (14; 48) at a first end of the body (12), and an outlet (16; 50) at a second end of the body (12). A first electrically resistive heating element (28; 52) is located in the inlet (14; 48) and heats a first fluid source (24) to a temperature above 0 degrees C. A second electrically resistive heating element (30; 54) is located in the outlet (16; 50) and heats a second fluid source (26) to a temperature above 0 degrees C.

5. 发明公开

EP3342710A1 STRUCTURE POUR ENSEMBLE PROPULSIF D'AERONEF, SYSTEME ET ENSEMBLE PROPULSIF ASSOCIES 无效
公开(公告)号：EP3342710A1
公开(公告)日：2018-07-04
申请号：EP17206791.0
申请日：2017-12-12
申请人： Airbus Operations S.A.S.
发明人： MENAY, Hassan , RAVISE, Florian
IPC分类号： B64D15/12 , F02C7/045 , F02C7/047 , B64D33/02
CPC分类号： B64D15/12 , B32B2305/18 , B32B2307/202 , B32B2605/18 , B64D33/02 , B64D2033/0206 , B64D2033/0233 , B64D2033/0273 , F01D25/005 , F02C7/045 , F02C7/047 , F05D2300/603 , Y02T50/672
摘要： L'invention concerne une structure (16) en matériau composite pour ensemble propulsif d'aéronef, la structure (16) comportant au moins une zone thermique (24) propre à recevoir de l'énergie électrique, la structure (16) étant caractérisée en ce que chaque zone thermique (24) comporte au moins une pellicule résistive (26) comprenant un film interne (30) réalisé dans un matériau thermoplastique rendu conducteur par inclusion de nanotubes de carbone, de sorte que chaque pellicule résistive (26) est propre à dissiper, par effet Joule, au moins une partie l'énergie électrique reçue par la zone thermique (24), un pli intermédiaire (28) réalisé dans un tissu satin imprégné d'un matériau thermoplastique, et un film externe (32) réalisé dans un matériau thermoplastique.

6. 发明公开

EP3333081A1 ICE PROTECTION SYSTEM FOR A MULTI-SEGMENT AIRCRAFT COMPONENT 审中-公开
公开(公告)号：EP3333081A1
公开(公告)日：2018-06-13
申请号：EP18151771.5
申请日：2008-12-17
申请人： Goodrich Corporation , Rohr, Inc.
发明人： ZECCA, Joseph Christopher , BOTURA, Galdemir Cezar , BURKETT, Brian Bobby , HUBERT, Claude Marc , LAYLAND, Michael John , OLSON, Timothy Robert , ROMAN, James Michael
IPC分类号： B64D15/12 , B64D33/02 , F02C7/047 , F02C7/045 , H05B3/28 , B64D15/14 , H05B3/06
CPC分类号： B64D15/12 , B64D33/02 , B64D2033/0206 , B64D2033/0233 , F02C7/045 , F02C7/047 , F05D2250/132 , H05B3/06 , Y02T50/672 , Y10T29/49826
摘要： An aircraft component (200) is disclosed which comprises a first segment (110) comprising a first exterior surface, a first end, and a first electric heater element (227) having a first edge proximate to the first end; a second segment (112) comprising a second exterior surface, a second end, and a second electric heater element (223) having a second edge proximate to the second end, wherein the second end is joined to the first end such that the first external surface and the second external surface combine to form at least a portion of a substantially continuous leading edge surface; a first bus bar connected to the first edge of the first heater element; and a second bus bar connected to the second edge of the second heater element; wherein the first and second bus bars (230) are disposed between the first end and the second end when the first end is joined to the second end.

7. 发明公开

EP3297394A3 NANO ALUMINA FABRIC PROTECTION PLY FOR DE-ICERS 有权
标题翻译：纳米氧化铝织物保护膜适用于DE-ICERS
公开(公告)号：EP3297394A3
公开(公告)日：2018-03-28
申请号：EP17192201.6
申请日：2017-09-20
申请人： Goodrich Corporation
发明人： HU, Jin , BOTURA, Galdemir Cezar
IPC分类号： H05B3/14 , B64D15/02 , H05B3/34
CPC分类号： H05B3/34 , B64D15/02 , B64D15/12 , H05B3/14 , H05B2203/017 , H05B2214/02 , H05B2214/04
摘要： A nano alumina fabric protects heaters used for de-icing aircraft or other vehicles. This allows heaters to withstand mechanical foreign object damage (FOD), is environmentally safe, and is a cost-efficient alternative to other protection fabrics. A heating assembly (10A) includes a nano alumica fabric (20), a first adhesive (22), a heating element (24), wherein the nano alumina fabric (20) is attached to the heating element (24) by the first adhesive (22), a second adhesive (26), and a glass pre-preg fabric (28), wherein the glass pre-preg fabric (28) is attached to the heating element (24) by the second adhesive (26) on a side of the heating element (24) opposite the nano alumina fabric (20).
摘要翻译：纳米氧化铝织物可以保护用于除冰飞机或其他车辆的加热器。这使加热器能够承受机械外物损坏（FOD），是环保的，并且是其他防护织物的经济高效替代品。一种加热组件（10A），包括纳米氧化铝织物（20），第一粘合剂（22），加热元件（24），其中纳米氧化铝织物（20）通过第一粘合剂附着到加热元件其特征在于，所述玻璃预浸织物（28）通过所述第二粘合剂（26）连接到所述加热元件（24）上，所述第二粘合剂（26）和所述玻璃预浸织物（28）加热元件（24）的与纳米氧化铝织物（20）相对的一侧。

8. 发明公开

EP3297395A2 THERMALLY CONDUCTIVE, ELECTRICALLY INSULATING PROTECTION LAYER FOR DE-ICING HEATERS 有权转让
标题翻译：用于除冰加热器的导热绝缘保护层
公开(公告)号：EP3297395A2
公开(公告)日：2018-03-21
申请号：EP17192225.5
申请日：2017-09-20
申请人： Goodrich Corporation
发明人： HU, Jin , BOTURA, Galdemir Cezar
IPC分类号： H05B3/14 , B64D15/12 , H05B3/34
CPC分类号： H05B3/342 , B32B5/02 , B32B7/12 , B32B2255/02 , B32B2260/023 , B32B2260/046 , B32B2262/101 , B32B2262/105 , B32B2262/106 , B32B2307/206 , B32B2307/302 , B32B2457/00 , B32B2605/18 , B64D15/12 , B64D45/00 , H05B1/0236 , H05B3/14 , H05B3/34 , H05B2203/015 , H05B2203/017 , H05B2214/02 , H05B2214/04
摘要： Disclosed is the use of a boron nitride nanotube (BNNT) fabric for protection of nano-carbon heaters used for de-icing aircrafts or other vehicles. This allows the heaters to be resistant to hail, bird, and other mechanical striking damages, and can be applied to parts of aircraft that require acoustic protection. The heating assembly comprises a boron nitride nanotube fabric (20); a first adhesive (22); a heating element (24), wherein the boron nitride nanotube fabric (20) is attached to the heating element (24) by the first adhesive (22); a second adhesive (26); a glass pre-preg fabric (28), wherein the glass pre-preg fabric (28) is attached to the heating element (24) by the second adhesive (26) on a side of the heating element (24) opposite the boron nitride nanotube fabric (20).
摘要翻译：公开了使用氮化硼纳米管（BNNT）织物来保护用于除冰飞机或其他车辆的纳米碳加热器。这使得加热器可以抵抗冰雹，鸟类和其他机械撞击损伤，并且可以应用于需要声学保护的飞机部件。该加热组件包括氮化硼纳米管织物（20）; 第一粘合剂（22）; 加热元件（24），其中所述氮化硼纳米管织物（20）通过所述第一粘合剂（22）附接到所述加热元件（24）。第二粘合剂（26）; （28），其中玻璃预浸织物（28）通过第二粘合剂（26）在加热元件（24）的与氮化硼相对的一侧上附着于加热元件（24）纳米管织物（20）。

9. 发明公开

EP3223671A1 THERMALLY SPRAYED RESISTIVE HEATERS AND USES THEREOF 审中-公开
标题翻译：热喷涂电阻加热器及其用途
公开(公告)号：EP3223671A1
公开(公告)日：2017-10-04
申请号：EP15804617.7
申请日：2015-11-25
申请人： Regal Ware, Inc.
发明人： KAZANAS, Athinodoros Chris , MARCOUX, Pierre , ABBOTT, Richard C.
IPC分类号： A47J37/06 , C23C4/10 , C23C4/073
CPC分类号： A47J37/0676 , A47J37/06 , B64D15/12 , C23C4/073 , C23C4/10 , H05B3/0095 , H05B3/06 , H05B3/08 , H05B3/141 , H05B3/143 , H05B3/262 , H05B3/265 , H05B3/68 , H05B3/84 , H05B3/845 , H05B2203/013 , H05B2203/017 , H05B2203/019 , H05B2203/026 , H05B2203/029 , H05B2203/036 , H05B2214/02
摘要： A heater is provided having at least one thermally sprayed resistive heating layer, the resistive heating layer comprising a first metallic component that is electrically conductive and capable of reacting with a gas to form one or more carbide, oxide, nitride, and boride derivative; one or more oxide, nitride, carbide, and boride derivative of the first metallic component that is electrically insulating; and a third component capable of stabilizing the resistivity of the resistive heating layer. In some embodiments, the third component is capable of pinning the grain boundaries of the first metallic component deposited in the resistive heating layer and/or altering the structure of aluminum oxide grains deposited in the resistive heating layer.
摘要翻译：提供具有至少一个热喷涂电阻加热层的加热器，所述电阻加热层包含导电的且能够与气体反应以形成一种或多种碳化物，氧化物，氮化物和硼化物衍生物的第一金属组分; 所述第一金属部件的一种或多种电绝缘的氧化物，氮化物，碳化物和硼化物衍生物; 以及能够稳定电阻加热层的电阻率的第三部件。在一些实施例中，第三组件能够钉扎沉积在电阻加热层中的第一金属组分的晶界和/或改变沉积在电阻加热层中的氧化铝晶粒的结构。

10. 发明公开

EP3187882A1 APPARATUS AND METHOD FOR ANTI-ICING OF SPEED MEASUREMENT PROBES 有权
标题翻译：用于抗速度测量探针的装置和方法
公开(公告)号：EP3187882A1
公开(公告)日：2017-07-05
申请号：EP16194073.9
申请日：2016-10-17
申请人： The Boeing Company
发明人： DICHEK, Daniel Jonathan Gunnar , KHOZIKOV, Vyacheslav , MORROW, Jonathan
IPC分类号： G01P5/165 , B64D15/12
CPC分类号： B64D15/12 , B64D43/02 , G01P5/165
摘要： A de-icing system is provided that includes a member, a coil, and a power supply. The member includes an anti-icing portion. The coil is inductively coupled to the anti-icing portion of the member. The power supply is coupled to the coil, and is configured to provide voltage to the coil. The coil emits electromagnetic energy responsive to power supplied by the power supply. Responsive to the electromagnetic energy, eddy currents are generated in the anti-icing portion that provide heating of the anti-icing portion.
摘要翻译：提供了除冰系统，其包括构件，线圈和电源。该部件包括防冰部分。线圈感应耦合到部件的防冰部分。电源耦合到线圈，并被配置为向线圈提供电压。线圈响应于由电源供应的电力而发射电磁能量。响应于电磁能量，在抗冰部分中产生涡电流，其提供防冰部分的加热。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式