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1. 发明专利

JP2012062049A Propeller blades having ice-phobic coating 有权
标题翻译：具有冰晶涂层的螺旋叶片
公开(公告)号：JP2012062049A
公开(公告)日：2012-03-29
申请号：JP2011200363
申请日：2011-09-14
申请人： Ge Aviation Systems Ltd , ジーイー・アビエイション・システムズ・リミテッドGe Aviation Systems Limited
发明人： TOWKAN MICHAEL FEDOR
IPC分类号： B64C11/20 , B64D15/00
CPC分类号： B64C11/205 , B64D15/00
摘要： PROBLEM TO BE SOLVED: To provide a propeller blade having ice-phobic coating which is a passive system capable of improving reliability and maintainability and furthermore reducing both the initial acquirement cost and the maintenance cost during procession.SOLUTION: The propeller blade 1 rotating about a hub assembly has a coating 6 comprising an ice-phobic material disposed thereon at least along a leading edge 7. The coating 6 extends along the blade 1 from a radially inner region to a radially outer region, wherein the radially outer region is disposed between the blade root and the blade tip at a position where rotational forces on the blade 1 are sufficient, in use, to cause removal of ice from the uncoated blade 1.
摘要翻译：要解决的问题：提供具有防冰涂层的螺旋桨叶片，其是能够提高可靠性和可维护性的被动系统，并且进一步降低了游行过程中的初始获取成本和维护成本。解决方案：围绕轮毂组件旋转的螺旋桨叶片1具有至少沿着前缘7设置在其上的防恐石材料的涂层6。涂层6沿着刀片1从径向内部区域延伸到径向外部区域，其中径向外部区域设置在叶片根部和叶片尖端之间，其在叶片1上的旋转力足以在使用中从未涂覆的叶片1移除冰的位置。版权所有：（C）2012，JPO＆INPIT

2. 发明专利

JP3364911B2 Fan for aircraft engine 失效
公开(公告)号：JP3364911B2
公开(公告)日：2003-01-08
申请号：JP226994
申请日：1994-01-14
申请人：石川島播磨重工業株式会社
发明人：良也中村 , 淳清水 , 聡一野口
IPC分类号： B64C11/20 , F02C7/00 , F02K3/06

3. 发明专利

JPH1199994A BLADE WITH SWEEP-BACK WING END FOR ROTOR OF AIRCRAFT 失效
公开(公告)号：JPH1199994A
公开(公告)日：1999-04-13
申请号：JP31851197
申请日：1997-11-19
申请人： EUROCOPTER FR , ONERA (OFF NAT AEROSPATIALE)
发明人： TOULMAY FRANCOIS VALENTIN G , ZIBI JOELLE MARGUERITE
IPC分类号： B64C11/20 , B64C27/46 , B64C27/467
摘要： PROBLEM TO BE SOLVED: To provide a blade with sweep-back wing end for the rotor of an aircraft designed so as to be optimum for ensuring best performance, optimum for ensuring high speed flying in particular. SOLUTION: A blade with sweep-back wing end for the rotor of an aircraft is formed with a continuous base cross section. In this constitution, fractionation of the blade 1 to different areas, the length L of a chord, deflection Y'f from a pressure center pitch changing shaft and the relative thickness of each base cross section are optimized for high speed flying.

4. 发明专利

JPH06144382A LEADING EDGE PROTECTING STRUCTURE FOR AIRCRAFT WING 失效
公开(公告)号：JPH06144382A
公开(公告)日：1994-05-24
申请号：JP29579692
申请日：1992-11-05
申请人： KAWASAKI HEAVY IND LTD
发明人： KAKINUMA ASAO , KAWAGUCHI HITOSHI , MIYABE HIDEKI
IPC分类号： B64C3/26 , B64C11/20 , B64C27/46 , B64C27/467
摘要： PURPOSE:To provide a leading edge protecting member made of nonmetal excellent in wearing against collision or the like with a rain drop in little apprehension of damage without determining a life of a wing total unit by wearing the protecting member, as the wing leading eve protecting member. CONSTITUTION:A protecting member 3 is constituted to be manufactured by roll molding by a polymer alloy material, so that a roll direction of the molding agrees with a direction orthogonal to the lengthwise direction of a wing 1, and to be adhesively mounted on a wing leading end part by a rubber bonding agent.

5. 发明专利

JPH0427079B2 失效
公开(公告)号：JPH0427079B2
公开(公告)日：1992-05-08
申请号：JP7257287
申请日：1987-03-26
申请人： KAWASAKI HEAVY IND LTD
发明人： KAKINUMA ASAO , BANDO SHUNICHI
IPC分类号： B64C3/26 , B64C11/20 , B64C27/46 , B64C27/473

6. 发明专利

JPH0249627B2 失效
公开(公告)号：JPH0249627B2
公开(公告)日：1990-10-30
申请号：JP9139484
申请日：1984-05-08
申请人： KAWASAKI HEAVY IND LTD
发明人： BANDO SHUNICHI , KAKINUMA ASAO
IPC分类号： B32B3/18 , B29C43/10 , B29C43/18 , B29K105/06 , B29L31/30 , B32B3/28 , B64C3/20 , B64C11/20 , B64C11/26

7. 发明专利

JPS63258298A ADJUSTABLE BLAST BLADE 失效
公开(公告)号：JPS63258298A
公开(公告)日：1988-10-25
申请号：JP7218588
申请日：1988-03-28
申请人： MTU MUENCHEN GMBH
发明人： JIIKUFURIITO JIKORUSUKI
IPC分类号： B64C11/20 , B64C11/26 , F01D5/28 , F04D29/36 , F04D29/38

9. 发明专利

JP5232174B2 Retention of the propeller blade 有权
公开(公告)号：JP5232174B2
公开(公告)日：2013-07-10
申请号：JP2009548729
申请日：2007-11-01
申请人：ジーイー・アビエイション・ユーケー
发明人：ペントニー，ケヴィン
IPC分类号： B64C11/20
CPC分类号： B64C11/06 , Y10T29/49332 , Y10T29/49336

10. 发明专利

JP2011179488A Rotor 审中-公开
标题翻译：转子
公开(公告)号：JP2011179488A
公开(公告)日：2011-09-15
申请号：JP2010089005
申请日：2010-03-01
申请人： Hiroo Ichikawa , 博夫市川
发明人： ICHIKAWA HIROO
IPC分类号： F03D1/06 , B64C11/20 , B64C27/473
CPC分类号： Y02E10/721 , Y02P70/523
摘要： PROBLEM TO BE SOLVED: To reduce minus drag by acting plus drag/lift on a rotor to the maximum even under a low and middle wind speed condition; to reduce the weight of the whole of the rotor; to provide a stable structure of a wing and the rotor while achieving increase of the plus drag/lift and the reduction of the weight at the same time; and to reduce the material cost of a wing, a rotor and a supporting material, a manufacturing cost, the total equipment cost, a transportation cost, and a maintenance cost. SOLUTION: At least one closed wing constituted by a substantially ring-shaped blade 1 having a bent portion on an outer side of a surface in a pitch length direction and a small curve cross section on an outer side of a surface in a pitch width direction on the prescribed position, is provided on a rotating shaft 3 through a hub 2. COPYRIGHT: (C)2011,JPO&INPIT
摘要翻译：要解决的问题：即使在中低风速条件下，通过将转子上的加减速/减速减至最大也可减少减阻; 减轻整个转子的重量; 提供机翼和转子的稳定结构，同时实现加减速和同时减轻重量的增加; 并减少机翼，转子和支撑材料的材料成本，制造成本，总设备成本，运输成本和维护成本。解决方案：至少一个由基本上环形的叶片1构成的封闭翼片，其具有在俯仰长度方向上的表面的外侧上的弯曲部分和在其中的表面的外侧上的小曲线横截面在规定位置上的俯仰宽度方向通过轮毂2设置在旋转轴3上。版权所有（C）2011，JPO＆INPIT

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