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. 发明申请

WO2017123291A1 SEALS FOR ROTOR SYSTEM FAIRINGS 审中-公开
标题翻译：用于转子系统修补的密封件
公开(公告)号：WO2017123291A1
公开(公告)日：2017-07-20
申请号：PCT/US2016/055893
申请日：2016-10-07
申请人： SIKORSKY AIRCRAFT CORPORATION
发明人： HUNTER, David, H. , NUSSENBLATT, Eric, L. , EADIE, William, J. , BUTLER, Chris, P. , BASKIN, Bryan, K.
IPC分类号： B64C27/32 , B64C11/02 , B64C27/48
CPC分类号： B64C27/32 , B64C7/00 , B64C27/10
摘要： A fairing system, includes a hub fairing and a fixed fairing, such as a shaft fairing or a pylon fairing, both arranged about a rotation axis. A gap is defined between the hub fairing and the fixed fairing, and a seal assembly is axially interposed between the hub fairing and the fixed fairing. The fixed fairing and the hub fairing are both removably mounted to the seal assembly such that either or both of the fairings can be dismounted from the seal assembly without disturbing the seal assembly to provide access to components disposed within the fairing.
摘要翻译：整流装置包括一个轮毂整流罩和一个固定的整流罩，例如轴整流罩或挂架整流罩，它们均围绕旋转轴线布置。轮毂整流罩和固定整流罩之间限定有间隙，并且轴向插入轮毂整流罩和固定整流罩之间的密封组件。固定的整流罩和轮毂整流罩都可拆卸地安装到密封组件，使得整流罩中的任一个或两个均可从密封组件拆卸下来，而不会干扰密封组件以提供通往布置在整流罩内的部件的通路。

2. 发明申请

WO2016053408A1 ACOUSTIC SIGNATURE VARIATION OF AIRCRAFT UTILIZING A CLUTCH 审中-公开
标题翻译：使用离合器的飞机的声学签名变化
公开(公告)号：WO2016053408A1
公开(公告)日：2016-04-07
申请号：PCT/US2015/036354
申请日：2015-06-18
申请人： SIKORSKY AIRCRAFT CORPORATION
发明人： GARCIA, Todd, A. , EADIE, William, J. , STILLE, Brandon, L.
IPC分类号： B64C27/22
CPC分类号： B64C27/82 , B64C1/0009 , B64C7/00 , B64C13/04 , B64C13/18 , B64C13/50 , B64C13/503 , B64C19/00 , B64C27/001 , B64C27/006 , B64C27/008 , B64C27/08 , B64C27/10 , B64C27/12 , B64C27/14 , B64C27/16 , B64C27/32 , B64C27/322 , B64C27/33 , B64C27/467 , B64C27/473 , B64C27/48 , B64C27/51 , B64C27/52 , B64C27/54 , B64C27/57 , B64C27/78 , B64C27/80 , B64C2027/004 , B64C2027/8209 , B64C2027/8227 , B64C2027/8236 , B64C2027/8263 , B64C2027/8272 , B64C2027/8281 , B64C2201/024 , B64D35/06 , B64D39/00 , B64D39/06 , B64D45/02 , F02C9/28 , F05D2220/329 , F05D2270/021 , F16D13/52 , F16D13/72 , F16D13/74 , F16H37/02 , G05D1/0077 , G05D1/0202 , G05D1/0204 , G05D1/08 , G05D1/0816 , G05D1/0858 , G06F19/00
摘要： An aircraft is provided including an airframe, an extending tail, and a counter rotating coaxial main rotor assembly including an upper rotor assembly and a lower rotor assembly. A translational thrust system including a propeller is positioned at the extending tail. The translational thrust system provides translational thrust to the airframe. A drive system is configured to operate both the main rotor system and the translational thrust system. The drive system includes a clutch configured to selectively couple or decouple the propeller from the drive system.
摘要翻译：提供一种包括机身，延伸尾部和包括上转子组件和下转子组件的反转同轴主转子组件的飞行器。包括螺旋桨的平移推力系统位于延伸尾部。平移推力系统为机身提供平移推力。驱动系统被配置成操作主转子系统和平移推力系统。驱动系统包括被配置为选择性地将螺旋桨与驱动系统联接或分离的离合器。

3. 发明申请

WO2008018912A2 RADIO FREQUENCY EMITTING HOOK SYSTEM FOR A ROTARY-WING AIRCRAFT EXTERNAL LOAD HANDLING 审中-公开
标题翻译：用于旋转式飞机外部负载处理的无线电频率发射钩系统
公开(公告)号：WO2008018912A2
公开(公告)日：2008-02-14
申请号：PCT/US2007/002723
申请日：2007-01-31
申请人： SIKORSKY AIRCRAFT CORPORATION
发明人： EADIE, William, J. , SCOTT, Mark, W.
IPC分类号： B64D9/00
CPC分类号： B64D1/22 , B66C13/063 , B66C13/46
摘要： An aircraft load management system that determines the position of an aircraft cargo hook for display to an aircrew. The cargo hook positional information may alternatively or additionally be communicated directly to a flight control system and a winch control system to automate and coordinate flight control inputs with winch operation to actively position the cargo hook. Data transfer from the cargo through a data link system also provides the load management system with exact position of the cargo load connection points even prior to attachment of the cargo hook to the load. The load management system also includes anti-sway algorithms for active load stability inputs to the flight control system and to alter flight control laws and automatically compensate for CG. excursions.
摘要翻译：航空器负载管理系统，用于确定飞机货物挂钩的位置，以显示给机组人员。货钩位置信息可以替代地或附加地直接传达到飞行控制系统和绞盘控制系统，以通过绞车操作自动化和协调飞行控制输入，以主动定位货物吊钩。通过数据链接系统从货物的数据传输，即使在将货钩连接到负载之前，也可以使负载管理系统具有货物负载连接点的精确位置。负载管理系统还包括用于飞行控制系统的主动负载稳定性输入的反摆动算法，并改变飞行控制规律并自动补偿CG。游览。

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