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1. 发明公开

EP4393817A1 ENGINE-CARRYING FLIGHT DEVICE 审中-实审
公开(公告)号：EP4393817A1
公开(公告)日：2024-07-03
申请号：EP22861088.7
申请日：2022-08-02
申请人： Ishikawa Energy Research Co., Ltd.
发明人： ISHIKAWA Mitsuru , NAGASHIMA Hiroyuki
IPC分类号： B64C27/08 , B64C13/18 , B64C39/02 , B64D27/04 , B64D27/10 , B64D27/24
CPC分类号： Y02T50/60 , B64C39/02 , B64D27/24 , B64D27/10 , B64C13/18 , B64C27/08 , B64D27/04
摘要： An engine-carrying flight device capable of stably hovering is provided. The engine-carrying flight device 10 can fly in a hovering state in which an altitude is maintained and in an ascending/descending state in which the altitude is changed. The engine-carrying flight device 10 includes main rotors 14, sub-rotors 15, an engine 26; motors 21; and an arithmetic control unit 25. The main rotors 14 are rotated by drive force received from the engine 26, the sub-rotors 15 are rotated by drive force received from the motors 21, and the arithmetic control unit 25 causes a thrust generated by rotation of the main rotors 14 to be smaller than a thrust necessary for keeping the altitude constant, in the hovering state.

2. 发明公开

EP3261923A1 AIRFRAME-INTEGRATED PROPELLER-DRIVEN PROPULSION SYSTEMS 有权
标题翻译：机载飞机一体化螺旋桨驱动推进系统
公开(公告)号：EP3261923A1
公开(公告)日：2018-01-03
申请号：EP16710084.1
申请日：2016-02-19
申请人： Embraer S.A.
发明人： HIRANO, Helio , TRAPP, Luis Gustavo
IPC分类号： B64C5/02 , B64C5/06 , B64D27/04 , B64D27/10
CPC分类号： B64C11/46 , B64C5/02 , B64C5/06 , B64C23/005 , B64D27/04 , B64D27/10
摘要： Propeller-driven craft (e.g., aircraft) are provided with at least one propulsion system having at least one engine and at least one aerial tractor propeller which generates a propeller propwash airflow when driven by the engine. At least one airfoil is disposed in the propeller propwash airflow of the at least one aerial tractor propeller. The airfoil is contoured and oriented relative to a swirl rotation angle (ω) of the propeller propwash airflow in order to induce a forward force component on the craft in response to the propeller propwash airflow over the at least one airfoil, thus improving the craft's performance and/or reducing fuel consumption.

3. 发明授权

EP2571764B1 HYBRIDANTRIEB FÜR HUBSCHRAUBER 有权转让
标题翻译：混合动力驱动直升机
公开(公告)号：EP2571764B1
公开(公告)日：2017-04-12
申请号：EP11724574.6
申请日：2011-05-19
申请人： Airbus Defence and Space GmbH , AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： BOTTI, Jean , STUHLBERGER, Johannes , JÄNKER, Peter , KLÖPPEL, Valentin , NIESL, Georg
IPC分类号： B64D27/24 , B64D27/14 , B64D27/04
CPC分类号： B64D35/02 , B60L11/12 , B60L2200/10 , B64C27/04 , B64C27/14 , B64D27/04 , B64D27/24 , B64D2027/026 , Y02T10/646 , Y02T10/7077 , Y02T50/64 , Y10S903/903

4. 发明公开

EP3107807A1 FLUGGERÄT 审中-公开
公开(公告)号：EP3107807A1
公开(公告)日：2016-12-28
申请号：EP15704564.2
申请日：2015-02-17
申请人： IAT 21 Innovative Aeronautics Technologies GmbH
发明人： SCHWAIGER, Meinhard
IPC分类号： B64C3/38 , B64C3/56 , B64C29/00 , B64C39/00 , B64C39/02
CPC分类号： B64C29/0033 , B64C3/385 , B64C3/56 , B64C27/026 , B64C27/20 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/044 , B64C2201/102 , B64C2201/108 , B64C2201/162 , B64D27/04 , B64D27/24 , B64D2027/026 , B64D2211/00
摘要： The invention relates to an aircraft comprising a fuselage (1), a plurality of propeller units (3) that can pivot in relation to the fuselage (1), and wings (5) that can pivot at least partially in relation to the fuselage (1) and independently of the propeller units (3).
摘要翻译：本发明涉及一种飞机，其包括机身（1），可相对于机身（1）枢转的多个螺旋桨单元（3）和能够相对于机身至少部分地枢转的翼（5） 1）并且独立于螺旋桨单元（3）。

5. 发明公开

EP2815115A1 SYSTEM AND METHOD FOR ALERTING AND SUPPRESSION OF DETONATION AND/OR PRE IGNITION PHENOMENA IN INTERNAL COMBUSTION ENGINES BY MONITORING RPM FLUCTUATION 有权
标题翻译：方法为警告和爆炸和/或VORZÜNDUNGSPHÄNOMENEN在内燃机中的减少通过监测转速波动
公开(公告)号：EP2815115A1
公开(公告)日：2014-12-24
申请号：EP12868864.5
申请日：2012-12-04
申请人： Israel Aerospace Industries Ltd.
发明人： GRUMER, Bernard , LEVY, Nathan
IPC分类号： F02D41/22
CPC分类号： F02D41/22 , B64D27/04 , B64D31/00 , B64D31/06 , F02D35/02 , F02D35/024 , F02D35/027 , F02D37/02 , F02D41/0007 , F02D41/0097 , F02D41/1497 , F02D41/263 , F02D41/266 , F02D2200/1012 , F02P5/045 , F02P5/152 , G01M15/046 , G01M15/11 , Y02T10/144
摘要： An engine system with advance detection of detonation and / or pre ignition, the system comprising an engine, operative for propulsion of a vehicle by generating rotational motion, whose rotational velocity over time is monitored; and a detonation and / or pre ignition detector operative to provide an alert for impending detonation and / or pre ignition of the engine, if the rotational velocity fluctuates over time to an extent which is predetermined to be unsafe.

6. 发明公开

EP2766588A1 AN AERODIESEL ENGINE 有权转让
标题翻译： AERODIESELMOTOR
公开(公告)号：EP2766588A1
公开(公告)日：2014-08-20
申请号：EP12839362.6
申请日：2012-10-12
申请人： Engineered Propulsion Systems, Inc. , Weinzierl, Steven M. , Fuchs, Michael J.
发明人： WEINZIERL, Steven M. , FUCHS, Michael J.
IPC分类号： F02B75/22 , B64D27/04 , F02B75/00
CPC分类号： F02B75/246 , B23P15/00 , B64D27/04 , F02B37/007 , F02B61/04 , F02B75/00 , F02B75/18 , F02B75/22 , F02B2075/1832 , F02D41/0082 , F02D41/0087 , Y02T50/44 , Y10T29/49231
摘要： The present invention is an aero engine that is provided with compression combustion and weighs less than 725 lbs. The present invention is further a method of forming the aero engine.

7. 发明公开

EP1998600A3 Dual mode searchlight dimming controller systems and methods 有权
标题翻译：系统和用于控制双模Scheinwerferdimmung方法
公开(公告)号：EP1998600A3
公开(公告)日：2012-07-25
申请号：EP08157342.0
申请日：2008-05-30
申请人： Honeywell International Inc.
发明人： Mubaslat, Saed M. , Giffen, Craig E. , Policy, Richard P. , Ferguson, Joseph L.
IPC分类号： H05B33/08 , H05B39/04 , H05B37/03 , H05B39/10 , B64D47/02
CPC分类号： H05B39/105 , B64D27/04 , B64D2203/00 , H05B33/0818 , H05B33/0851 , H05B37/036 , H05B39/047 , Y02B20/346 , Y02B20/48
摘要： A solid state microprocessor or digital signal processor (DSP) for dual mode illumination and dimming into modem aerospace searchlights. The system (20) is a universal dimming platform with "smart functions" that include and arc not limited to multiple light intensity linearization curves, analog and/or digital input dimming interface, built-in tests and health monitoring, synchronized dual mode light output with canopy position, light driver redundancy, lamp life reporting, and controlled switching with improved EMI. With real-time monitoring of the system parameters it monitors the lights proper operation and failures which can be a concern for flight-critical lighting.

8. 发明授权

EP1323632B1 Oil receiver 有权
标题翻译：油接收器
公开(公告)号：EP1323632B1
公开(公告)日：2010-05-19
申请号：EP02026544.3
申请日：2002-11-27
申请人： HONDA GIKEN KOGYO KABUSHIKI KAISHA
发明人： Niimi, Atsushi , Sasaki, Takashi
IPC分类号： B64C11/38
CPC分类号： B64C11/38 , B64D27/04

9. 发明公开

EP1470335A4 RECIPROCATING FLUID ENGINE 有权
标题翻译： HUBKOLBEN-FLUIDMOTOR
公开(公告)号：EP1470335A4
公开(公告)日：2008-10-15
申请号：EP02798634
申请日：2002-12-31
申请人： SPIN MASTER LTD
发明人： BILYK DEREK , DE LAURIER JAMES , KOWNACKI CHARLES
IPC分类号： A63H27/28 , F15B1/00 , A63H29/00 , B64C33/00 , B64D27/04 , F01B11/04 , F01B17/02 , F01L23/00 , F02B75/34
CPC分类号： F01B11/001 , B64C33/00 , B64D27/04 , F01B17/02 , F01L21/04 , F01L23/00 , F01L2003/25 , F02B75/34 , F15B21/12
摘要： A reciprocating fluid engine (31) is provided having a high frequency and a high stroke force. The reciprocating fluid engine may be used to power a vehicle, such as a toy ornithopter (51). The reciprocating fluid engine has a piston (7) in which every stroke is a drive stroke. An ornithopter having the reciprocating fluid engine has a piston in which each piston stroke moves the wings of the ornithopter either up or down, thereby causing the wings to flap.

10. 发明公开

EP1323632A1 Oil receiver 有权
标题翻译： OL-Empfänger
公开(公告)号：EP1323632A1
公开(公告)日：2003-07-02
申请号：EP02026544.3
申请日：2002-11-27
申请人： HONDA GIKEN KOGYO KABUSHIKI KAISHA
发明人： Niimi, Atsushi , Sasaki, Takashi
IPC分类号： B64C11/38
CPC分类号： B64C11/38 , B64D27/04
摘要： The invention provides an oil receiver in which friction with respect to the shaft body generated in association with introduction of hydraulic pressure into the oil receiver is alleviated, and thus the amount of fuel consumption is reduced and durability is improved, whereby the types of the components is reduced, and thus the costs may be reduced.
An oil receiver including a connecting oil passage (21) communicating with the inside of the shaft body(12) via the communication hole (16) formed on the outer periphery of the aforementioned shaft body(12), an lead-in oil passage (22) for introducing lubricating oil into the aforementioned connecting oil passage(21) extending from the aforementioned connecting oil passage(21)radially outward wherein lubricating oil is introduced from the aforementioned lead-in oil passage (22) into the inside of the aforementioned shaft body (12), characterized in that a balance oil passage(23)is extending integrally from the aforementioned connecting oil passage(21) radially outward on the opposite side symmetrically with the aforementioned lead-in oil passage(22), and the balance oil passage(23)is closed at the extremity thereof.
摘要翻译：本发明提供了一种油接收器，其中相对于在将油压引入储油器中产生的轴体的摩擦力减轻，因此燃料消耗量减少并且耐久性得到改善，由此构件的类型减少，因此可能降低成本。一种油接收器，包括：连接油路（21），其经由形成在所述轴体（12）的外周上的连通孔（16）与所述轴体（12）的内部连通，引入油路（ 22），用于将润滑油引入到从上述连接油路（21）径向向外延伸的上述连接油路（21）中，其中润滑油从上述引入油路（22）引入上述轴主体（12），其特征在于，平衡油路（23）从上述连接油路（21）的一侧延伸，与上述引入油路（22）对称地在相对侧径向向外延伸，余量油通道（23）在其末端封闭。

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