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

WO2005097599A3 AIRCRAFT DEFUELING APPARATUS AND METHOD 审中-公开
标题翻译：飞机预定装置和方法
公开(公告)号：WO2005097599A3
公开(公告)日：2006-08-17
申请号：PCT/US2004032051
申请日：2004-09-30
申请人： SPOKANE IND INC
发明人： KUNTZ JAMES P
IPC分类号： B64D37/20 , B64D37/24 , B64D37/28 , B64F1/28
CPC分类号： B64F1/28 , B64D37/20
摘要： An apparatus and method for defueling an aircraft, including a defueling fitting (100) comprising one or more structural connectors (102, 104) or suction cups, attached by a mount (130) and an actuator assembly (140) for opening the aircraft defueling valve.
摘要翻译：一种用于对飞行器进行排油的装置和方法，包括由安装件（130）和致动器组件（140）附接的一个或多个结构连接器（102,104）或吸盘的防油接头（100），用于打开飞机阀。

2. 发明申请

WO2022216474A1 MANAGING HYDROGEN FUEL IN HYDROGEN FUEL CELL-POWERED AIRCRAFT 审中-公开
公开(公告)号：WO2022216474A1
公开(公告)日：2022-10-13
申请号：PCT/US2022/022278
申请日：2022-03-29
申请人： ZEROAVIA, INC.
发明人： MIFTAKHOV, Valery , DE VAULT, Gabriel
IPC分类号： B60L55/00 , H02J3/38 , H02J15/00 , B64D27/24 , B64D37/30 , B64D37/20
摘要： Method and system for managing hydrogen fuel in hydrogen fuel cell-powered aircraft is disclosed. The method identifies unused hydrogen fuel in a fuel tank of the aircraft. Determines an amount of the unused hydrogen fuel in the fuel tank of the aircraft. Transfers the amount of the unused hydrogen fuel from the fuel tank of the aircraft into a hydrogen fuel cell of the aircraft and converts the amount of the unused hydrogen fuel into electricity via the hydrogen fuel cell of the aircraft.

3. 发明申请

WO2015048695A1 METHODS, SYSTEMS AND APPARATUS FOR AIRCRAFT AUXILIARY FUEL TANKS 审中-公开
标题翻译：用于飞机辅助燃油箱的方法，系统和装置
公开(公告)号：WO2015048695A1
公开(公告)日：2015-04-02
申请号：PCT/US2014/058145
申请日：2014-09-29
申请人： LONG RANGE AG , KIRK, Philip , PRAKASH, Om , SWIFT, Peter
发明人： KIRK, Philip , PRAKASH, Om , SWIFT, Peter
IPC分类号： B64C1/20 , B64D37/00 , B64D37/04 , B64D37/20
CPC分类号： B60K15/06 , B60K15/035 , B60K15/067 , B60K2015/03144 , B60K2015/03164 , B60K2015/03217 , B60K2015/03447 , B64C1/20 , B64D37/00 , B64D37/04 , B64D37/20 , Y10T137/6906 , Y10T137/86187 , Y10T137/86196
摘要： An aircraft auxiliary fuel tank system comprising a master tank and a plurality of slave tanks connectable to the master tank. The slave tanks can be easily added or removed to adjust fuel capacity. A rail assembly is provided to assist in the easy installation and removal of the slave and master fuel tanks. Methods are provided for using the auxiliary fuel tanks system and for providing a service for slave tank distribution, reservation and installation.
摘要翻译：一种飞机辅助油箱系统，包括主油箱和可连接到主油箱的多个从油箱。可以方便地添加或移除子液箱以调节燃油容量。提供了一种轨道组件，以帮助容易地安装和拆卸从动和主燃料箱。提供了使用辅助燃料箱系统和提供从罐分配，预约和安装的服务的方法。

4. 发明申请

WO2009139801A2 OFFSET AMBIENT LEVEL FUEL FEED SYSTEM 审中-公开
公开(公告)号：WO2009139801A2
公开(公告)日：2009-11-19
申请号：PCT/US2008/088507
申请日：2008-12-30
申请人： SIKORSKY AIRCRAFT CORPORATION , SMITH, David, R. , BURG, Joe, James
发明人： SMITH, David, R. , BURG, Joe, James
IPC分类号： B64D37/20 , F02C7/236 , B64D37/14 , B64D37/02
CPC分类号： F02C7/236 , B64D37/00 , B64D37/04 , B64D37/14 , F05D2220/329 , Y10T137/0396 , Y10T137/85978
摘要： A fuel system for an aircraft includes a fuel collector downstream of a boost pump and upstream of an engine fuel pump.
摘要翻译：用于飞机的燃料系统包括在增压泵下游的燃料收集器和发动机燃料泵的上游。

5. 发明申请

WO2009137942A1 AUXILIARY FUEL TANK SYSTEM 审中-公开
标题翻译：辅助燃油箱系统
公开(公告)号：WO2009137942A1
公开(公告)日：2009-11-19
申请号：PCT/CA2009/000687
申请日：2009-05-19
申请人： ELISEN TECHNOLOGIES INC. , RAHMAN, Taifur , MILES, David, F., E.
发明人： RAHMAN, Taifur , MILES, David, F., E.
IPC分类号： B64D37/20 , B64D37/02
CPC分类号： B64D37/02 , B64D37/04 , B64D37/20
摘要： An auxiliary fuel tank system connected to a main tank of an aircraft having a refuel input assembly. The auxiliary fuel tank system comprises an ejector system operatively connected to the refuel input assembly, a forward tank operatively connected to the ejector system, and/or at least one aft tank operatively connected to the ejector system. The forward and/or at least one aft tank transfer fuel to the main tank using gravity.
摘要翻译：辅助燃料箱系统连接到具有加油输入组件的飞机的主油箱。辅助燃料箱系统包括可操作地连接到加油输入组件的喷射器系统，可操作地连接到喷射器系统的前舱和/或操作性地连接到喷射器系统的至少一个后舱。前部和/或至少一个后舱通过重力将燃料转移到主油箱。

6. 发明申请

WO2005097599A9 AIRCRAFT DEFUELING APPARATUS AND METHOD 审中-公开
标题翻译：飞机预定装置和方法
公开(公告)号：WO2005097599A9
公开(公告)日：2006-01-26
申请号：PCT/US2004032051
申请日：2004-09-30
申请人： SPOKANE IND INC
发明人： KUNTZ JAMES P
IPC分类号： B64D37/20 , B64F1/28 , B65B31/04
CPC分类号： B64F1/28 , B64D37/20
摘要： A method and apparatus for defueling an aircraft. The apparatus includes a defueling fitting comprising one or more structural connectors, which may include one or more suction cups. The one or more structural members are attached to a mount. The mount may be of any shape, including generally straight, angled, polygonal, or circular. An actuator assembly is attached to the mount for opening an aircraft defueling valve. The first and second suction cups are operatively connected to a vacuum source to connect the defueling fitting to an aircraft body, with the actuator assembly positioned at the aircraft defueling valve. The defueling fitting facilitates safe and convenient defueling of certain aircraft that have recessed or covered fuel drain valves. For example, the Boeing C-17 has fuel drain valves that are recessed behind doors, heretofore presenting a great obstacle to appropriate defueling. The defueling fitting described herein may be used in small and tight spaces, even when other conventional defueling fittings are not helpful.
摘要翻译：一种用于防空飞机的方法和装置。该装置包括一个包括一个或多个结构连接器的排放配件，其可以包括一个或多个吸盘。一个或多个结构构件附接到安装件。安装件可以是任何形状，包括大致直的，有角度的，多边形的或圆形的。致动器组件附接到安装件以打开飞机防油阀。第一和第二吸盘可操作地连接到真空源，以将排油配件连接到飞行器主体，致动器组件定位在飞机排出阀处。防空配件有助于安全方便地对具有凹陷或覆盖燃油排放阀的飞机进行排污。例如，波音C-17具有在门后凹陷的排油阀，迄今为止阻碍了适当的排污。即使在其他常规的排放配件没有帮助的情况下，这里描述的排油配件可以用在小而紧密的空间中。

7. 发明申请

WO2003011691A1 EXHAUSTION VALVE OF WATER FROM FUEL TANK, WITH A DEVICE AGAINST ROBBERY OF THE FUEL AND OF THE VALVE FOR AIRPLANES 审中-公开
标题翻译：来自燃油箱的水的排气阀，具有针对飞机的燃料和阀门的装置的装置
公开(公告)号：WO2003011691A1
公开(公告)日：2003-02-13
申请号：PCT/BR2002/000107
申请日：2002-08-02
申请人： CAMPOS, Alican, Macedo, Calabrezi
发明人： CAMPOS, Alican, Macedo, Calabrezi
IPC分类号： B64D37/20
CPC分类号： B64D37/20
摘要： The invention describes a drain for manual exhaustion of water that lies at the bottom of airplanes' fuel tanks, working together with a second device that avoids the robbery of fuel as well as the robbery of the exhaustion valve. The main goals are the exhaustion of water that lies on the bottom of airplanes' fuel tanks, to avoid the damage of the valve as well as the robbery of it. Once the drains can be taken off from the airplanes, it is usual the robbery of fuel through the drains. Although the valves are made for exhaustion of water, nothing avoids the exhaustion of fuel. The frequency of such situations prevent the operation of airplanes for lack of fuel as well for absence of the valve, once this is also usually stolen.
摘要翻译：本发明描述了一种用于手动耗尽水的排水装置，其位于飞机燃料箱的底部，与避免燃料抢抢以及排气阀抢险的第二装置一起工作。主要目标是耗尽飞机燃油箱底部的水，以避免阀门的损坏以及抢劫。一旦下水道可以从飞机上卸下，通常会通过排水渠抢劫燃料。虽然这些阀门是为了用尽水而制造的，但是没有什么可以避免燃料的耗尽。这种情况的频率阻止了飞机缺乏燃料以及没有阀门的操作，一旦这样也通常被盗。

8. 发明申请

WO2021054521A1 공중 급유 드론을 이용한 전동 카트의 연료 공급 시스템 및 방법 审中-公开
公开(公告)号：WO2021054521A1
公开(公告)日：2021-03-25
申请号：PCT/KR2019/015509
申请日：2019-11-14
申请人： 주식회사 아이온커뮤니케이션즈
发明人： 백경석 , 오재철
IPC分类号： G06Q50/30 , B64C39/02 , B64D39/00 , B64D37/20 , B64D47/08 , B60K15/077 , B60K15/04
摘要： 본 발명은 공중 급유 드론을 이용한 전동 카트의 연료 공급 시스템 및 방법에 관한 것으로서, 적어도 하나의 공중 급유 드론을 이용한 적어도 하나의 전동 카트로의 연료 공급을 관제하는 연료 공급 관제 서버에 있어서, 상기 적어도 하나의 전동 카트로부터 급유 요청 메시지와 함께 연료 소진 예상 시간 및 카트 위치 정보를 수신하는 카트 정보 수신부, 상기 적어도 하나의 공중 급유 드론의 드론 위치 정보 및 급유 가능 여부 정보를 포함하는 드론 상태 정보를 획득하는 드론 정보 획득부, 상기 적어도 하나의 공중 급유 드론이 드론 기지에서 출발하여 급유를 요청한 전동 카트의 위치까지 도착하는 소요되는 이동 예상 시간을 계산하고, 상기 전동 카트의 연료 소진 예상 시간에 따라 현 시점에서 얼마나 여유 시간이 남아있는지 예측하여 스케줄 정보를 생성하는 스케줄 생성부, 상기 드론 상태 정보와 스케줄 정보에 따라 각각의 전동 카트에 급유를 실행할 공중 급유 드론을 선택하는 드론 선택부, 및 상기 선택된 공중 급유 드론에 급유 실행 메시지 및 급유 대상인 전동 카트의 위치 정보를 전송하는 급유 실행부를 포함할 수 있다.

9. 发明申请

WO2019217285A1 SYSTEM AND METHOD OF DEFUELING AN AIR VEHICLE 审中-公开
公开(公告)号：WO2019217285A1
公开(公告)日：2019-11-14
申请号：PCT/US2019/030863
申请日：2019-05-06
申请人： AGE LOGISTICS CORPORATION
发明人： FISHMAN, Yehuda R. , FISHMAN, Daniel
IPC分类号： B60K15/03 , B64D37/20 , B64F1/28
摘要： A movable system for defueling an air vehicle comprising a movable tank for holding the fuel, a mobile base, and a fuel transfer system. The tank comprises at least one filling port and at least one discharge port, at least one on-off valve for the discharge port, and a lock for locking and unlocking the on-off valve. The fuel transfer system is supported by the mobile base to move with the mobile base and comprises at least one pump for pumping the fuel from the aircraft to the tank. A method of defueling an air vehicle comprising selecting the system, moving both the mobile base with the fuel transfer system and the tank proximate to an air vehicle with fuel in its fuel tank, pumping fuel from the air vehicle fuel tank into the tank with the pump, and discharging fuel from the tank through the discharge port.

10. 发明申请

WO2013056626A1 一种飞机燃油放沉淀工具审中-公开
公开(公告)号：WO2013056626A1
公开(公告)日：2013-04-25
申请号：PCT/CN2012/082672
申请日：2012-10-10
申请人：中国商用飞机有限责任公司 , 中国商用飞机有限责任公司上海飞机设计研究院
发明人：邓英华 , 孙欣 , 罗世明
IPC分类号： B64D37/20
CPC分类号： B64F1/28
摘要：一种飞机燃油放沉淀工具，其用于在飞机机翼整流鼓包内打开飞机燃油放沉淀阀排放燃油箱内的沉淀，飞机燃油放沉淀工具包括：开启装置、照明装置、盛放杯、杆体和支撑板等。由于本发明的工具通过支撑板固定，所以在使用过程中不再需要人手托举，操作省力简便。并且，工具中带有支撑板和支撑弹簧，利用工具盛放杯内液体的重量变化与和支撑弹簧力的平衡，自动调节燃油放沉淀阀流量的功能，从而避免燃油的溢出。

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