Title:
空中給油アセンブリ内の圧力を示すシステムおよび方法
Document Type and Number:
Japanese Patent JP6492065
Kind Code:
B2
Abstract:
An aerial refueling assembly includes, for example, a pressure transducer, a processor, and one or more light sources. The processor is coupled to the pressure transducer. The one or more light sources are coupled to the processor. The pressure transducer is configured to sense a fuel pressure inside the aerial refueling assembly and to provide a signal that is indicative of the sensed fuel pressure inside the aerial refueling assembly. The processor is configured to receive the signal and to cause the one or more light sources to flash in a manner that relates to the sensed fuel pressure.
Inventors:
David Black
Christopher Eales
Christopher Eales
Application Number:
JP2016517374A
Publication Date:
March 27, 2019
Filing Date:
August 26, 2014
Export Citation:
Assignee:
The Boeing Company
International Classes:
B64D39/00
Domestic Patent References:
JP2011507755A | ||||
JP2004268722A | ||||
JP54061800A | ||||
JP2008531377A | ||||
JP2007050871A | ||||
JP2011494A | ||||
JP63075808A | ||||
JP2013527077A | ||||
JP2007038925A | ||||
JP2013184702A | ||||
JP2005199902A |
Foreign References:
US20120049004 | ||||
US20130020441 | ||||
US20130068889 | ||||
US2954190 | ||||
WO2009082400A1 | ||||
US20100213318 |
Attorney, Agent or Firm:
Yasuhiko Murayama
Tatsuhiko Abe
Kuroda Shinpei
Choi
Tatsuhiko Abe
Kuroda Shinpei
Choi