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Patent Searching and Data


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
Application Number:
JP2016517374A
Publication Date:
March 27, 2019
Filing Date:
August 26, 2014
Export Citation:
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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