HEAT INPUT REDUCING STRUCTURE FOR AIRCRAFT, HEAT INPUT REDUCING SYSTEM, AIRCRAFT, AND AIRCRAFT MANUFACTURING METHOD

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United States of America Patent

APP PUB NO 20230059838A1
SERIAL NO

17795674

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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An outer surface of a part of an airframe includes a mixed region in which a first color similar to a color applied to an adjacent region and a second color having a lower absorption rate of sunlight than the first color are mixed in a predetermined color distribution pattern. A reflective material that contributes to an increase in a reflection rate of sunlight is added to a part to which at least the first color is applied in the mixed region.

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Patent Owner(s)

Patent OwnerAddress
MITSUBISHI AIRCRAFT CORPORATION2-15 OYE-CHO MINATO-KU NAGOYA-SHI AICHI 455-8555

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Hara, Nobuhide Tokyo, JP 36 34
Kudo, Hideyuki Tokyo, JP 8 0
Oda, Takuo Tokyo, JP 18 9
Suzuta, Tadahiko Tokyo, JP 13 40
Umemoto, Toshiyuki Aichi, JP 11 157

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Citation count rangeNumber of patents cited in rangeNumber of patents cited in various citation count ranges510655382301 - 1011 - 2021 - 3031 - 4002505007501000125015001750200022502500275030003250350037504000425045004750500052505500

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