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Legal status
Patent not validated
(51) | INT.CL. | B64C 23/00 | |
B64C 25/10 | |||
B64F 5/00 |
(11) | Number of the document | 2415670 |
(13) | Kind of document | T |
(96) | European patent application number | 10761366.3 |
Date of filing the European patent application | 2010-03-26 | |
(97) | Date of publication of the European application | 2012-02-08 |
(45) | Date of publication and mention of the grant of the patent | 2016-03-23 |
(46) | Date of publication of the claims translation |
(86) | Number | PCT/JP2010/002209 |
Date | 2010-03-26 |
(87) | Number | WO 2010/116658 |
Date | 2010-10-14 |
(30) | Number | Date | Country code |
2009081708 | 2009-03-30 | JP |
(72) |
ISOTANI, Kazuhide, JP
HAYAMA , Kenji, JP
KUMADA, Toshiyuki, JP
ONO, Masaru, JP
|
(73) |
Kawasaki Jukogyo Kabushiki Kaisha,
1-1, Higashikawasaki-cho 3-chome Chuo-ku, Kobe-shi, Hyogo 650-8670,
JP
Sumitomo Precision Products Co., Ltd., 1-10 Fuso-cho Amagasaki -shi, Hyogo 660-0891, JP The Society of Japanese Aerospace Companies, 1-1-14, Akasaka, Minato-ku Tokyo 107-0052, JP |
(54) | METHOD OF ATTENUATING NOISE IN AIRCRAFT, LANDING GEAR STRUCTURE OF AIRCRAFT, AND AIRCRAFT |
METHOD OF ATTENUATING NOISE IN AIRCRAFT, LANDING GEAR STRUCTURE OF AIRCRAFT, AND AIRCRAFT |