Invention Grant
- Patent Title: Anti-icing system and aircraft
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Application No.: US15390799Application Date: 2016-12-27
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Publication No.: US10589866B2Publication Date: 2020-03-17
- Inventor: Masatoshi Morishita , Masanori Tsujita , Satoshi Watanabe , Yoichi Uefuji , Kazuhiro Kawai , Toshiyuki Ishida , Gento Ichikawa , Go Fujita
- Applicant: MITSUBISHI AIRCRAFT CORPORATION
- Applicant Address: JP Aichi
- Assignee: MITSUBISHI AIRCRAFT CORPORATION
- Current Assignee: MITSUBISHI AIRCRAFT CORPORATION
- Current Assignee Address: JP Aichi
- Agency: Pearne & Gordon LLP
- Priority: JP2016-009788 20160121
- Main IPC: B64D15/04
- IPC: B64D15/04 ; B64C3/00

Abstract:
An anti-icing system according to the present invention includes: a piccolo tube that includes a flow path through which heated gas flows in the longitudinal direction from a rear end to a front end, and a plurality of ejection holes provided along the longitudinal direction to make the flow path communicate with an outside; and an engine serving as a supply source that supplies the heated gas toward the piccolo tube. The piccolo tube is decreased in an area of the flow path in a stepwise manner or in a continuous manner in the longitudinal direction, and has a continuous side surface provided with the ejection holes.
Public/Granted literature
- US20170210476A1 ANTI-ICING SYSTEM AND AIRCRAFT Public/Granted day:2017-07-27
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