| 摘要 |
<p>The leading edge has external wall (5a) and de-icing assembly to allow circulation of hot air along span of wind. The de-icing assembly has hot air distribution duct (15a) extending inside leading edge and with multiple openings (25a) over at least a part of its length. An accumulator for hot air (19a) is connected to ends of duct which is coupled via conduits at exterior of leading edge to engine of aircraft.</p> |
