Rotary-Wing Vehicle, and Rotary-Wing Turbine
US-2024328327-A1 · Oct 3, 2024 · US
US9011102B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9011102-B2 |
| Application number | US-201113231246-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 13, 2011 |
| Priority date | Sep 16, 2010 |
| Publication date | Apr 21, 2015 |
| Grant date | Apr 21, 2015 |
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Official abstract text for this publication.
A blade ( 1 ) having a working shell ( 10 ) defining an inner space ( 16 ). The blade has a leading-edge space ( 31 ) and at least one filler means ( 40, 50 ) in said inner space ( 16 ) and a leading-edge fairing ( 20 ) protecting the working shell ( 10 ). The fairing ( 20 ) extends from a pressure-side part ( 21 ) to a suction-side part ( 22 ) via a central part ( 23 ). The working shell ( 10 ) has in the first zone ( 13 ): a pressure-side portion ( 131 ), a central portion ( 133 ), and a suction-side portion ( 132 ). The pressure-side portion ( 131 ) is secured to the pressure-side part ( 21 ). The suction-side portion ( 132 ) is secured to the suction-side part ( 22 ). The blade ( 10 ) includes first damper means ( 60 ) with damping material.
Opening claim text (preview).
What is claimed is: 1. A blade comprising a working shell extending from a leading-edge first zone to a trailing-edge second zone, the working shell defining an inner space, there being a leading-edge spar and a filler material arranged in the inner space extending in the span direction (Y) of the blade, the leading-edge spar being arranged against the working shell in the leading-edge first zone, the blade being provided with a leading-edge fairing protecting the working shell in…
Operations & Transport · mapped topic
Operations & Transport · mapped topic
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