ROTOR BLADE STRUCTURES

A closeout structure for a rotor blade includes a first fluid channel for supplying a first pressure to a first port of a trailing edge (TE) device, a second fluid channel for supplying a second pressure to a second port of the TE de vice, and a trough disposed between the first fluid channel and th...

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Main Authors SCOTT, Mark, W, THOMAS, Justin, KOPANSKI, Krzysztof
Format Patent
LanguageEnglish
French
German
Published 19.09.2018
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Abstract A closeout structure for a rotor blade includes a first fluid channel for supplying a first pressure to a first port of a trailing edge (TE) device, a second fluid channel for supplying a second pressure to a second port of the TE de vice, and a trough disposed between the first fluid channel and the second fluid channel. The closeout structure forms a double-W shape.
AbstractList A closeout structure for a rotor blade includes a first fluid channel for supplying a first pressure to a first port of a trailing edge (TE) device, a second fluid channel for supplying a second pressure to a second port of the TE de vice, and a trough disposed between the first fluid channel and the second fluid channel. The closeout structure forms a double-W shape.
Author THOMAS, Justin
KOPANSKI, Krzysztof
SCOTT, Mark, W
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DocumentTitleAlternate ROTORBLATTSTRUKTUREN
STRUCTURES D'AUBE DE ROTOR
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RelatedCompanies Sikorsky Aircraft Corporation
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Snippet A closeout structure for a rotor blade includes a first fluid channel for supplying a first pressure to a first port of a trailing edge (TE) device, a second...
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SubjectTerms AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
Title ROTOR BLADE STRUCTURES
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