Each rotor blade includes a blade tip at a radially distal end of each blade.
The rotor blade includes a blade root arranged within the slot.
The rotor blade extends, starting from the blade connection (10), along a longitudinal extension direction to the blade tip (11).
The blade tip (8) results in a blade tip vortex downstream of the rotor blade (1)during operation.
A helicopter rotor blade that has a blade body and a control flap secured to the blade body.
The paddle area is delimited by a paddle sheet (18).
A first paddle has a first plurality of pixel elements wherein the first paddle is arranged to sweep out a first area during a first paddle cycle.
The motorized paddle assembly comprises a paddle, internal mechanisms, and a housing that encloses the internal mechanisms.
A paddle is mounted on the shaft.
Each blade has a blade compliance.
The sectional blade comprises a first blade portion and a second blade portion.
The blade is a two part blade with a first leading blade portion (7) pivotably connected to a second trailing blade portion (8).
A blade part having a conventional blade design is utilised for a part of the outboard blade part in order to form a longer, assembled blade having a similar, conventional blade design.
The mid-blade end (148) of the outboard blade section (108) is joined to the mid-blade end (114) of the inboard blade section (106).
The blade shell (7) receives the vane (61) in positive engagement and can be separated from the blade (61).
The vane assembly comprises at least a first blade, a second blade and a flexible component.
This applies to the vane-end leakage vortex that extends from the vane-end clearance between the tip of the full blade (5F) and the shroud towards the front edge (7a) section of the splitter blade (7).
The invention relates to a rotor blade and a wind energy installation with a rotor blade.
The invention relates to a rotor blade for a wind energy installation, comprising at least one flange extending longitudinally from the base of a rotor blade to the tip of the rotor blade, the flange tapering off in the longitudinal direction.
The rotor blade assembly also includes a sheath extending around the composite blade portion.
The invention relates to a rotor blade (5) of a wind turbine (1), comprising a rotor blade shell (7) and a blade root (6) for fixing the rotor blade (5) on a hub (4) of the wind turbine (1).
The rotor blade assembly further includes a noise reducer configured on the rotor blade.
Blade for a wind turbine, and wind turbine provided with a blade of this type.
The wind turbine blade (20) includes a plurality of pivotable blade segments (30).
Each blade now consists of two blades (a rear blade and a front blade, called interactive blades).
The first blade (118) is generally parallel to the second blade (120).
The blade has a recess extending radially and inwardly into the blade.
The wind turbine blade (1) is provided with a blade tip (2), a blade root (4) connected to a hub (112), and an airfoil (6) located between the blade tip (2) and the blade root (4).
Furthermore, the unit generator may include a main blade and a sub-blade which is smaller than the main blade.
A normally open blade (55) is positioned relatively parallel to a movable blade (68).
The rotating element includes a plurality of blades each having a blade root proximal to the axis, a blade tip remote from the axis, and a blade span measured between the blade root and the blade tip.
A blade assembly having a rotatable flap is coupled to the blade arm.
The multiplane wing (116) has a first blade (118) and a second blade (120).
The blade pitch, blade thickness, blade width, blade weight, static-balance, and dynamic-balance of the propeller are calculated by utilizing computer numerical calculation method.
A blade shank shaft (2) is coaxially arranged on the blade shank seat (11), and a blade (3) is fixedly arranged on the blade shank shaft (2).
Said system comprises a blade footing (12) that is retained on a blade holder (14) against the forces acting on the blade.
As a result, the blade may pivot about the blade axis while traveling along a blade path during rotation of the hub.
Requêtes fréquentes français :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
Requêtes fréquentes anglais :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
Traduction Translation Traducción Übersetzung Tradução Traduzione Traducere Vertaling Tłumaczenie Mετάφραση Oversættelse Översättning Käännös Aistriúchán Traduzzjoni Prevajanje Vertimas Tõlge Preklad Fordítás Tulkojumi Превод Překlad Prijevod 翻訳 번역 翻译 Перевод