One could say that the vane leading edge (22) is oriented towards the leading edge of the blade and the vane trailing edge (23) looks in the direction of the trailing edge of the blade.
Wire mesh materials are coated with an erosion-resistant coating, formed to the shape of the airfoil leading edge, and molded into the leading edge during airfoil fabrication.
The leading edge of the vane is without the erosion coating and is bare metal.
The impeller vane is configured to continuously present an aggressive cutting surface at the leading edge of the vane even though the vane may become degraded and worn through continuous use.
A cambered vane leading edge or nose is positioned along a first inner and outer airfoil surface junction, and a vane trailing edge positioned along a second inner and outer surface junction.
In its first position, the leading edge of the blade compresses a length of tube against a first surface disposed in the tube-receiving portion, while in the second position, the blade does not compress the tube.
The outer end (10) of the leading edge of the vane is positioned behind a shoulder (9) provided with grooves (11), which cooperates with the vanes of the impeller.
The diffuser vane includes a leading edge at a downstream end of the vane and a trailing edge at an upstream end of the vane.
The guide vane (22) comprises a leading edge (38) and a trailing edge (40) and the guide vane (22) extends from the leading edge (38) to the trailing edge (40) along a mean camber line (42).
One could say that the vane leading edge (22) is oriented towards the leading edge of the blade and the vane trailing edge (23) looks in the direction of the trailing edge of the blade.
Wire mesh materials are coated with an erosion-resistant coating, formed to the shape of the airfoil leading edge, and molded into the leading edge during airfoil fabrication.
The leading edge of the vane is without the erosion coating and is bare metal.
The outer wall includes a leading edge (20), a trailing edge (22) opposed from the leading edge in a chordal direction, a pressure side (24), and a suction side (26).
A radius of curvature of the leading edge and a radius of curvature of the trailing edge vary along a span of the vane.
The blade includes one or more openings at the suction side, in some cases between the leading edge and the trailing edge.
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,
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