摘要:
A method includes joining an integral bulkhead (20) and a blade shell (22, 24) to form a blade (12) and separating the blade into two blade segments at a location including the integral bulkhead such that each blade segment comprises a portion of the integral bulkhead and a portion of the blade shell.
摘要:
A spar for a rotor blade assembly is provided including a generally hollow tubular body. A spacer protrudes from at least one surface of the body along a length of the body. A hole extends through the body and the spacer. The hole is configured to align with a through hole in an adjacent flexbeam assembly. The spacer is configured to contact a surface of the adjacent flexbeam assembly to create a match fit between the body and the flexbeam assembly.
摘要:
Fan assemblies, and in particular fan wheels and stator assemblies for fan assemblies, are disclosed. In one embodiment, the fan wheel includes a wheel back having an outer surface forming one of a curved dome-shape and a truncated cone-shape. The fan wheel may also include a plurality of fan blades radially spaced about and mounted to the outer surface of the wheel back. In one embodiment, each of the fan blades is formed from a segment of an airfoil-shaped aluminum extrusion defining at least one internal cavity. The fan blade first ends can be provided with a compound cut profile with at least one curved cut such that the first end of the blade is mounted flush to the wheel back outer surface. The stator assembly can also be provided with a plurality of stator blades formed from airfoil-shaped aluminum extrusion segments and provided with compound cut profiles.
摘要:
The invention relates to a method for cutting a preform (1) intended for the production of a turbomachine part and comprising a weaving of a plurality of threads (9), said threads (9) comprising singles (3) that are visually identifiable, along a cutting contour (5) calculated based on a preform model in which the threads (9) have a reference arrangement, said method including the steps consisting of: - taking an image of the preform (1), - processing the image in such a way as to determine a deviation in the arrangement of the threads (3) which are visually identifiable relative to the reference layout, - correcting the cutting contour (5) according to said deviation, and - cutting the preform along the corrected cutting contour (13).
摘要:
Fastening system for wind turbines characterized by comprising a front flange (9) and a rear flange (8), which are joined together and supported on the hollow rotary shaft (2), and coupled to the pitch system comprising the bearings (6) for the shaft and the star-shaped part (4). The fastening method couples the rear flange (8) to the hollow shaft (2) with a tapered collar (10) and also to the front flange (9) through some spacer bushings (11). The collar (10) uses friction to transfer significant moments and axial stresses so as to improve the fastening system, and the direction of the bolts on the collar (10) and the bolts (12) on the spacer bushings (11) simplify inspection and maintenance tasks.
摘要:
The invention relates to a lifting beam (1) for lifting and handling a rotor blade (2) of a wind energy plant (100), comprising a fastening means (6) for fastening the lifting beam to a crane, at least one fastening means (12) for fastening the lifting beam to the rotor blade (2), a longitudinal pivoting means (18) for pivoting the rotor blade (2) which is supported by the lifting beam (1) about a longitudinal axis of the rotor blade (2), and/or a transverse pivoting means (10, 22) for pivoting the rotor blade (2) which is supported by the lifting beam (1) about a transverse axis perpendicular to the longitudinal axis. The invention further relates to a method for mounting rotor blades of a wind energy plant using a lifting beam according to the invention.