摘要:
An ceiling fan (10) comprising a motor system (16). The motor system (16) is mounted around a motor shaft (90). The motor shaft (90) couples to a downrod (14) for suspending the ceiling fan (10) from a structure. The motor shaft (90) and motor (16) are encased by a motor housing (198). The motor housing (198) comprises hub arms (202) for mounting a plurality of blade holders (18). The blade holders (18) coupled to a plurality of blades (20) rotatable about the motor (16) during operation. The downrod (14) comprises a wire disk (58) mounting guy wiring (22) to the downrod (14). A retention rod (304) is utilized internal of the motor (16) and downrod (14) as a secondary retention method. An electrical connector (568) is internal of the motor shaft (90) and electrically couples to the stator to power the motor (16).
摘要:
A fan blade (60) and method of covering a fan blade root portion (64) for a gas turbine engine (20) are disclosed. The fan blade includes an airfoil (68) having a leading edge end (70) and a trailing edge end (72), a root portion having a first side surface (74) extending from the leading edge end to the trailing edge end and a second side surface (76) at an opposite side of the first side surface and extending from the leading edge end to the trailing edge end, and a covering (82) disposed against the first side surface and the second side surface, wherein the covering is positioned against the root portion as a single member.
摘要:
A fan system includes a rotor having plurality of blades and a ring airfoil, the plurality of blades being rotatably joined to a hub and the ring airfoil. The fan system may include a second contra-rotationally disposed rotor having a plurality of blades and a ring airfoil. The first and second ring airfoils having a cambered shape and an angle of attack between about -5 degrees and about 45 degrees, more preferably between about 5 degrees and about 30 degrees. Optionally, an outlet guide vane may be mounted rearward of the one or more rotors having a ring airfoil.
摘要:
In an axial flow fan according to the present invention, a plurality of blades rotate about a rotation axis of the blades to convey a fluid. In the axial flow fan, the plurality of blades each have a leading edge at a leading side in a rotational direction, a trailing edge at a trailing side in the rotational direction, and an outer peripheral edge connecting the leading edge and the trailing edge. The leading edge of one of the plurality of blades and the trailing edge of another blade adjacent to the leading edge of the blade in the rotational direction are connected by a plate-shaped connection portion. The plurality of blades each have at least one plate-shaped reinforcement rib extending from a periphery of the rotation axis toward the outer peripheral edge of the blade.
摘要:
A ceiling fan is designed with enhanced structural strength and prolonged service life. The ceiling fan comprises a stator (1), a loading plate (2), a rotor (3) and a plurality of blades (4) is disclosed. The stator (1) includes a shaft (11). The loading plate (2) includes a sleeve (21) and a radial extending portion (22). The radial extending portion (22) radially extends outwards in radial directions of the shaft (11). The sleeve (21) receives a bearing (23) coupled with an outer periphery of the shaft (11). The rotor (3) includes a hub (31) coupled with the loading plate (2). The plurality of blades (4) is coupled with the radial extending portion (22).
摘要:
A load absorbing system that may include a rotor blade retention system (52) is provided. The load absorbing system may include a block (56), a first retainer plate (62A), and a deformable core (54). The block (56) may be selectively positioned alongside a dovetail groove (50). The block (56) may have a first face (66) directed away from the blade root (44) and an axially-spaced second face (68) directed toward the blade root (44). The first retainer plate (62A) may be attached to the second face (68) of the block (56) and axially positioned between the block (56) and the axially-directed surface of the blade root (44). The deformable core (54) may be positioned between the block (56) and the first retainer plate (62A).
摘要:
An axial-flow air blower's fan blades may include a blade portion, and a guide blade portion provided behind the blade portion. The guide blade portion has five guide blades, and the blade portion has a hub and a plurality of blades provided on the hub. The blades and the hub are integrated. There are twelve blades, and an outer circumference defined by the outer edges of the twelve blades has a diameter of 84 mm. The structure is simple and reasonable. The integration of the blades and hub improves concentricity and strength of the blades, increases air volume, and reduces noise. A reasonable number of blades and fan diameter together with a reasonable number of guide blades can improve efficiency and wind speed.
摘要:
An edge seal for preventing airflow through a space between a fan platform and an adjacent airfoil in a gas turbine engine may include a bonding segment being bondable to the fan platform. A sealing flap converges with the bonding segment so that the sealing flap is operatively contactable with the adjacent airfoil. A bumper rib protrudes from the bonding segment so that the bumper rib is bondable to the fan platform.
摘要:
Die Erfindung betrifft einen Nasenkonus (2) für einen Fan (10) eines Flugtriebwerks (1), der ein Konusteil (21) aus faserverstärktem Kunststoff aufweist. Es ist vorgesehen, dass in das Konusteil (21) ein Elastomer (202, 252) integriert ist. Durch Integration eines Elastomers (202, 252) in das Konusteil (21) wird eine verbesserte mechanische Dämpfung einer Schwingungsanregung der Fan-Schaufeln (11) eines Flugtreibwerks (1) bereitgestellt. Die Erfindung betrifft des Weiteren einen Fan (10) und ein Flugtriebwerk (1) mit einem derartigen Nasenkonus (2).
摘要:
A fan rotor, for an aircraft engine, including at least one blade root attachment lug, each blade root attachment lug including an attachment lug surface, wherein at least one cavity is disposed on each attachment lug surface.