The first vane (12) and the second vane (14) can be substantially parallel.
In such an embodiment, the first vane (12) is disposed offset from the second vane (14).
The disk (10) has a first vane (12) and a second vane (14) disposed relative to the first vane (10).
A vane is displaceably received in the rotor with its vane base (32) and rests on the interior peripheral surface of the pump housing with its vane tips (28), thereby defining a suction chamber and a pressure chamber, said vane having a constant length.
Each of the plurality of vanes is substantially rectangular or square.
The capacitive reactive armor includes, but is not limited to, a first flyer plate, a second flyer plate, and a capacitor positioned between the first flyer plate and the second flyer plate.
The armature includes a first portion 22, a second portion 24, and a fin 26.
The wing-panel extends laterally beyond at least one lateral side edge of the backsheet (28) in the intermediate portion (76) of the article, and the wing-panel (42) is configured to wrap about an undergarment.
The clip may include a base, a pair of flaps, a pair of arms and at least one wing.
A clamp assembly (10) having a body (12), a power supply (110), a vane jaw arm (42) and stop (66) is provided.
The louvres (3) which can move forward are formed by one longitudinal fin (11) having an annular fin part (12) in the centre.
A fin is located between two adjacent heat exchange tubes, and the fin includes fin plates each having louvers.
Each tube is interference fit in one of the openings of the plate fin, positioning a louver between each tube.
The plate fin includes openings, and a louver including parallel vertical slots is located between each of the openings.
Each side wall (21a) is provided with a louver (31) which at least operates to turn the cooling medium communicating inside a corresponding fin section (21).
spindle flyer for spinning frames
A rotary flyer (14) generates on a template coil windings that are removed by a lifter.
The inventive spindle is characterized by the fact that the twisting device is embodied as a flyer (7) with a thread guide.
The roving frame is provided with so called suspended flyers (1), that is to say flyers arranged pivotingly in a flyer head.
A coil winding machine in which a stepped winding frame moves in the direction of the center axis of rotation as a flyer turns, whereby the winding frame is wound with coils on a plurality of steps to form coils different in perimeter.
A turbine blade (66) imparts energy to the liquids which are kept from swirling by the kinetic baffles (58).
The nozzle may also include a third guide vane or baffle (4) that lacks a curved deflecting part.
A baffle (20) is mounted at the centre of the opening and is rotatable by a fin (30) or an electric motor (31).
Many externally baffled models are built with a plastic fin on the outside edge.
A blade (121) pushed by gas is provided in the blade chamber (12).
The fluid flow controller may include a casing having a casing blade.
The fluid flow controller may also include a rotor having a first rotor blade and a second rotor blade radially spaced from the first rotor blade.
The fan [110] has a blade [112], a motor [114] and an air guiding portion [116] positioned near the blade [112].
A damper seal (10) and method of sealing and damping a rotating shaft (12) is provided with a stator housing (14) and at least two sealing blades, an upstream sealing blade (16) and a downstream sealing blade (18).
A rotatably paddle wheel (4) is arranged between said magnets, the space between the paddle wheel (4) and the stator being filled with fluid metal.
A paddle (42) transfers the group to the packaging machine (14).
Furthermore, a cushioned compression paddle or x-ray plate is provided wherein said compression paddle or x-ray plate and said cushion can be separately or integrally formed.
The paddles are each oriented to extend at an angle relative to the radius of the rear base plate and the at least one forward ring.
The bolt includes a paddle section (11) formed by deforming a portion (12, 13) of the bolt through application of an eccentric shear force.
A turbine bucket (10) includes an airfoil (14) and a shroud (16).
The single bucket drag-type turbine is thus able to efficiently extract the rotational kinetic energy of fluid particles in waves.
The tip section may include a winglet.
The at least one winglet is compliant in a preferential direction.
A winglet includes a vertical member and a mounting member.
A winglet includes a vertical member and a mounting member.
A winglet (12) for an aircraft wing is provided.
There may be a corresponding second cross-fin adjacent each cross-fin (127).
The fins constitute a first fin (31) and a second fin (30), the local heat flux of which on the partition wall (19) is smaller than the first fin (31).
Disclosed is a variable fin assembly including a fin having a planar structure.
Fin field effect transistors can be formed on the at least one silicon-germanium alloy fin and the at least one silicon fin.
An indoor heat exchanger (10) comprises a lower fin (30), and an upper fin (40).
The cutting head (1) includes a first linear flange (9), a second linear flange substantially parallel to the first linear flange (9) and means for holding a cutting bit.
A separate finger flange (32) may subsequently be snapped into place if required.
In another embodiment, an outer circumference portion of the second flange has an increased thickness relative to an inner, annular portion of the second flange.
There is provided a novel tracheostomy tube flange.
Each vane at said other end thereof forms a flange (50) projecting at both sides of the vane and forming a seal against the inside surface of the outer cylinder.
By this method, damage of the fin of the turbine rotor blade can be repaired.
A rotor blade element (40, 50, 60) adapted for mounting on a wind turbine rotor blade (5) is described.
Also disclosed is a turbine rotor blade designed to form a stage pair with the stator vane.
Rotor blade element and method for improving the efficiency of a wind turbine rotor blade.
A wind turbine rotor blade (10) comprising one or more means (4) secured to the blade (10) for changing the profile thereof depending on the atmospheric temperature.
Meandering cooling channels inside a turbine blade are difficult to produce in one piece by using casting techniques.
The present invention refers to a turbine blade (1) comprising a fin (6) for a turbo machine, especially a turbine.
A turbine blade system relating to a tip device appended to the blade tip of a turbine.
Turbine blade (10) has a plurality of trailing edge discharge openings (28) discharging cooling air.
The process is suitable for a component produced by directional solidification and liquid metal cooling, especially a turbine blade.
The plurality of wings include a right wing and a left wing.
The flaring portion comprises at least one distal wing and at least one proximal wing.
The first wing and the second wing are coupled together by at least one hinge (135a, 135b).
The aforementioned ladle (2) comprises a rectangular metal sheet having two folds such as to form three parts, namely: a central section (2.2), a large section (2.1) and a small section (2.3).
During an implant procedure, the winged implant may be implanted in a crater, whereby the at least one wing may offer an enhanced support of the winged implant in the crater.
Two main fields of application are Ball Pump with Rotary Wing (BPRW) and Ball Engine with Rotary Wing (BERW).
The first bracket includes a U-shaped section extending between first and second wings; a first slot defined in the first wing; and a second slot defined in the second wing.
The invention has a first-type of FinFET which includes a first fin (100), and a second-type of FinFET which includes a second fin (102) running parallel to the first fin (100).
A heat exchanger has a first fin having a hole, a collar attached to the first fin and associated with the hole, and a bluff body carried by the first fin.
The invention also relates to a heat exchanger comprising such a fin (7) and to a method of manufacturing such a fin (7).
An inner fin (1) of a heat exchanger has, on front and rear faces thereof, protruding ridges (2, 3) protruding in opposite directions to each other.
The ratio of the height of the first fin to the height of the second fin comprises a ratio of one to 2/3.
The portion covers each of the fins in the array.
A plug (1) has two wipers (4, 5) on its leading portion, a rear sealing fin (8) and a second sealing fin (15).
The stripping can further comprise a fin, whereby the fin can be located within the pile or alongside the pile.
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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