AIR FOIL
    1.
    发明专利
    AIR FOIL 失效

    公开(公告)号:JPH1068305A

    公开(公告)日:1998-03-10

    申请号:JP18024697

    申请日:1997-06-23

    Abstract: PROBLEM TO BE SOLVED: To manufacture a light air foil, having rigidity adaptable to a load generated by a gas turbine engine, at a low cost. SOLUTION: An air foil 30 of which, for example, a fan outlet guide vane consists has a body with geometrical cross section comprising a first wall 44; a second wall 46 arranged opposite to the first wall; a front edge 48; a rear edge 50 arranged opposite to the front edge; and at least one of cavities 52 and 54. The cavities 52 and 54 are formed between the first and second walls 44 and 46 and between the front and rear edges 48 and 50. The air foil 30 is extrusion-molded by using non-continuous reinforced aluminum such that the body with geometrical cross section is extended between first and second ends.

    HIGH STRENGTH ALUMINUM ALLOY
    2.
    发明专利

    公开(公告)号:JP2001181767A

    公开(公告)日:2001-07-03

    申请号:JP2000388095

    申请日:2000-12-21

    Inventor: WATSON THOMAS J

    Abstract: PROBLEM TO BE SOLVED: To provide an aluminum alloy having excellent mechanical properties at the temperature up to about 300 deg.C. SOLUTION: This aluminum alloy strengthened by high strength dispersion consists of an aluminum solid solution matrix strengthened by the dispersion of particles based on a compound Al3X having an L12 structure. Various alloy elements are used so that the matrix and particles have similar lattice constants, thus the lattice constants of the matrix and particles are modified. The alloy is produced from a melt by rapid solidification.

    HYBRID METAL FAN BLADE
    6.
    发明申请
    HYBRID METAL FAN BLADE 审中-公开
    混合金属风扇叶片

    公开(公告)号:WO2014196987A3

    公开(公告)日:2015-02-26

    申请号:PCT/US2013046819

    申请日:2013-06-20

    Abstract: A fan blade comprises an airfoil portion and a sheath portion. The sheath portion has a sheath head section, a first sheath flank, and a second sheath flank, both flanks extending chordwise from the forward sheath section. The sheath portion is bonded to the airfoil portion such that the sheath head section covers the forward airfoil edge, defining a blade leading edge. The first sheath flank covers a portion of the first airfoil surface proximate the airfoil forward edge, jointly defining a blade suction surface. The second sheath flank covers a portion of the second airfoil surface proximate the airfoil forward edge, jointly defining a blade pressure surface. The first metallic material is an aluminum alloy containing between about 0.5 wt% and about 3.0 wt% of lithium.

    Abstract translation: 风扇叶片包括翼型部分和鞘部分。 护套部分具有鞘头部分,第一护套侧面和第二护套侧面,两个侧面从前鞘部分向翼伸出。 护套部分结合到翼型部分,使得鞘头部分覆盖前翼型边缘,限定叶片前缘。 第一护套侧面覆盖靠近翼型件前缘的第一翼型件表面的一部分,共同限定叶片抽吸表面。 第二护套侧面覆盖靠近翼型件前缘的第二翼型件表面的一部分,共同限定叶片压力表面。 第一种金属材料是含有约0.5wt%至约3.0wt%的锂的铝合金。

    ALUMINUM BRAZING OF HOLLOW TITANIUM FAN BLADES
    7.
    发明申请
    ALUMINUM BRAZING OF HOLLOW TITANIUM FAN BLADES 审中-公开
    空心钛风扇叶片的铝钎焊

    公开(公告)号:WO2014099067A2

    公开(公告)日:2014-06-26

    申请号:PCT/US2013061571

    申请日:2013-09-25

    Abstract: A fan blade includes first and second titanium portions that are secured to one another with an aluminum alloy braze. A method of manufacturing a fan blade includes providing first and second titanium portions, applying an aluminum alloy braze to at least one of the first and second titanium portions, and heating the fan blade to melt the aluminum alloy braze and join the first and second portions to one another to provide a fan blade with an airfoil exterior contour.

    Abstract translation: 风扇叶片包括用铝合金铜焊彼此固定的第一和第二钛部分。 一种制造风扇叶片的方法包括:提供第一和第二钛部分;将铝合金铜焊施加到第一和第二钛部分中的至少一个上;以及加热风扇叶片以熔化铝合金铜焊并将第一和第二部分 以提供具有翼型外部轮廓的风扇叶片。

    10.
    发明专利
    未知

    公开(公告)号:DE602004025062D1

    公开(公告)日:2010-03-04

    申请号:DE602004025062

    申请日:2004-02-27

    Inventor: WATSON THOMAS J

    Abstract: High strength, high ductility aluminum base alloys consisting of: from 3.0 to 18.5 weight percent nickel, from 3.0 to 14.0 weight percent yttrium, optionally at least one addition selected from the group consisting of from 0.1 to 6.5 weight percent magnesium, from 0.05 to 5.0 weight percent scandium, from 0.1 to 4.0 weight percent titanium, from 0.1 to 4.0 wt% zirconium, from 0.1 to 3.5 weight percent iron, from 0.1 to 3.5 weight percent cobalt, and from 0.1 to 10 weight percent gadolinium, optionally at least one alloying addition selected from the group consisting of gadolinium, cerium, praseodymium, neodymium, and scandium in a combined sum total of from 3.0 to 33 weight percent, and the balance aluminum, and said alloy being in the devitrified state and containing less than 40 percent intermetallic phases.

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