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NOZZLE SHUTTER FOR AVIATION GAS-TURBINE ENGINE (VERSIONS) AND METHOD FOR MANUFACTURE OF NOZZLE SHUTTER (VERSIONS)

机译:航空燃气发动机的气门嘴(版本)和制造气门嘴的方法(版本)

摘要

FIELD: engines and pumps.;SUBSTANCE: nozzle shutter for aviation gas-turbine engine is arranged in the form of cone having shape of hollow truncated cone, which is flattened in transverse direction, along rectilinear geometric generatrices. Body comprises thin wall of permanent thickness, which is divided in transverse direction into trapezoidal hot wall, trapezoidal cold wall parallel to hot wall and two symmetrical side walls, which connect cold wall and hot wall by sides. Thin wall comprises solid internal surface having rounded sections with radius of curvature, which is at least equal to two thicknesses of thin wall. Thin wall is arranged from fire-resistant composite material created by reinforcing solid and crossing fibers from fire-resistant material, which are submerged in matrix from fire-resistant material. In other version trapezoidal walls have thickness that increases from side walls to central strip. In this version shutter comprises stiffening ribs, which are parallel to side walls that connect trapezoidal walls to each other and couple with them by means of rounded sections with curvature radius along internal surface, which is at least equal to double thickness of side walls. Method for manufacture of nozzle shutter comprises stages of single structure creation with solid edges from crossing fire resistant fibers, structure stretching around rigid, porous bent profiles opposite to each other and application of fire resistant matrix by means of deposition in steam-like phase onto structure and via profiles. Opposite bent profiles are arranged with prominences in diverging directions that have curvature radius, which is at least equal to double thickness of structure. In the other version nozzle shutter is made of several structures. Structures are arranged with sections overlapping each other, and matrix is solid and passes through mentioned sections that overlap each other.;EFFECT: increased strength of shutter, reduced heat transfer to its cold wall, possibility to reject air cooling of shutter between its walls.;12 cl, 16 dwg
机译:领域:航空和燃气涡轮发动机的喷嘴百叶窗以空心截锥形的圆锥形形式布置,该圆锥形沿直线几何形母线在横向方向上变平。主体包括具有永久厚度的薄壁,该薄壁在横向方向上被分为梯形热壁,与热壁平行的梯形冷壁和两个对称的侧壁,其将冷壁和热壁并排连接。薄壁包括固体内表面,该固体内表面具有曲率半径的圆形部分,该曲率半径至少等于薄壁的两个厚度。薄壁由耐火复合材料制成,该材料由耐火材料加固的实心纤维和交叉纤维制成,而耐火材料浸没在基质中。在其他版本中,梯形壁的厚度从侧壁到中心带增加。在该版本中,百叶窗包括平行于侧壁的加强肋,该加强肋将梯形壁彼此连接并通过具有沿着内表面的曲率半径的倒圆部分与它们耦合,该倒角部分至少等于侧壁的两倍厚度。制造喷嘴百叶窗的方法包括以下步骤:创建单个结构,该结构具有由耐火纤维交叉形成的实心边缘,围绕彼此相对的刚性,多孔弯曲轮廓拉伸的结构以及通过以蒸汽状相沉积到结构上来施加耐火基质的步骤以及通过个人资料。相反的弯曲轮廓在具有曲率半径的发散方向上突出设置,该曲率半径至少等于结构的两倍厚度。在另一个版本中,喷嘴百叶窗由几种结构制成。结构排列成彼此重叠的部分,矩阵是实心的,并穿过上述相互重叠的部分。效果:增加百叶窗的强度,减少向冷壁的热传递,有可能拒绝百叶窗在其壁之间的空气冷却。 ; 12 cl,16 dwg

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