The invention provides a heat-proof integrated aircraft rudder wing and an additive manufacturing method thereof. The aircraft rudder wing comprises a front cone, a gradient transition area, a rudder wing surface and a rudder wing shaft. The manufacturing method comprises the following steps: (1) carrying out laser melting deposition on the titanium alloy rudder airfoil, the airfoil cover plate and the rudder shaft; (2) welding the wing surface cover plate on the rudder wing cooling flow channel by adopting a welding technology; (3) titanium alloy/high-temperature alloy gradient transition area laser melting deposition forming is carried out on the basis of the titanium alloy rudder airfoil; (4) selective laser melting forming of a rudder wing front cone structure powder bed; (5) welding the front cone of the rudder wing to the gradient transition area to form a rudder wing blank; and (6) the welded rudder wing blank is subjected to post-treatment procedures such as overall heat treatment and machining. According to the invention, an additive manufacturing method is adopted, so that the integrated manufacturing of the material/structure/function of the rudder wing of the ultra-high-speed aircraft can be realized.
本发明提供了一种防热一体化飞行器舵翼及其增材制造方法,飞行器舵翼包括:前锥体、梯度过渡区、舵翼翼面和舵翼轴。制造方法包括如下步骤:(1)钛合金舵翼面、翼面盖板和舵轴激光熔化沉积;(2)采用焊接技术将翼面盖板焊接于舵翼冷却流道;(3)以钛合金舵翼面为基础开展钛合金/高温合金梯度过渡区激光熔化沉积成形;(4)舵翼前锥体结构粉末床激光选区熔化成形;(5)将舵翼前锥体焊接于梯度过渡区部位形成舵翼毛胚;(6)将焊接后的舵翼毛胚进行整体热处理、机加工等后处理工序。本发明专利采用增材制造方法,可实现超高速飞行器舵翼材料/结构/功能的一体化制造。
Heat-proof integrated aircraft rudder wing and additive manufacturing method thereof
防热一体化飞行器舵翼及其增材制造方法
2024-01-26
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge / B22F Verarbeiten von Metallpulver , WORKING METALLIC POWDER / B33Y ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING , Additive (generative) Fertigung, d. h. die Herstellung von dreidimensionalen [3D] Bauteilen durch additive Abscheidung, additive Agglomeration oder additive Schichtung, z. B. durch 3D- Drucken, Stereolithografie oder selektives Lasersintern / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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