首页> 外国专利> METHODS FOR ADDITIVELY MANUFACTURING TURBINE ENGINE COMPONENTS VIA BINDER JET PRINTING WITH NICKEL-CHROMIUM-TUNGSTEN-MOLYBDENUM ALLOYS

METHODS FOR ADDITIVELY MANUFACTURING TURBINE ENGINE COMPONENTS VIA BINDER JET PRINTING WITH NICKEL-CHROMIUM-TUNGSTEN-MOLYBDENUM ALLOYS

机译:通过镍-铬-钨-钼合金粘合剂射流印刷法制造涡轮发动机成分的方法

摘要

Methods for manufacturing an article include providing a three-dimensional computer model of the article and providing a metal alloy in powdered form. The metal alloy is a nickel-chromium-tungsten-molybdenum alloy. The powdered form includes a grain size range of about 5 to about 22 microns and a d50 grain size average of about 10 to about 13 microns. The methods further include, at a binder jet printing apparatus, supplying the metal alloy and loading the three-dimensional model, and, using the binder jet printing apparatus, manufacturing the article in accordance with the loaded three-dimensional model in a layer-by-layer manner with the supplied metal alloy. A liquid binder is applied at each layer, and each layer has a thickness of about 10 to about 150 microns. The methods avoid remelting of the metal alloy and avoid metal alloy cooling rates of greater than about 100° F. per minute.
机译:制造物品的方法包括提供物品的三维计算机模型和提供粉末形式的金属合金。该金属合金是镍铬钨钼合金。粉末形式包括约5至约22微米的粒度范围和约10至约13微米的d50粒度平均值。所述方法还包括:在粘合剂喷射印刷设备处,供应金属合金并加载三维模型;以及,使用粘合剂喷射印刷设备,根据加载的三维模型来逐层制造物品。所提供的金属合金的分层方法。将液体粘合剂施加在每一层上,并且每一层具有约10至约150微米的厚度。该方法避免了金属合金的重熔并且避免了金属合金的冷却速率大于每分钟约100°F。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号