[1] 吴志恩. 复合材料热隔膜成型[J]. 航空制造技术, 2009(25):113-116. [2] 匡载平, 戴棣, 王雪明. 热隔膜成型技术[C]//复合材料: 创新与可持续发展. 2010. [3] 陈亚莉. 复合材料成型工艺在A400M军用运输机上的应用[J]. 航空制造技术, 2008(10):32-35. [4] Monaghan M R, Mallon P J. High temperature mechanical characterisation of polyimide diaphragm forming films[J]. Composites Part A: Applied Science & Manufacturing, 1998, 29(3):265-272. [5] Gutowski T G, Dillon G, Chey S, et al. Laminate wrinkling scaling laws for ideal composites[J]. Composites Manufacturing, 1995, 6(3,4):123-134. [6] Bersee H E N, Beukers A. Diaphragm forming of continuous fibre reinforced thermoplastics: influence of temperature, pressure and forming velocity on the forming of Upilex-Rw diaphragms[J]. Composites Part A: Applied Science & Manufacturing, 2002, 33(7):949-958. [7] Delaloye S, Niedermeier M. Optimization of the diaphragm forming process for continuous fibre-reinforced advanced thermoplastic composites[J]. Composites Manufacturing, 1995, 6(3,4):135-144. [8] Keane M A, Mulhern M B, Mallon P J, et al. Investigation of the effects of varying the processing parameters in diaphragm forming of advanced thermoplastic composite laminates[J]. Composites Manufacturing, 1995, 6(3,4):145-152. [9] Krebs J, Friedrich K, Bhattacharyya D. A direct comparison of matched-die versus diaphragm forming[J]. Composites Part A: Applied Science & Manufacturing, 1998, 29(1):183-188. [10] Mallon P J, O'Brádaigh C M, Pipes R B. Polymeric diaphragm forming of complex-curvature thermoplastic composites[J]. Composites, 1989, 20(1):48-56. [11] Pantelakis S G, Baxevani E A. Optimization of the diaphragm forming process with regard to product quality and cost[J]. Composites Part A: Applied Science & Manufacturing, 2002, 33(4):459-470. [12] 边旭霞, 顾轶卓, 孙晶, 等. 热隔膜工艺温度与成型速率对C形复合材料成型质量的影响[J]. 玻璃钢/复合材料, 2013(5). [13] 姚双, 李敏, 顾轶卓, 等. 碳纤维复合材料C形结构热隔膜成型工艺[J]. 北京航空航天大学学报, 2013, 39(1):95-99. [14] Ersoy N, Potter K, Wisnom M R, et al. An experimental method to study the frictional processes during composites manufacturing[J]. Composites Part A:Applied Science & Manufacturing, 2005, 36(11):1536-1544. [15] Martin C J, Seferis J C, Wilhelm M A. Frictional resistance of ther-moset prepregs and its influence on honeycomb composite processing[J]. Composites Part A: Applied Science & Manufacturing, 1996, 27(10):943-951. [16] Maulik D, Karantza M, Spandou E, et al. On the Effect of Temperature on the Creep Behavior of Neat and Carbon Fiber Reinforced PEEK and Epoxy Resin[J]. Journal of Composite Materials, 1995, 29(3):372-387. |