title: Ð Ð°Ð·ÑÐ°Ð±Ð¾ÑÐºÐ° ÑÐ¸ÑÑÐ¾Ð²Ð¾Ð¹ Ð¼Ð¾Ð´ÐµÐ»Ð¸ ÑÐ°Ð²Ð½Ð¾Ð½Ð°Ð¿ÑÑÐ¶ÐµÐ½Ð½Ð¾Ð³Ð¾ Ð´Ð¸ÑÐºÐ°
title: Ð²ÑÐ¿ÑÑÐºÐ½Ð°Ñ ÐºÐ²Ð°Ð»Ð¸ÑÐ¸ÐºÐ°ÑÐ¸Ð¾Ð½Ð½Ð°Ñ ÑÐ°Ð±Ð¾ÑÐ° Ð¼Ð°Ð³Ð¸ÑÑÑÐ°
titleType: Subtitle
title: Development of a digital model of a uniform-stress spinning filamentary disk
Creators: name: Ð¡ÑÐ´Ð°ÐºÐ¾Ð², ÐÐ»Ð°Ð´Ð¸ÑÐ»Ð°Ð²
Publisher: name: Ð¡Ð°Ð½ÐºÑ-ÐÐµÑÐµÑÐ±ÑÑÐ³ÑÐºÐ¸Ð¹ Ð¿Ð¾Ð»Ð¸ÑÐµÑÐ½Ð¸ÑÐµÑÐºÐ¸Ð¹ ÑÐ½Ð¸Ð²ÐµÑÑÐ¸ÑÐµÑ ÐÐµÑÑÐ° ÐÐµÐ»Ð¸ÐºÐ¾Ð³Ð¾
Year: 2023
Subjects: ÐÐ¾Ð¼Ð¿Ð¾Ð·Ð¸ÑÐ¸Ð¾Ð½Ð½ÑÐµ Ð¼Ð°ÑÐµÑÐ¸Ð°Ð»Ñ Ð¿Ð¾Ð»Ð¸Ð¼ÐµÑÐ½ÑÐµ
ÐÐ¾Ð¼Ð¿ÑÑÑÐµÑÐ½Ð¾Ðµ Ð¼Ð¾Ð´ÐµÐ»Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ðµ
ÐÐ¸ÑÐºÐ¸
Ð¿ÑÐ¾ÐµÐºÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð¸Ðµ
ÑÑÐ°ÐµÐºÑÐ¾ÑÐ¸Ñ Ð°ÑÐ¼Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ñ
Ð½Ð°Ð¿ÑÑÐ¶ÐµÐ½Ð½Ð¾ Ð´ÐµÑÐ¾ÑÐ¼Ð¸ÑÐ¾Ð²Ð°Ð½Ð½Ð¾Ðµ ÑÐ¾ÑÑÐ¾ÑÐ½Ð¸Ðµ
Ð¿ÑÐ¾ÑÐ½Ð¾ÑÑÑ ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð¸
design
reinforcement path
stress-strain state
structural strength

description: Ð Ð°Ð±Ð¾ÑÐ° Ð¿Ð¾ÑÐ²ÑÑÐµÐ½Ð° Ð¼Ð°ÑÐµÐ¼Ð°ÑÐ¸ÑÐµÑÐºÐ¾Ð¼Ñ Ð¸ ÐºÐ¾Ð¼Ð¿ÑÑÑÐµÑÐ½Ð¾Ð¼Ñ Ð¼Ð¾Ð´ÐµÐ»Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ñ ÑÐ²Ð¾Ð¹ÑÑÐ² ÑÐ°Ð²Ð½Ð¾Ð¼ÐµÑÐ½Ð¾ Ð½Ð°Ð¿ÑÑÐ¶ÐµÐ½Ð½Ð¾Ð³Ð¾ Ð²ÑÐ°ÑÐ°ÑÑÐµÐ³Ð¾ÑÑ Ð´Ð¸ÑÐºÐ° Ð¸Ð· Ð²Ð¾Ð»Ð¾ÐºÐ½Ð¸ÑÑÐ¾Ð³Ð¾ Ð¿Ð¾Ð»Ð¸Ð¼ÐµÑÐ½Ð¾Ð³Ð¾ ÐºÐ¾Ð¼Ð¿Ð¾Ð·Ð¸ÑÐ¸Ð¾Ð½Ð½Ð¾Ð³Ð¾ Ð¼Ð°ÑÐµÑÐ¸Ð°Ð»Ð°, Ð¿Ð¾Ð»ÑÑÐµÐ½Ð½Ð¾Ð³Ð¾ Ð¼ÐµÑÐ¾Ð´Ð¾Ð¼ Ð½Ð°Ð¼Ð¾ÑÐºÐ¸. ÐÐ±ÑÐµÐºÑ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ - ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ñ ÑÐ°Ð²Ð½Ð¾Ð½Ð°Ð¿ÑÑÐ¶ÐµÐ½Ð½Ð¾Ð³Ð¾ Ð´Ð¸ÑÐºÐ° Ð¸Ð· Ð²Ð¾Ð»Ð¾ÐºÐ½Ð¸ÑÑÑÑ Ð¿Ð¾Ð»Ð¸Ð¼ÐµÑÐ½ÑÑ ÐºÐ¾Ð¼Ð¿Ð¾Ð·Ð¸ÑÐ¸Ð¾Ð½Ð½ÑÑ Ð¼Ð°ÑÐµÑÐ¸Ð°Ð»Ð¾Ð² (Ð ÐÐ Ð¸Ð· ÐÐÐÐ). Ð¦ÐµÐ»Ñ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ - ÑÐ°Ð·ÑÐ°Ð±Ð¾ÑÐºÐ° ÑÐ¸ÑÑÐ¾Ð²Ð¾Ð¹ Ð¼Ð¾Ð´ÐµÐ»Ð¸ Ð ÐÐ Ð¸Ð· ÐÐÐÐ, Ð¿Ð¾Ð·Ð²Ð¾Ð»ÑÑÑÐµÐ¹ Ð¿ÑÐ¾Ð²Ð¾Ð´Ð¸ÑÑ ÑÐ°ÑÑÐµÑÑ Ð¼Ð°ÑÐ¾Ð²Ð¸ÐºÐ°. ÐÐµÑÐ¾Ð´Ñ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ â Ð°Ð½Ð°Ð»Ð¸ÑÐ¸ÑÐµÑÐºÐ¸Ð¹ Ð¸ ÐºÐ¾Ð½ÐµÑÐ½Ð¾ÑÐ»ÐµÐ¼ÐµÐ½ÑÐ½ÑÐ¹ Ð°Ð½Ð°Ð»Ð¸Ð· Ð½Ð°Ð¿ÑÑÐ¶ÐµÐ½Ð½Ð¾-Ð´ÐµÑÐ¾ÑÐ¼Ð¸ÑÐ¾Ð²Ð°Ð½Ð½Ð¾Ð³Ð¾ ÑÐ¾ÑÑÐ¾ÑÐ½Ð¸Ñ, Ð°Ð½Ð°Ð»Ð¸ÑÐ¸ÑÐµÑÐºÐ¾Ðµ Ð¸ ÑÐ¸ÑÐ»ÐµÐ½Ð½Ð¾Ðµ Ð¼Ð¾Ð´ÐµÐ»Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ðµ ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð¸ Ð¸ ÑÐ²Ð¾Ð¹ÑÑÐ² ÑÐ°Ð²Ð½Ð¾Ð½Ð°Ð¿ÑÑÐ¶ÐµÐ½Ð½Ð¾Ð¹ ÑÑÑÑÐºÑÑÑÑ ÐºÐ¾Ð¼Ð¿Ð¾Ð·Ð¸ÑÐ¸Ð¾Ð½Ð½Ð¾Ð³Ð¾ Ð¼Ð°ÑÐµÑÐ¸Ð°Ð»Ð° Ð² ÑÐ¾ÑÑÐ°Ð²Ðµ Ð´Ð¸ÑÐºÐ° Ñ ÑÑÐµÑÐ¾Ð¼ ÑÑÐ°ÐµÐºÑÐ¾ÑÐ¸Ð¸ Ð°ÑÐ¼Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ñ Ð¸ ÑÐ¾ÑÐ¼Ð¾Ð¾Ð±ÑÐ°Ð·Ð¾Ð²Ð°Ð½Ð¸Ñ. ÐÐ°ÑÑÐ½Ð°Ñ Ð½Ð¾Ð²Ð¸Ð·Ð½Ð° Ð·Ð°ÐºÐ»ÑÑÐ°ÐµÑÑÑ Ð² ÑÐ°Ð·ÑÐ°Ð±Ð¾ÑÐºÐµ ÑÐ°ÑÑÐµÑÐ½Ð¾Ð¹ Ð¼ÐµÑÐ¾Ð´Ð¸ÐºÐ¸, Ð¾ÑÐ½Ð¾Ð²Ð°Ð½Ð½Ð¾Ð¹ Ð½Ð° ÑÐ¾Ð²ÑÐµÐ¼ÐµÐ½Ð½ÑÑ ÑÐ¸ÑÐ»ÐµÐ½Ð½ÑÑ Ð¿Ð¾Ð´ÑÐ¾Ð´Ð°Ñ, Ñ Ð¿Ð¾Ð¼Ð¾ÑÑÑ ÐºÐ¾ÑÐ¾ÑÐ¾Ð¹ Ð¼Ð¾Ð¶Ð½Ð¾ Ð¿ÑÐ¾ÐµÐºÑÐ¸ÑÐ¾Ð²Ð°ÑÑ ÑÑÑÑÐºÑÑÑÑ Ð¸ ÑÐ²Ð¾Ð¹ÑÑÐ²Ð° Ð²ÑÑÐ¾ÐºÐ¾ÑÑÑÐµÐºÑÐ¸Ð²Ð½ÑÑ ÐºÐ¸Ð½ÐµÑÐ¸ÑÐµÑÐºÐ¸Ñ Ð½Ð°ÐºÐ¾Ð¿Ð¸ÑÐµÐ»ÐµÐ¹ ÑÐ½ÐµÑÐ³Ð¸Ð¸ Ð¸Ð· ÐÐÐÐ Ð´Ð»Ñ ÐºÐ¾ÑÐ¼Ð¸ÑÐµÑÐºÐ¾Ð³Ð¾ Ð½Ð°Ð·Ð½Ð°ÑÐµÐ½Ð¸Ñ. Ð ÑÐ°Ð¼ÐºÐ°Ñ Ð´Ð°Ð½Ð½Ð¾Ð¹ ÑÐ°Ð±Ð¾ÑÑ ÑÐ°Ð·ÑÐ°Ð±Ð¾ÑÐ°Ð½Ð° ÑÐ°ÑÑÑ ÑÐ°ÑÑÐµÑÐ½Ð¾Ð¹ Ð¼ÐµÑÐ¾Ð´Ð¸ÐºÐ¸ Ð¸ Ð´Ð¾ÑÑÐ¸Ð³Ð½ÑÑÑ ÑÐ»ÐµÐ´ÑÑÑÐ¸Ðµ ÐºÐ»ÑÑÐµÐ²ÑÐµ ÑÐµÐ·ÑÐ»ÑÑÐ°ÑÑ: - ÑÐ°Ð·ÑÐ°Ð±Ð¾ÑÐ°Ð½Ñ Ð¼Ð°ÑÐµÐ¼Ð°ÑÐ¸ÑÐµÑÐºÐ¸Ðµ Ð¼Ð¾Ð´ÐµÐ»Ð¸, Ð¾Ð±ÐµÑÐ¿ÐµÑÐ¸Ð²Ð°ÑÑÐ¸Ðµ ÑÐ²ÑÐ·Ñ ÑÐµÑÐ½Ð¾Ð»Ð¾Ð³Ð¸ÑÐµÑÐºÐ¸Ñ Ð¿Ð°ÑÐ°Ð¼ÐµÑÑÐ¾Ð² Ð½Ð°Ð¼Ð¾ÑÐºÐ¸, ÑÐ¾ÑÐ¼Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ñ ÑÑÑÑÐºÑÑÑÑ Ð¼Ð°ÑÐµÑÐ¸Ð°Ð»Ð°, Ð¸, ÐºÐ°Ðº ÑÐ»ÐµÐ´ÑÑÐ²Ð¸Ðµ, Ð¿ÑÐ¾ÑÐ½Ð¾ÑÑÐ½ÑÑ ÑÐ²Ð¾Ð¹ÑÑÐ² ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð¸; - ÑÐ°Ð·ÑÐ°Ð±Ð¾ÑÐ°Ð½Ð° Ð¿ÑÐ¾ÑÐµÐ´ÑÑÐ° Ð°Ð²ÑÐ¾Ð¼Ð°ÑÐ¸Ð·Ð¸ÑÐ¾Ð²Ð°Ð½Ð½Ð¾Ð³Ð¾ Ð¿Ð¾ÑÑÑÐ¾ÐµÐ½Ð¸Ñ Ð¼Ð¾Ð´ÐµÐ»Ð¸ Ð ÐÐ Ð² Ð¿ÑÐ¾Ð³ÑÐ°Ð¼Ð¼Ð½Ð¾Ð¹ ÑÐ¸ÑÑÐµÐ¼Ðµ ANSYS Composite PrepPost; - Ð¿ÑÐ¾Ð²ÐµÐ´ÐµÐ½Ð° Ð²ÐµÑÐ¸ÑÐ¸ÐºÐ°ÑÐ¸Ñ ÑÐ¿Ð¾ÑÐ¾Ð±Ð° Ð¼Ð¾Ð´ÐµÐ»Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ñ ÑÑÑÑÐºÑÑÑÑ ÐÐÐÐ ÑÐµÑÐµÐ· ÑÐµÐ°Ð»Ð¸Ð·Ð°ÑÐ¸Ñ Ð°Ð½Ð°Ð»Ð¸ÑÐ¸ÑÐµÑÐºÐ¾Ð³Ð¾ ÑÐ°ÑÑÐµÑÐ° Ð¿Ð¾ Ð¾Ð¿ÑÐµÐ´ÐµÐ»ÐµÐ½Ð¸Ñ ÐºÐ¾Ð¼Ð¿Ð¾Ð½ÐµÐ½Ñ Ð½Ð°Ð¿ÑÑÐ¶ÐµÐ½Ð½Ð¾-Ð´ÐµÑÐ¾ÑÐ¼Ð¸ÑÐ¾Ð²Ð°Ð½Ð½Ð¾Ð³Ð¾ ÑÐ¾ÑÑÐ¾ÑÐ½Ð¸Ñ; - ÑÐ°Ð·ÑÐ°Ð±Ð¾ÑÐ°Ð½Ð° ÑÐ¸ÑÑÐ¾Ð²Ð°Ñ Ð¼Ð¾Ð´ÐµÐ»Ñ Ð ÐÐ, Ð¸ Ð¿ÑÐ¾Ð¸Ð·Ð²ÐµÐ´ÐµÐ½ ÑÐ°ÑÑÐµÑ Ð¿ÑÐµÐ´ÐµÐ»ÑÐ½Ð¾Ð¹ ÑÐºÐ¾ÑÐ¾ÑÑÐ¸ Ð²ÑÐ°ÑÐµÐ½Ð¸Ñ ÑÐµÑÐµÐ· ÐºÑÐ¸ÑÐµÑÐ¸Ð¸ ÑÐ°Ð·ÑÑÑÐµÐ½Ð¸Ñ Ð¿Ð¾ Ð¼Ð°ÐºÑÐ¸Ð¼Ð°Ð»ÑÐ½ÑÐ¼ Ð½Ð°Ð¿ÑÑÐ¶ÐµÐ½Ð¸ÑÐ¼; - Ð¿ÑÐ¾Ð²ÐµÐ´ÐµÐ½ ÑÐ°ÑÑÐµÑ Ð¸ ÑÑÐ°Ð²Ð½Ð¸ÑÐµÐ»ÑÐ½ÑÐ¹ Ð°Ð½Ð°Ð»Ð¸Ð· ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð¹ Ð ÐÐ Ð¸Ð· ÐÐÐÐ Ð¸ Ð¼ÐµÑÐ°Ð»Ð»Ð° Ð´Ð»Ñ Ð¾Ð±Ð¾ÑÐ½Ð¾Ð²Ð°Ð½Ð¸Ñ ÑÐ°Ð±Ð¾ÑÐ¾ÑÐ¿Ð¾ÑÐ¾Ð±Ð½Ð¾ÑÑÐ¸ ÑÐ°ÑÑÐµÑÐ½Ð¾Ð¹ Ð¼ÐµÑÐ¾Ð´Ð¸ÐºÐ¸ Ð² Ð·Ð°Ð´Ð°ÑÐµ Ð¿ÑÐ¾ÐµÐºÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð¸Ñ; - Ð¿Ð¾Ð»ÑÑÐµÐ½Ñ ÑÐµÐ·ÑÐ»ÑÑÐ°ÑÑ Ð¼Ð°ÑÑÐ¾-ÑÐ½ÐµÑÐ³ÐµÑÐ¸ÑÐµÑÐºÐ¾Ð³Ð¾ ÑÐ¾Ð²ÐµÑÑÐµÐ½ÑÑÐ²Ð° ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð¸ Ð ÐÐ Ð¸Ð· ÐÐÐÐ Ð¿Ð¾ ÑÑÐ°Ð²Ð½ÐµÐ½Ð¸Ñ Ñ Ð°Ð½Ð°Ð»Ð¾Ð³Ð¸ÑÐ½ÑÐ¼ Ð¿Ð¾ Ð¼Ð°ÑÑÐµ Ð¼ÐµÑÐ°Ð»Ð»Ð¸ÑÐµÑÐºÐ¸Ð¼ Ð´Ð¸ÑÐºÐ¾Ð¼. ÐÐ±Ð»Ð°ÑÑÑ Ð¿ÑÐ¸Ð¼ÐµÐ½ÐµÐ½Ð¸Ñ â Ð¿Ð¾Ð»ÑÑÐµÐ½Ð½ÑÐµ ÑÐµÐ·ÑÐ»ÑÑÐ°ÑÑ Ð¼Ð¾Ð¶Ð½Ð¾ Ð¿ÑÐ¸Ð¼ÐµÐ½ÑÑÑ ÐºÐ°Ðº ÑÐ°ÑÑÐµÑÐ½ÑÑ Ð¾ÑÐ½Ð¾Ð²Ñ Ð¸ Ð¼ÐµÑÐ¾Ð´Ð¸ÐºÑ Ð¿ÑÐ¸ Ð¿ÑÐ¾ÐµÐºÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð¸Ð¸ Ð¼ÐµÑÐ°Ð½Ð¸ÑÐµÑÐºÐ¸Ñ ÐºÐ¸Ð½ÐµÑÐ¸ÑÐµÑÐºÐ¸Ñ Ð±Ð¾ÑÑÐ¾Ð²ÑÑ Ð¸ÑÑÐ¾ÑÐ½Ð¸ÐºÐ¾Ð² Ð¿Ð¸ÑÐ°Ð½Ð¸Ñ Ð´Ð»Ñ ÐºÐ¾ÑÐ¼Ð¸ÑÐµÑÐºÐ¸Ñ Ð°Ð¿Ð¿Ð°ÑÐ°ÑÐ¾Ð² (ÐÐ) Ñ Ð·Ð°Ð´Ð°Ð½Ð½ÑÐ¼Ð¸ Ð³Ð°Ð±Ð°ÑÐ¸ÑÐ°Ð¼Ð¸ Ð¿Ð¾ ÐºÐ¾Ð¼Ð¿Ð¾Ð½Ð¾Ð²Ð¾ÑÐ½Ð¾Ð¹ ÑÑÐµÐ¼Ðµ ÐÐ. ÐÐ»Ñ Ð²Ð½ÐµÐ´ÑÐµÐ½Ð¸Ñ ÑÐ°Ð·ÑÐ°Ð±Ð¾ÑÐºÐ¸ Ð½ÐµÐ¾Ð±ÑÐ¾Ð´Ð¸Ð¼Ð¾ Ð¿ÑÐ¾Ð²ÐµÑÑÐ¸ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ðµ Ð¸ Ð¿Ð¾Ð¸ÑÐº Ð²Ð¾Ð·Ð¼Ð¾Ð¶Ð½Ð¾Ð¹ ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð¸ Ð¾Ð¿ÑÐ°Ð²ÐºÐ¸ Ð´Ð»Ñ ÑÑÐ¾ÑÐ½ÐµÐ½Ð¸Ñ Ð¼Ð°ÑÐµÐ¼Ð°ÑÐ¸ÑÐµÑÐºÐ¸Ñ Ð¸ ÐºÐ¾Ð¼Ð¿ÑÑÑÐµÑÐ½ÑÑ Ð¼Ð¾Ð´ÐµÐ»ÐµÐ¹, Ð° ÑÐ°ÐºÐ¶Ðµ Ð¿ÑÐ¾Ð²ÐµÑÑÐ¸ Ð²Ð°Ð»Ð¸Ð´Ð°ÑÐ¸Ñ ÑÐ¸ÑÑÐ¾Ð²Ð¾Ð¹ Ð¼Ð¾Ð´ÐµÐ»Ð¸ Ð ÐÐ. Ð­ÐºÐ¾Ð½Ð¾Ð¼Ð¸ÑÐµÑÐºÐ°Ñ ÑÑÑÐµÐºÑÐ¸Ð²Ð½Ð¾ÑÑÑ Ð¿Ð¾Ð»ÑÑÐ°ÐµÐ¼Ð¾Ð¹ ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð¸ Ð ÐÐ Ð¸Ð· ÐÐÐÐ Ð² ÑÐ¾ÑÑÐ°Ð²Ðµ Ð±Ð¾ÑÑÐ¾Ð²Ð¾Ð³Ð¾ Ð¸ÑÑÐ¾ÑÐ½Ð¸ÐºÐ° Ð¿Ð¸ÑÐ°Ð½Ð¸Ñ Ð·Ð°ÐºÐ»ÑÑÐ°ÐµÑÑÑ Ð² Ð´Ð¾ÑÑÐ¸Ð¶ÐµÐ½Ð¸Ð¸ Ð¼Ð°ÑÑÐ¾-ÑÐ½ÐµÑÐ³ÐµÑÐ¸ÑÐµÑÐºÐ¾Ð³Ð¾ ÑÐ¾Ð²ÐµÑÑÐµÐ½ÑÑÐ²Ð°, Ð² ÑÐµÐ·ÑÐ»ÑÑÐ°ÑÐµ ÐºÐ¾ÑÐ¾ÑÐ¾Ð³Ð¾ Ð¾Ð±ÐµÑÐ¿ÐµÑÐ¸Ð²Ð°ÐµÑÑÑ Ð½Ðµ ÑÐ¾Ð»ÑÐºÐ¾ ÑÐ½ÐµÑÐ³ÐµÑÐ¸ÑÐµÑÐºÐ°Ñ ÑÑÑÐµÐºÑÐ¸Ð²Ð½Ð¾ÑÑÑ, Ð° ÑÐ°Ðº Ð¶Ðµ Ð¾Ð±ÐµÑÐ¿ÐµÑÐ¸Ð²Ð°ÐµÑÑÑ Ð½Ð¸Ð·ÐºÐ°Ñ ÑÑÐ¾Ð¸Ð¼Ð¾ÑÑÑ Ð²ÑÐ²Ð¾Ð´Ð° Ð¿Ð¾Ð»ÐµÐ·Ð½Ð¾Ð¹ Ð½Ð°Ð³ÑÑÐ·ÐºÐ¸ Ð² ÐºÐ¾ÑÐ¼Ð¸ÑÐµÑÐºÐ¾Ðµ Ð¿ÑÐ¾ÑÑÑÐ°Ð½ÑÑÐ²Ð¾. Ð Ð°Ð·Ð²Ð¸ÑÐ¸ÐµÐ¼ Ð½Ð°ÑÑÐ¾ÑÑÐµÐ¹ ÑÐ°Ð±Ð¾ÑÑ Ð¼Ð¾Ð¶Ð½Ð¾ Ð½Ð°Ð·Ð²Ð°ÑÑ Ð¿Ð¾Ð¸ÑÐº Ð²Ð¾Ð·Ð¼Ð¾Ð¶Ð½Ð¾Ð¹ ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð¸ Ð¾Ð¿ÑÐ°Ð²ÐºÐ¸ Ð´Ð»Ñ Ð½Ð°Ð¼Ð¾ÑÐºÐ¸ Ð² ÑÐµÐ»ÑÑ ÑÑÐ¾ÑÐ½ÐµÐ½Ð¸Ñ ÑÐ¾ÑÐ¼Ñ ÑÐ°ÑÐ¿ÑÐµÐ´ÐµÐ»ÐµÐ½Ð¸Ñ ÑÐ¾Ð»ÑÐ¸Ð½Ñ Ð²Ð±Ð»Ð¸Ð·Ð¸ Ð²Ð½ÑÑÑÐµÐ½Ð½ÐµÐ¹ Ð¸ Ð½Ð°ÑÑÐ¶Ð½Ð¾Ð¹ Ð³ÑÐ°Ð½Ð¸ Ð ÐÐ, Ð° ÑÐ°ÐºÐ¶Ðµ ÑÑÐ¾ÑÐ½ÐµÐ½Ð¸Ðµ ÑÑÐ°ÐµÐºÑÐ¾ÑÐ¸Ð¸ Ð°ÑÐ¼Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ñ Ð´Ð»Ñ Ð´Ð¾ÑÑÐ¸Ð¶ÐµÐ½Ð¸Ñ Ð±Ð¾Ð»ÐµÐµ ÑÐ°Ð²Ð½Ð¾Ð¼ÐµÑÐ½Ð¾Ð¹ ÑÐ°Ð²Ð½Ð¾Ð½Ð°Ð¿ÑÑÐ¶ÐµÐ½Ð½Ð¾ÑÑÐ¸ Ð¸ ÑÑÐ¸Ð»ÐµÐ½Ð¸Ñ Ð¼Ð°ÑÑÐ¸ÑÐ½Ð¾Ð³Ð¾ Ð½Ð°Ð¿ÑÐ°Ð²Ð»ÐµÐ½Ð¸Ñ.
description: The paper is devoted to mathematical and computer modelling of the properties of a uniform-stress spinning filamentary disk, which is made of a fibrous polymer composite material obtained by winding. The object of research is the design of an uniform-stress spinning filamentary disk made of fibrous polymer composite materials (USSFD) from FPCM). The purpose of the study is to develop a digital model of the USSFD from the FPCM, which makes it possible to do flywheel calculations. Current methods â analytical and finite element analysis of the stress-strain state, analytical and numerical modeling of the design and properties of the uniform stress structure of the composite material in the disk considering to the trajectory of reinforcement and shaping. The scientific novelty is the development of a computational technique based on modern numerical approaches, with the help of which it is possible to design the structures and properties of highly efficient kinetic energy storage from FPCM for space purposes.Â As part of this work, a part of the calculation methodology was developed and the following key results were achieved: - mathematical models have been developed that provide a link between the technological parameters of winding, the formation of the material structure, and, as a result, the strength properties of the structure; - a procedure for the automated construction of an USSFD model in the ANSYS Composite PrepPost software system have been developed; - verification of the method for modeling the structure of the FPCM through the realisation of an analytical calculation to determine the components of the stress-strain state; - a digital model of USSFD was developed, and the calculation of the limiting rotation speed was made through the failure criteria for maximum stresses; - calculation and comparative analysis of USSFD structures made of FPCM and metal for substantiate the efficiency of the calculation technique in the design problem; - the results of the mass-energy perfection of the USSFD design from FPCM in comparison with a metal disk of the same mass were obtained. Scope - the results obtained can be used as a calculation basis and methodology for the design of mechanical kinetic onboard power sources for spacecraft (SC) with specified dimensions according to the SC layout. To implement the development, it is necessary to conduct a investigation and search for a possible design of the mandrel to clarify mathematical and computer models, as well as to validate the digital model of the USSFD. The economic efficiency of the USSFD design obtained from FPCM as part of an onboard power source is to achieve mass and energy perfection, which results in not only energy efficiency, but also low cost of launching the payload into outer space. The extension of this work can be called the search for a possible design of the mandrel for winding in order to clarify the shape of the thickness distribution near the inner and outer faces of the USSFD, as well as the refinement of the reinforcement trajectory to achieve a more uniform uniform tension and enhance the matrix direction.