title: ÐÐ²ÑÑ ÐºÐ¾Ð½ÑÑÑÐ½ÑÐ¹ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ ÑÑÐ³Ð¾Ð¹ 110 ÐºÐ
title: Ð²ÑÐ¿ÑÑÐºÐ½Ð°Ñ ÐºÐ²Ð°Ð»Ð¸ÑÐ¸ÐºÐ°ÑÐ¸Ð¾Ð½Ð½Ð°Ñ ÑÐ°Ð±Ð¾ÑÐ° Ð±Ð°ÐºÐ°Ð»Ð°Ð²ÑÐ°
titleType: Subtitle
title: High-bypass turbofan aircraft engine with a thrust of 110 kn
Creators: name: ÐÐ°Ð±Ð¾Ð²ÑÐºÐ¸Ð¹, ÐÐ¾Ð³Ð´Ð°Ð½
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: 2020
Subjects: Ð´Ð²ÑÑ ÐºÐ¾Ð½ÑÑÑÐ½ÑÐ¹ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ
Ð¿ÑÐ¾ÑÐ¾ÑÐ¸Ð¿ cfm56
Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ð¿Ð°ÑÑÐ°Ð¶Ð¸ÑÑÐºÐ¾Ð³Ð¾ ÑÐ°Ð¼Ð¾Ð»ÑÑÐ° Ñ Ð²ÑÑÐ¾ÐºÐ¾Ð¹ ÑÑÐµÐ¿ÐµÐ½ÑÑ Ð´Ð²ÑÑ ÐºÐ¾Ð½ÑÑÑÐ½Ð¾ÑÑÐ¸
turbofan engine
prototype cfm56
high-bypass civil aircraft engine

description: ÐÑÐµÐ´ÑÑÐ°Ð²Ð»ÐµÐ½Ð½Ð°Ñ ÑÐ°Ð±Ð¾ÑÐ° Ð¿Ð¾ÑÐ²ÑÑÐµÐ½Ð° Ð¿ÑÐ¾ÐµÐºÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð¸Ñ Ð°Ð²Ð¸Ð°ÑÐ¸Ð¾Ð½Ð½Ð¾Ð³Ð¾ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ð´Ð»Ñ ÑÑÐµÐ´Ð½ÐµÐ¼Ð°Ð³Ð¸ÑÑÑÐ°Ð»ÑÐ½Ð¾Ð³Ð¾ ÑÐ°Ð¼Ð¾Ð»ÐµÑÐ° Ð½Ð° Ð¾ÑÐ½Ð¾Ð²Ðµ Ð¿ÑÐ¾ÑÐ¾ÑÐ¸Ð¿Ð° CFM56. ÐÑÐ½Ð¾Ð²Ð½ÑÐ¼Ð¸ Ð¿Ð°ÑÐ°Ð¼ÐµÑÑÐ°Ð¼Ð¸, Ð² Ð±Ð¾Ð»ÑÑÐµÐ¹ ÑÑÐµÐ¿ÐµÐ½Ð¸ Ð¾ÐºÐ°Ð·ÑÐ²Ð°ÑÑÐ¸Ð¼Ð¸ Ð²Ð»Ð¸ÑÐ½Ð¸Ðµ Ð½Ð° Ð¿ÑÐµÐ´ÑÑÐ°Ð²Ð»ÐµÐ½Ð½ÑÐ¹ ÑÐ°ÑÑÑÑ, Ð²ÑÑÑÑÐ¿Ð°ÑÑ: ÑÐµÐ¼Ð¿ÐµÑÐ°ÑÑÑÐ° Ð¿ÐµÑÐµÐ´ ÑÑÑÐ±Ð¸Ð½Ð¾Ð¹ Ð²ÑÑÐ¾ÐºÐ¾Ð³Ð¾ Ð´Ð°Ð²Ð»ÐµÐ½Ð¸Ñ; ÑÑÐµÐ¿ÐµÐ½Ñ Ð´Ð²ÑÑÐºÐ¾Ð½ÑÑÑÐ½Ð¾ÑÑÐ¸; ÑÑÐ³Ð° Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ. ÐÐ°Ð´Ð°ÑÐ¸, ÐºÐ¾ÑÐ¾ÑÑÐµ ÑÐµÑÐ°ÑÑÑÑ Ð² ÑÐ¾Ð´Ðµ Ð´Ð°Ð½Ð½Ð¾Ð³Ð¾ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ: 1. ÐÐ·ÑÑÐµÐ½Ð¸Ðµ Ð¾ÑÐ¾Ð±ÐµÐ½Ð½Ð¾ÑÑÐµÐ¹ ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð¸ Ð¿ÑÐ¾ÑÐ¾ÑÐ¸Ð¿Ð° Ð°Ð²Ð¸Ð°Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ CFM56. 2. ÐÑÐ¾Ð²ÐµÐ´ÐµÐ½Ð¸Ðµ Ð²Ð°ÑÐ¸Ð°Ð½ÑÐ½Ð¾Ð³Ð¾ ÑÐµÐ¿Ð»Ð¾Ð²Ð¾Ð³Ð¾ ÑÐ°ÑÑÑÑÐ° ÑÐ¸ÐºÐ»Ð° Ð³Ð°Ð·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½Ð¾Ð³Ð¾ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ñ Ð²ÑÐ±Ð¾ÑÐ¾Ð¼ Ð¾Ð¿ÑÐ¸Ð¼Ð°Ð»ÑÐ½Ð¾Ð³Ð¾ Ð²Ð°ÑÐ¸Ð°Ð½ÑÐ°. 3. ÐÐ½Ð°Ð»Ð¸Ð· Ð´Ð°Ð½Ð½ÑÑ Ð¾ÑÐ´ÐµÐ»ÑÐ½ÑÑ ÑÐ·Ð»Ð¾Ð² Ð³Ð°Ð·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½Ð¾Ð³Ð¾ Ð´Ð²ÑÑÐºÐ¾Ð½ÑÑÑÐ½Ð¾Ð³Ð¾ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ñ Ð¿Ð¾Ð¼Ð¾ÑÑÑ Ð³Ð°Ð·Ð¾Ð´Ð¸Ð½Ð°Ð¼Ð¸ÑÐµÑÐºÐ¸Ñ Ð¸ ÑÐ°ÑÑÑÑÐ¾Ð² ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ°, ÐºÐ°Ð¼ÐµÑÑ ÑÐ³Ð¾ÑÐ°Ð½Ð¸Ñ Ð¸ ÑÑÑÐ±Ð¸Ð½Ñ. 4. ÐÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ðµ Ð¿ÑÐ¾ÑÐ½Ð¾ÑÑÐ¸ Ð»Ð¾Ð¿Ð°ÑÐºÐ¸, Ð´Ð¸ÑÐºÐ° Ð¸ ÑÐ¾ÑÐ¾ÑÐ° Ð¿Ð¾ÑÐ»ÐµÐ´Ð½ÐµÐ¹ ÑÑÑÐ¿ÐµÐ½Ð¸ Ð¿ÑÐµÐ´ÑÑÐ°Ð²Ð»ÐµÐ½Ð½Ð¾Ð¹ ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð¸. Ð Ð°Ð±Ð¾ÑÐ° ÑÐ²Ð»ÑÐµÑÑÑ Ð°ÐºÑÑÐ°Ð»ÑÐ½Ð¾Ð¹ Ð¸Ð·-Ð·Ð° ÑÐ¾Ð³Ð¾, ÑÑÐ¾ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ð¸ CFM56 Ð¸ÑÐ¿Ð¾Ð»ÑÐ·ÑÑÑÑÑ Ð½Ð° Ð¿Ð°ÑÑÐ°Ð¶Ð¸ÑÑÐºÐ¸Ñ ÑÐ°Ð¼Ð¾Ð»ÐµÑÐ°Ñ (Ð½Ð°Ð¿ÑÐ¸Ð¼ÐµÑ: Airbus A320, Boeing 737 Ð½Ð¾Ð²Ð¾Ð³Ð¾ Ð¿Ð¾ÐºÐ¾Ð»ÐµÐ½Ð¸Ñ), Ð° ÑÐ°ÐºÐ¶Ðµ Ð½Ð° Ð±Ð°Ð·Ðµ Ð´Ð°Ð½Ð½Ð¾Ð³Ð¾ Ð¿ÑÐ¾ÑÐ¾ÑÐ¸Ð¿Ð° ÑÐ¾Ð·Ð´Ð°ÑÑÑÑ Ð´ÑÑÐ³Ð¸Ðµ Ð¼Ð¾Ð´ÐµÐ»Ð¸ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»ÐµÐ¹, ÐºÐ¾ÑÐ¾ÑÑÐµ Ð¿ÑÐ¸Ð¼ÐµÐ½ÑÑÑÑÑ Ð½Ð° ÑÐ°Ð·Ð»Ð¸ÑÐ½ÑÑ ÑÐ°Ð¼Ð¾Ð»ÑÑÐ°Ñ. Ð¢ÐµÐ¼Ð° Ð²ÑÐ¿ÑÑÐºÐ½Ð¾Ð¹ ÐºÐ²Ð°Ð»Ð¸ÑÐ¸ÐºÐ°ÑÐ¸Ð¾Ð½Ð½Ð¾Ð¹ ÑÐ°Ð±Ð¾ÑÑ: Â«ÐÐ²ÑÑÐºÐ¾Ð½ÑÑÑÐ½ÑÐ¹ ÑÑÑÐ±Ð¾ÑÐµÐ°ÐºÑÐ¸Ð²Ð½ÑÐ¹ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ ÑÑÐ³Ð¾Ð¹ 110 ÐºÐÂ». ÐÑÐµÐ´ÑÑÐ°Ð²Ð»ÐµÐ½Ð½Ð°Ñ ÑÐ°Ð±Ð¾ÑÐ° Ð¿Ð¾ÑÐ²ÑÑÐµÐ½Ð° Ð¿ÑÐ¾ÐµÐºÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð¸Ñ Ð°Ð²Ð¸Ð°ÑÐ¸Ð¾Ð½Ð½Ð¾Ð³Ð¾ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ð´Ð»Ñ ÑÑÐµÐ´Ð½ÐµÐ¼Ð°Ð³Ð¸ÑÑÑÐ°Ð»ÑÐ½Ð¾Ð³Ð¾ ÑÐ°Ð¼Ð¾Ð»ÐµÑÐ° Ð½Ð° Ð¾ÑÐ½Ð¾Ð²Ðµ Ð¿ÑÐ¾ÑÐ¾ÑÐ¸Ð¿Ð° CFM56. ÐÑÐ½Ð¾Ð²Ð½ÑÐ¼Ð¸ Ð¿Ð°ÑÐ°Ð¼ÐµÑÑÐ°Ð¼Ð¸, Ð² Ð±Ð¾Ð»ÑÑÐµÐ¹ ÑÑÐµÐ¿ÐµÐ½Ð¸ Ð¾ÐºÐ°Ð·ÑÐ²Ð°ÑÑÐ¸Ð¼Ð¸ Ð²Ð»Ð¸ÑÐ½Ð¸Ðµ Ð½Ð° Ð¿ÑÐµÐ´ÑÑÐ°Ð²Ð»ÐµÐ½Ð½ÑÐ¹ ÑÐ°ÑÑÑÑ, Ð²ÑÑÑÑÐ¿Ð°ÑÑ: ÑÐµÐ¼Ð¿ÐµÑÐ°ÑÑÑÐ° Ð¿ÐµÑÐµÐ´ ÑÑÑÐ±Ð¸Ð½Ð¾Ð¹ Ð²ÑÑÐ¾ÐºÐ¾Ð³Ð¾ Ð´Ð°Ð²Ð»ÐµÐ½Ð¸Ñ; ÑÑÐµÐ¿ÐµÐ½Ñ Ð´Ð²ÑÑÐºÐ¾Ð½ÑÑÑÐ½Ð¾ÑÑÐ¸; ÑÑÐ³Ð° Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ. ÐÐ°Ð´Ð°ÑÐ¸, ÐºÐ¾ÑÐ¾ÑÑÐµ ÑÐµÑÐ°ÑÑÑÑ Ð² ÑÐ¾Ð´Ðµ Ð´Ð°Ð½Ð½Ð¾Ð³Ð¾ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ: 1. ÐÐ·ÑÑÐµÐ½Ð¸Ðµ Ð¾ÑÐ¾Ð±ÐµÐ½Ð½Ð¾ÑÑÐµÐ¹ ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð¸ Ð¿ÑÐ¾ÑÐ¾ÑÐ¸Ð¿Ð° Ð°Ð²Ð¸Ð°Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ CFM56. 2. ÐÑÐ¾Ð²ÐµÐ´ÐµÐ½Ð¸Ðµ Ð²Ð°ÑÐ¸Ð°Ð½ÑÐ½Ð¾Ð³Ð¾ ÑÐµÐ¿Ð»Ð¾Ð²Ð¾Ð³Ð¾ ÑÐ°ÑÑÑÑÐ° ÑÐ¸ÐºÐ»Ð° Ð³Ð°Ð·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½Ð¾Ð³Ð¾ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ñ Ð²ÑÐ±Ð¾ÑÐ¾Ð¼ Ð¾Ð¿ÑÐ¸Ð¼Ð°Ð»ÑÐ½Ð¾Ð³Ð¾ Ð²Ð°ÑÐ¸Ð°Ð½ÑÐ°. 3. ÐÐ½Ð°Ð»Ð¸Ð· Ð´Ð°Ð½Ð½ÑÑ Ð¾ÑÐ´ÐµÐ»ÑÐ½ÑÑ ÑÐ·Ð»Ð¾Ð² Ð³Ð°Ð·Ð¾ÑÑÑÐ±Ð¸Ð½Ð½Ð¾Ð³Ð¾ Ð´Ð²ÑÑÐºÐ¾Ð½ÑÑÑÐ½Ð¾Ð³Ð¾ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ Ñ Ð¿Ð¾Ð¼Ð¾ÑÑÑ Ð³Ð°Ð·Ð¾Ð´Ð¸Ð½Ð°Ð¼Ð¸ÑÐµÑÐºÐ¸Ñ Ð¸ ÑÐ°ÑÑÑÑÐ¾Ð² ÐºÐ¾Ð¼Ð¿ÑÐµÑÑÐ¾ÑÐ°, ÐºÐ°Ð¼ÐµÑÑ ÑÐ³Ð¾ÑÐ°Ð½Ð¸Ñ Ð¸ ÑÑÑÐ±Ð¸Ð½Ñ. 4. ÐÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ðµ Ð¿ÑÐ¾ÑÐ½Ð¾ÑÑÐ¸ Ð»Ð¾Ð¿Ð°ÑÐºÐ¸, Ð´Ð¸ÑÐºÐ° Ð¸ ÑÐ¾ÑÐ¾ÑÐ° Ð¿Ð¾ÑÐ»ÐµÐ´Ð½ÐµÐ¹ ÑÑÑÐ¿ÐµÐ½Ð¸ Ð¿ÑÐµÐ´ÑÑÐ°Ð²Ð»ÐµÐ½Ð½Ð¾Ð¹ ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð¸. Ð Ð°Ð±Ð¾ÑÐ° ÑÐ²Ð»ÑÐµÑÑÑ Ð°ÐºÑÑÐ°Ð»ÑÐ½Ð¾Ð¹ Ð¸Ð·-Ð·Ð° ÑÐ¾Ð³Ð¾, ÑÑÐ¾ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ð¸ CFM56 Ð¸ÑÐ¿Ð¾Ð»ÑÐ·ÑÑÑÑÑ Ð½Ð° Ð¿Ð°ÑÑÐ°Ð¶Ð¸ÑÑÐºÐ¸Ñ ÑÐ°Ð¼Ð¾Ð»ÐµÑÐ°Ñ (Ð½Ð°Ð¿ÑÐ¸Ð¼ÐµÑ: Airbus A320, Boeing 737 Ð½Ð¾Ð²Ð¾Ð³Ð¾ Ð¿Ð¾ÐºÐ¾Ð»ÐµÐ½Ð¸Ñ), Ð° ÑÐ°ÐºÐ¶Ðµ Ð½Ð° Ð±Ð°Ð·Ðµ Ð´Ð°Ð½Ð½Ð¾Ð³Ð¾ Ð¿ÑÐ¾ÑÐ¾ÑÐ¸Ð¿Ð° ÑÐ¾Ð·Ð´Ð°ÑÑÑÑ Ð´ÑÑÐ³Ð¸Ðµ Ð¼Ð¾Ð´ÐµÐ»Ð¸ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»ÐµÐ¹, ÐºÐ¾ÑÐ¾ÑÑÐµ Ð¿ÑÐ¸Ð¼ÐµÐ½ÑÑÑÑÑ Ð½Ð° ÑÐ°Ð·Ð»Ð¸ÑÐ½ÑÑ ÑÐ°Ð¼Ð¾Ð»ÑÑÐ°Ñ. Ð Ð²ÑÐ¿ÑÑÐºÐ½Ð¾Ð¹ ÑÐ°Ð±Ð¾ÑÐµ Ð±ÑÐ»Ð° Ð¿ÑÐ¾Ð¸Ð·Ð²ÐµÐ´ÐµÐ½Ð° Ð¾ÑÐµÐ½ÐºÐ° Ð¸Ð·Ð¼ÐµÐ½ÐµÐ½Ð¸Ð¹ ÑÐ°Ð·Ð»Ð¸ÑÐ½ÑÑ Ð¿Ð°ÑÐ°Ð¼ÐµÑÑÐ¾Ð² Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ñ, Ð¿Ð¾Ð»ÑÑÐµÐ½Ð½ÑÑ Ð² ÑÐ¾Ð´Ðµ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ, Ñ ÑÑÐµÑÐ¾Ð¼ Ð¸Ð·Ð¼ÐµÐ½ÐµÐ½Ð¸Ñ Ð½Ð°ÑÐ°Ð»ÑÐ½ÑÑ Ð´Ð°Ð½Ð½ÑÑ, Ð¾ÑÐ»Ð¸ÑÐ½ÑÑ Ð¾Ñ Ð´Ð°Ð½Ð½ÑÑ Ð´Ð»Ñ ÐºÐ¾Ð½ÐºÑÐµÑÐ½Ð¾Ð³Ð¾ Ð¿ÑÐ¾ÑÐ¾ÑÐ¸Ð¿Ð°. Ð£Ð´Ð°Ð»Ð¾ÑÑ ÑÐ¾ÑÑÐ°Ð½Ð¸ÑÑ Ð´Ð¾ÑÑÐ¾Ð¹Ð½ÑÐµ Ð¿Ð¾ÐºÐ°Ð·Ð°ÑÐµÐ»Ð¸ ÐºÐ¾ÑÑÑÐ¸ÑÐ¸ÐµÐ½ÑÐ° Ð¿Ð¾Ð»ÐµÐ·Ð½Ð¾Ð³Ð¾ Ð´ÐµÐ¹ÑÑÐ²Ð¸Ñ Ð¸ Ð´ÑÑÐ³Ð¸Ñ Ð²Ð°Ð¶Ð½ÑÑ ÑÐ°ÑÐ°ÐºÑÐµÑÐ¸ÑÑÐ¸Ðº.
description: The given work is devoted to design of aircraft engine for mid-range aircraft based on CFM56. The main parameters that have a greater effect on the presented calculation are: temperature in front of the high-pressure turbine; bypass ratio; engine thrust. Tasks that are solved in the course of this study: 1. Study of the design features of the prototype aircraft engine CFM56. 2. Conducting a variant thermal calculation of the cycle of a gas turbine engine with the choice of the best option. 3. Data analysis of individual units of a gas turbine dual-circuit engine using gas-dynamic and calculations of the compressor, combustion chamber and turbine. 4. The study of the strength of the blades, disc and rotor of the last stage of the presented design. The work is urgent due to the fact that CFM56 engines are used on passenger aircraft (for example: Airbus A320, Boeing 737 of a new generation), and also on the basis of this prototype other engine models are created that can be used on various aircraft. In the graduation work, an assessment was made of the changes in various engine parameters obtained during the study, taking into account changes in the initial data, different from the data for a specific prototype. It was possible to maintain decent performance and other important characteristics.