| 摘要 |
FIELD: aviation. ^ SUBSTANCE: invention is related to auxiliary facilities for fixation of power units on aircraft. Turbojet engine (TJE) is designed for installation on top of aircraft hull (1) tail unit by means of mounting suspension ((28, 128), (28', 128')) and comprises fan (11), front part (12) of body, back part (18) of body, auxiliary devices (22, 23, 24, 25) installed along external side of body front part (12), which contains points ((31, 32, 33), (31', 32' 33')) for fixation of mounting suspension (28, 28'). Fixation points are located so that to provide for same fixation of TJE (10) in any side of hull (1) of aircraft. Auxiliary devices (22, 23, 24, 25) are located so that they are accessible outside hull (1) independently from side, on which TJE is installed. ^ EFFECT: inventions are aimed at reduction of production costs. ^ 9 cl, 3 dwg |
