FIELD: transport.
SUBSTANCE: aircraft power plant 1 comprises turbojet engine 2, attachment post 4, assemblage of engine suspension units (6a, 6b, 8, 9) arranged between said post 4 and turbojet engine 2. Assemblage of engine suspension units comprises first front and second front suspension units 6a and 6b, respectively, secured on turbojet engine blower 12 housing in symmetry about the plane formed by engine lengthwise axis 5 and its vertical orientation Z. Note here that both aforesaid front suspension units 6a, 6b can take up loads acting in crosswise (X) and lengthwise (Z) directions with respect to turbojet engine 2. Each of said units comprises safety pin 36 arranged in crosswise direction (Y) on blower housing 12 and fork 30 fixed on attachment post and including two crossarms 32a, 32b. Said safety pin 36 passes through both crossarms 32a, 32b of fork 30 in both first and second front engine suspension units 6a, 6b.
EFFECT: reduced sizes of engine suspension units.
17 cl, 6 dwg
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