The design of the gearbox of a single-engine aircraft has been developed ( Transport )




The design of the gearbox of a single-engine aircraft has been developed.
Specifications: -Gear ratio U=17.5;
-The power of the gas turbine engine N = 500kW;
-Center distance Aw=225mm;
-The direction of rotation of the input and output shafts is multidirectional.


Characteristics:

  • Rated torque: Hm.
  • Gear ratio number:


  • Fotos

    SEW-EURODRIVE Gmb&CoKG
    SETC Ltd.
    SME Tomsk Electronic Company
    Electroagregat corp.
    JSC «KAMAZ»
    LLC «Mechanic-R»
    PJSC «PNPPK»
    JSC «Tyazhmash»
    LLC «OKB Aviation Solutions»
    LLC «Power motor»
    JSC «KEMZ»
    JSC «Kryminntarm»
    LLC «Oil service»
    LLC «Tech Red Prom»
    LLC «Industrial Park»
    UEC «Aviadvigatel»
    Transputmash Trade Company, JSC
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