|
RU2583824C2
|
|
Supersonic aircraft with in-fuselage cargo compartments
|
|
RU2533597C1
|
|
Method of determination of sufficiency of oil cooling in jet turbine engine
|
|
RU2523117C1
|
|
Driveline for torque transmission and shaft used in it
|
|
RU2529094C1
|
|
Self-locking nut for closed areas
|
|
RU2520708C1
|
|
Aircraft gun localiser
|
|
RU2525102C2
|
|
Aircraft engine pylon
|
|
RU2503940C1
|
|
Method of determination of gas turbine intake area stability margin
|
|
RU2501130C1
|
|
Switching-separation device
|
|
RU2504057C1
|
|
Multipurpose aircraft antenna feeder system
|
|
RU2516312C2
|
|
Device for aperture piercing in conductor lugs
|
|
RU2496133C1
|
|
Control lever
|
|
RU2493549C1
|
|
Method of diagnosing input device of aircraft propulsion unit
|
|
RU2492366C1
|
|
Cylinder of canopy control
|
|
RU2487818C1
|
|
Canopy displacing and locking mechanism
|
|
RU2516322C2
|
|
Mould for corrugated parts forming from blanks
|
|
RU2488775C1
|
|
Multi-task aircraft integrated onboard hardware complex
|
|
RU2503584C2
|
|
Maneuvering aircraft
|
