|
US5713721A
(en)
|
|
Retention system for the blades of a rotary machine
|
|
US20120076641A1
(en)
|
|
Variable vane assembly for a turbine compressor
|
|
US4668167A
(en)
|
|
Multifunction labyrinth seal support disk for a turbojet engine rotor
|
|
US3799693A
(en)
|
|
Bullet nose fastening arrangement
|
|
US20090087304A1
(en)
|
|
Stage of variable-pitch vanes for a turbomachine
|
|
EP1111193B1
(en)
|
|
Axial blade retention system for turbomachines
|
|
CN102472295B
(zh)
|
|
用于具有可变斜度叶片的螺旋桨的毂
|
|
US20100166562A1
(en)
|
|
Turbine blade root configurations
|
|
SU167599A1
(cg-RX-API-DMAC7.html)
|
|
|
|
RU2002112338A
(ru)
|
|
Роторная машина (варианты), прокладка и модуль для роторной машины
|
|
US20080159861A1
(en)
|
|
Compressor with centripetal air takeoff
|
|
JPS6215726B2
(cg-RX-API-DMAC7.html)
|
|
|
|
US2935296A
(en)
|
|
Blade retaining means
|
|
US4598600A
(en)
|
|
Bearing support structure
|
|
US3521974A
(en)
|
|
Turbine blade construction
|
|
US20240410392A1
(en)
|
|
Hybrid shroud impeller
|
|
RU2241834C2
(ru)
|
|
Рабочее колесо осевой турбомашины
|
|
US10794219B2
(en)
|
|
Axial case ring to maximize thrust bushing contact area of variable vane
|
|
GB2556725A
(en)
|
|
Stage of variable-pitch blades for a turbine engine, turbine engine and associated installation method
|
|
US20230175527A1
(en)
|
|
Turbomachine compressor having a stationary wall provided with a shape treatment
|
|
US3936216A
(en)
|
|
Blade sealing and retaining means
|
|
US3314652A
(en)
|
|
Vibration damped turbo machinery
|
|
EP3550152A1
(en)
|
|
Impeller and centrifugal compressor
|
|
US20240035385A1
(en)
|
|
Turbomachine rotor having improved vibratory behaviour
|
|
US4025233A
(en)
|
|
Rotor for wind-driven machine
|