PL43194B1 - - Google Patents

Download PDF

Info

Publication number
PL43194B1
PL43194B1 PL43194A PL4319458A PL43194B1 PL 43194 B1 PL43194 B1 PL 43194B1 PL 43194 A PL43194 A PL 43194A PL 4319458 A PL4319458 A PL 4319458A PL 43194 B1 PL43194 B1 PL 43194B1
Authority
PL
Poland
Prior art keywords
rotor
blades
blade
flight
torque
Prior art date
Application number
PL43194A
Other languages
English (en)
Polish (pl)
Filing date
Publication date
Application filed filed Critical
Publication of PL43194B1 publication Critical patent/PL43194B1/pl

Links

PL43194A 1958-11-20 PL43194B1 (enrdf_load_stackoverflow)

Publications (1)

Publication Number Publication Date
PL43194B1 true PL43194B1 (enrdf_load_stackoverflow) 1960-04-15

Family

ID=

Similar Documents

Publication Publication Date Title
CN211918983U (zh) 用于交通工具的推力发生旋翼总成
US4203708A (en) Elastomeric rotor load reaction system
US3228478A (en) Control lag compensator for rotary wing aircraft
CN113396103B (zh) 用于直升机的反扭矩旋翼
RU2237599C2 (ru) Однолопастный несущий винт вертолета
US4284387A (en) Blade fold restraint system
US3470962A (en) Rotor heads for rotary wing aircraft
US4235570A (en) Elastomeric helicopter rotor load reaction system
US2757745A (en) Variable pitch rotor blade construction
US3215370A (en) Rotating wing aircraft
US3637321A (en) Tail rotor of a helicopter
US3321021A (en) Lightweight folding rotor
US3185410A (en) Vertical lift aircraft
US3450208A (en) Dual drive mechanism
EP0776820B1 (en) Propeller propulsion unit for aircrafts in general
PL43194B1 (enrdf_load_stackoverflow)
US2510006A (en) Rotating wing aircraft
US4669958A (en) Swashplate control system
ITTO20010101A1 (it) Rotore con gruppo di trasmissione omocinetico per un aeromobile.
US2537623A (en) Aircraft rotor hub construction
US3529790A (en) Means for changing wing incidence for varying angles of attack
US1023233A (en) Flying-machine.
US2237030A (en) Aeronautical propeller
US4650400A (en) Helicopter blade pitch adjusting system
US2971584A (en) Devices for stabilising helicopter aircraft