FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to propeller blades motion control systems. Screw (3, 3') for aircraft (1) made with possibility of hovering comprises drive shaft (6), bushing (5) connected to drive shaft (6) and made with possibility of rotation around first axis (A), and at least two blades (9) pivotally connected to bushing (5) by means of rigid or elastic connection so that they can take spatial position turned around and/or shifted along second axis (B, C, D). Aircraft (1) further comprises detection means (25) configured to detect the spatial position of at least one said vane (9) relative to bushing (5). Detector (25) is configured to obtain an optical image associated with the spatial position of blade (9) relative to bushing (5).
EFFECT: enabling determination of helicopter rotor blade displacements and turns using the minimum possible number of components.
13 cl, 9 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ROTOR FOR AIRCRAFT MADE WITH POSSIBILITY OF HANGING | 2019 |
|
RU2783551C1 |
| ROTOR | 2006 |
|
RU2338665C2 |
| BLADE FOR AIRCRAFT MADE WITH POSSIBILITY OF HANGING AND METHOD FOR REMOVAL OF ICE FROM SPECIFIED BLADE | 2019 |
|
RU2784218C1 |
| VERTICAL TAKE-OFF AND LANDING SEAPLANE WITH A MAIN ROTOR WITH FOLDING RETRACTABLE BLADES | 2021 |
|
RU2781817C1 |
| MAIN ROTOR | 2005 |
|
RU2281885C1 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH ROTOR WITH FOLDING RETRACTABLE BLADES | 2019 |
|
RU2727787C1 |
| SCREW FOR AIRCRAFT SUSCEPTIBLE TO HOVERING, AND CORRESPONDING CONTROL METHOD | 2017 |
|
RU2730786C1 |
| SCREW FOR HOVERING AIRCRAFT | 2020 |
|
RU2799170C1 |
| FLYING VEHICLE PROPELLER ENCASED IN COWL AND ROTORCRAFT | 2014 |
|
RU2570971C2 |
| ROTARY-WING VEHICLE ROTOR WITH BLADE FOLDING SYSTEM | 2008 |
|
RU2376201C1 |
