FIELD: propellers of flying vehicles and snowplanes. SUBSTANCE: propeller blade includes front and rear planes intersecting on trailing edges at angle of γ and surfaces of back and leading edge engageable with them and curved over radii r and ro. Surface of back is curved by radius r determined from formula r=k2v2/ω which is equal in shank to rounding-off radius ro of leading edge at minimum velocity V of incoming flow. EFFECT: enhanced reliability. 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| WING PROFILE | 1995 |
|
RU2094309C1 |
| PROPELLER BLADE | 1991 |
|
RU2015062C1 |
| WINDWHEEL BLADE | 1995 |
|
RU2076239C1 |
| STREAMLINED BODY OF CAR | 1995 |
|
RU2085427C1 |
| WINDWHEEL BLADE | 0 |
|
SU1793094A1 |
| FLYING VEHICLE FUSELAGE | 1995 |
|
RU2110444C1 |
| WINDWHEEL BLADE | 1991 |
|
RU2027893C1 |
| TILTING WING BLADE | 1991 |
|
RU2009075C1 |
| PROPELLER BLADE | 2001 |
|
RU2228882C2 |
| ROTOR BLADE | 2007 |
|
RU2376202C2 |
