FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to landing of rotorcraft. Proposed method consists in that, first, preset speed is selected at glide path slope. Then, total pitch of the rotor is selected. Then, reverse is actuated of engine reversing devices are activated depending upon engine type at preset altitude above landing ground to brake the rotorcraft and to reduce landing speed. Now, total pitch and rotor thrust are increased to reduce landing speed to zero unless touchdown.
EFFECT: landing without alighting run.
| Title | Year | Author | Number |
|---|---|---|---|
| HIGH-SPEED ROTORCRAFT | 2014 |
|
RU2573698C2 |
| METHOD OF ROTORCRAFT NO-RUN TAKEOFF WITH AUTOROTATING ROTOR AND WING | 2013 |
|
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| ROTOR-CRAFT | 2016 |
|
RU2662339C2 |
| ROTARY-WING AIRCRAFT | 2017 |
|
RU2673754C2 |
| FLIGHT VEHICLE (VERSIONS), FLIGHT VEHICLES PARTS, METHOD OF EXPLOITING FLIGHT VEHICLE AND ITS PARTS | 2010 |
|
RU2466061C2 |
| HIGH-SPEED TURBOFAN COMBINED HELICOPTER | 2016 |
|
RU2629475C1 |
| ROTOR "AIR WHEEL", GYROSTABILISED AIRCRAFT AND WIND-DRIVEN ELECTRIC PLANT USING ROTOR "AIR WHEEL", SURFACE/DECK DEVICES FOR THEIR START-UP | 2013 |
|
RU2538737C9 |
| UNMANNED HIGH-SPEED HELICOPTER, DESANTIFIED FROM PLANE AIRCRAFT | 2016 |
|
RU2627975C2 |
| METHOD OF GLIDING AND GLIDE VEHICLE | 2008 |
|
RU2397109C2 |
| MULTI-SCREW UNMANNED ROTORCRAFT | 2016 |
|
RU2611480C1 |
