FIELD: transport.
SUBSTANCE: proposed aircraft comprises fuselage, two landing gear assies with wheels secured therein, and wheel selective braking device. Proposed method consists in applying thrust required to run aircraft and braking force to one wheel of landing gear assy located closer to aircraft turnaround center. Note here that braking force is applied to one wheel, larger force being applied on first side of landing gear compared with that applied to second side. Side located closer to turnaround center is taken to be said first side.
EFFECT: reduced loads originating in aircraft turnaround on ground.
12 cl, 8 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT TOW DEVICE | 2014 |
|
RU2558523C1 |
| METHOD OF AIRCRAFT BRAKING DURING LANDING | 2019 |
|
RU2722597C1 |
| METHOD OF ADDITIONAL BRAKING OF AIRCRAFT WHEELS AND DEVICE TO THIS END | 2012 |
|
RU2502638C2 |
| AIRCRAFT (VERSIONS), TAKEOFF-LANDING GEAR (VERSIONS) AND METHOD OF LIFTING AIRCRAFT IN AIR (VERSIONS) | 2012 |
|
RU2588198C2 |
| AIRCRAFT | 2008 |
|
RU2466907C1 |
| DRIVE UNIT FOR AIRCRAFT LANDING GEAR WITH INTEGRATED COOLING | 2012 |
|
RU2601794C2 |
| FLYING VEHICLE | 2003 |
|
RU2235045C1 |
| AIRCRAFT AIRFRAME AND THE LANDING GEAR TECHNICAL CONDITION MONITORING METHOD AND DEVICE AND DEVICE FOR ITS IMPLEMENTATION | 2017 |
|
RU2678540C1 |
| AIRCRAFT | 1992 |
|
RU2023628C1 |
| METHOD AND DEVICE FOR INCREASING AIRCRAFT BRAKING DURING ITS LANDING RUN | 2005 |
|
RU2341409C1 |
