FIELD: transport.
SUBSTANCE: invention relates to single-engine aircraft, particularly, to bicycle landing gear. Bicycle landing gear comprises two wheels in fuselage and two wheels on sides. Note here that landing gear side legs are retracted into wing end play. Wheels of side legs can extend from end plates to turn in flight position together with end plates forward or backward.
EFFECT: decreased weight, takeoff and landing speed.
6 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HYDROPLANE (VERSIONS) | 2013 |
|
RU2513345C1 |
| LANDING GEAR COWL | 2012 |
|
RU2494010C1 |
| CHASSIS FOR TRANSPORT AIRCRAFT (VERSIONS) | 2012 |
|
RU2592123C2 |
| AIRCRAFT FOR LANDING AT CROSS WIND (VERSIONS) | 2008 |
|
RU2400398C2 |
| LANDING GEAR FOR CROSSWIND LANDING /VERSIONS/ | 2011 |
|
RU2471675C1 |
| UNDERCARRIAGE NLG (VERSIONS) | 2012 |
|
RU2513347C1 |
| STAROVEROV'S SPACECRAFT (VERSIONS) AND/OR ALGORITHMS OF ITS OPERATION | 2012 |
|
RU2503592C1 |
| STAROVEROV' WING (VERSIONS) | 2011 |
|
RU2480375C1 |
| EMERGENCY LANDING SYSTEM | 2006 |
|
RU2335437C2 |
| SEAPLANE FUSELAGE (VERSIONS) | 2013 |
|
RU2504501C1 |
