FIELD: aviation.
SUBSTANCE: invention relates to aviation. The aircraft has a fuselage (1), to the bottom of which a landing gear (4), a turbojet engine and wings (3) are attached. Two cables (5) are attached to the bottom of the fuselage (1) to its ends, having steel balls (6) at the ends. The runway has a reinforced concrete pavement and is 500-2000 kilometers long. In reinforced concrete pavement, bars are attached to steel reinforcement, on which two rows of channels (9) are fixed with shelves at a distance from each other less than the diameter of steel balls (6) attached by cables (5) to the fuselage (1) of the aircraft.
EFFECT: simplification of aircraft and runway structures is achieved.
2 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT AND RUNWAY THEREOF | 2019 |
|
RU2733674C1 |
| AIRCRAFT | 2017 |
|
RU2667836C1 |
| SEAPLANE | 2005 |
|
RU2305650C1 |
| AERODROME | 2020 |
|
RU2752838C1 |
| SEAPLANE | 2000 |
|
RU2184050C2 |
| DAM | 2021 |
|
RU2773527C1 |
| HELICOPTER | 2019 |
|
RU2722524C1 |
| AIRCRAFT | 2017 |
|
RU2657649C1 |
| AIRPLANE | 2007 |
|
RU2336198C1 |
| AIRCRAFT (VERSIONS), TAKEOFF-LANDING GEAR (VERSIONS) AND METHOD OF LIFTING AIRCRAFT IN AIR (VERSIONS) | 2012 |
|
RU2588198C2 |
