| 摘要 |
An aircraft with a device for rescue of passengers in case of emergency includes: a fuselage with hatches for entry and exit of passengers and crew from a cockpit equipped with an on-board computer and a device for issuing electric commands in required sequence for implementation of a rescue program that in the event of a decision to evacuate the passengers may be actuated by an on-board computer, pilot or from the ground; wings, a tail, engines, chassis, an emergency hatch in the rear part of fuselage made with possibility of automatic opening, and seats for passengers. The aircraft is equipped with at least one rigid airtight heat-insulated landing container located inside the fuselage, inside which in the longitudinal direction the seats for passengers and crew are located. In the upper and lower parts of fuselage upper and lower guides are installed, respectively which are made with possibility of interaction with them of relevant elements of the container and are means for fastening said container in a fixed position and unfixturing to move the container along the fuselage automatically. The aircraft is equipped with means for automatic closing the emergency hatch after moving-out of the container from the fuselage. |
