Safety lifesaving airplane
An aircraft and safety technology, applied in the field of aircraft, can solve the problems of fuel fire and explosion accidents, such as inapplicability and explosion, and achieve the effect of reducing fuel consumption and cost
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Embodiment 1
[0035] Embodiment 1 Medium-sized aircraft two-layer channel-shaped floor:
[0036] according to Figure 4 , the present invention adopts two-layer channel-shaped floor (24) to medium-sized aircraft, and under the same situation of cabin (9) length, number of seats is increased to twice of the number of seats of an ordinary layer of aircraft; The length of the cabin (9) of the aircraft is reduced by half compared with that of a common layer of aircraft, and the weight of the cabin (9) is reduced by nearly half. Seat (22) can be placed horizontally, also can be placed vertically, and the outer sides, both sides of the upper floor are child seats, and pillar (23) is used to support the upper floor (24). Same number of seats like this The aircraft weight of the present invention can be reduced a lot than existing common aircraft, and this just also can use parachute (20) and air bag to carry out safe lifesaving to create condition for medium-sized aircraft, also reduced fuel cons...
Embodiment 2
[0037] Embodiment 2 Large aircraft three-layer channel-shaped floor:
[0038] according to Figure 5 , the present invention adopts three-layer channel shape floor (24) to large-scale aircraft, under the same situation of passenger cabin (9) length, number of seats is increased to nearly three times of the number of seats of an ordinary layer of aircraft; The length of the passenger cabin (9) of the one-story aircraft is reduced by nearly two-thirds, and the weight of the passenger cabin (9) is reduced by nearly two-thirds. Seat (22) can be placed horizontally, also can be placed vertically, and the outer sides, both sides of the upper floor are child seats, and pillar (23) is used to support the upper floor (24). The weight of the aircraft of the present invention with the same number of seats can be reduced a lot than the existing common aircraft, which also creates conditions for large aircraft to use parachutes (20) and airbags for safe lifesaving, and also reduces fuel c...
Embodiment 3
[0039] Embodiment 3 mechanical control system fixed-wing aircraft in distress in the air:
[0040] According to Figure 1, Figure 2, image 3 , Figure 4 , Figure 5 , Figure 7 As shown, when the fixed-wing aircraft of the mechanical control system of the present invention is in distress in the air, the early warning device (1) installed in the cockpit (10) reports to the police, and the driver checks and judges the danger. If the air disaster is inevitable, the driver presses the The air rescue button (2) starts the emergency rescue system, and the signal is transmitted through the signal transmission line (3) and controls the explosive bolts leading to the control links of the wings (4), tail (6), front landing gear (5) and Wing (4), tail (6), nose landing gear (5), hatch cover of parachute compartment (7) at the top of fuselage, hatch cover of parachute compartment (8) at tail, hatch cover of airbag compartment (11) at the bottom of fuselage 1. The explosion bolt on the ...
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