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

Inactive Publication Date: 2009-03-25
林德全
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For many years, people have been thinking about designing a safe and life-saving aircraft, but so far only the four-seat light parachute aircraft developed by an American company can be partially app...

Method used

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  • Safety lifesaving airplane
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Examples

Experimental program
Comparison scheme
Effect test

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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Abstract

The invention discloses a safety rescuing airplane, which is applicable to large-scale, medium-scale and small-scale airplanes including fixed wing airplanes and rotor wing airplanes, a passenger cabin of the large-scale and medium-scale airplanes adopts at least two layers of channel-shaped floors, when the airplane runs into an inevitable air crash, the airplane can ignite exploding bolts that are used for fixing airplane wings, an airplane tail and a front undercarriage, and cut off an operating connection rod, a cable or an electric cable that are led into the airplane wings, the airplane tail and the front undercarriage, thus abandoning the airplane wings, the airplane tail and the front undercarriage, simultaneously opening parachutes on the top of an airplane body and at the airplane tail, motivating the charging of two air bags in the bottom and at the lower two sides of the airplane body, and leading the airplane body to land or stop smoothly, slowly and safely under the actions of the parachutes and the air bags. The fixed wing airplane can omit the abandoning of the front undercarriage and the abandoning of the airplane tail in a ground sliding process; and the lightweight fixed wing airplane also can omit the abandoning of the airplane tail.

Description

1. Technical field [0001] The invention relates to an aircraft, in particular to a safety and rescue aircraft, which belongs to the field of aircraft design. 2. Background technology [0002] With economic development and social progress, there are more and more aircraft, and there are more and more air accidents. Whenever an air accident occurs, most of the aircraft crashed and people died, and the death rate of the drivers and passengers is almost 100%. For many years people have been thinking about designing a safe and life-saving aircraft, but so far only the four-seater light full-flight parachute aircraft developed by an American company can be partially applied. However, this full-flight parachute aircraft also has fatal shortcomings. That is, although the parachute slows down the landing speed of the aircraft, there is still a risk of explosion after the fuel tank hits the ground. Fire and explosion accidents are not applicable. 3. Contents of the invention [00...

Claims

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Application Information

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IPC IPC(8): B64D25/00
CPCB64C27/006B64D25/12
Inventor (请求不公开姓名)
Owner 林德全
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