CN110606185A

CN110606185A - Safety airplane with combined structure

Info

Publication number: CN110606185A
Application number: CN201910962028.6A
Authority: CN
Inventors: 王彪
Original assignee: Individual
Current assignee: Individual
Priority date: 2019-10-11
Filing date: 2019-10-11
Publication date: 2019-12-24

Abstract

The invention relates to the technical field of spaceflight, in particular to a safety airplane with a combined structure, which comprises an airplane body, wherein the airplane body comprises an airplane chassis and a separable airplane cabin arranged on the airplane chassis; the aircraft cabin comprises an independent propulsion system, an oxygen supply guarantee system, a life guarantee system, a driving system and a landing system. The aircraft body can realize rapid vertical separation when the aircraft cabin or the aircraft wings explode, and the flying cabin can continue flying through the self-contained independent propulsion system after the aircraft is separated, so that the safety of passengers is ensured.

Description

Safety airplane with combined structure

Technical Field

The invention relates to the technical field of aircraft design, in particular to a safety aircraft with a combined structure.

Background

After an aircraft accident occurs, passengers of an airliner in the air basically live and die due to the fact that escape tools such as parachutes do not exist. In the prior art, for example, wings are damaged, an oil tank leaks oil, and the problem at the bottom of the airplane causes the airplane to go wrong, and the airplane is generally forced to land and parachutes, but the mode has great potential safety hazard, and the survival problem cannot be effectively guaranteed, in the improved technology, for example: CN201811134470.1 discloses a self-rescue device for a separable cabin of an airplane, wherein after the airplane leaves, the cabin is ejected out under the action of an ejection device, meanwhile, a storage umbrella layer arranged at the upper end of the cabin is automatically opened, the danger degree of the ejection mode to personnel is large, although the cabin is provided with a parachute, the landing is in an unpowered state, so that the landing has great randomness and is inconvenient to rescue; CN201720420252.9 discloses a safety airplane, which has the defect that the personnel in the airplane can not be safely separated, so that designing a new airplane is a problem which needs to be solved urgently at present.

Disclosure of Invention

In order to solve the above-mentioned problems of the prior art, the present invention provides a safety aircraft with a combined structure, which can improve the above disadvantages.

The invention relates to a safety airplane with a combined structure, which comprises an airplane body, wherein the airplane body comprises an airplane chassis and a separable airplane cabin arranged on the airplane chassis, when the lower part of the airplane is exploded, for example, wings are hit by guided missiles, the airplane chassis is subjected to oil leakage and other accidents, the airplane cabin can be separated from the airplane chassis, the airplane is prevented from falling down to cause air crash in time, a sealed cabin is arranged on the bottom surface of the airplane cabin, the upper part and the lower part of the sealed cabin can float on the water surface, and the sealed cabin can ensure the safety of passengers and passengers; the aircraft cabin comprises an independent propulsion system, an oxygen supply guarantee system, a life guarantee system, a driving system and a landing system, wherein the independent propulsion system is designed at the tail of the aircraft cabin, a direct reaction propulsion system or an indirect reaction propulsion system is adopted, and an engine in the independent propulsion system can be a piston type aircraft engine or a turboprop engine or a turboshaft engine; the oxygen supply packaging system comprises an air guarantee system in the passenger cabin of the aircraft and an independently used oxygen supply system, wherein the independently used oxygen supply system consists of an oxygen generator container, an oxygen mask cover and braces, the oxygen mask and the braces are arranged on the front end surface of the oxygen generator container, and the oxygen mask cover is arranged on the oxygen mask; the life support system is designed to be a single spherical device, passengers can be hidden inside the spherical device, and the life support system is internally provided with a breathing device and emergency products such as standby food and drinking water.

Furthermore, a quick interlocking device is arranged between the aircraft chassis and the aircraft cabin, the quick separation of the aircraft can be realized through the quick interlocking device, and the quick interlocking device is controlled by an electric control system of the cockpit to release the locking, so that the aircraft cabin is quickly separated from the aircraft chassis.

Furthermore, the airplane chassis comprises an airplane cargo cabin, an airplane flying system, an oil tank, an engine, a tail wing, double wings and a wheel system.

Further, flight cabin back sets up the parachute locker room, and the parachute locker room sets up on flight cabin focus line, and the parachute locker room is the multiunit, sets up the parachute that can launch in the parachute locker room, and the multiunit parachute can position balance, and helps the stability in flight cabin, considers the holistic focus position in aircraft cabin in the design.

Furthermore, the quick interlocking device is controlled by an electric control system to release locking, and is arranged between the airplane passenger cabin and the contact surface of the airplane chassis.

The aircraft body can realize rapid vertical separation when the aircraft cabin or the aircraft wings explode, and the flying cabin can continue flying through the self-contained independent propulsion system after the aircraft is separated, so that the safety of passengers is ensured.

Drawings

FIG. 1 is a schematic view of the structure of the present invention.

Fig. 2 is a schematic view of a safe airplane in a detached state.

FIG. 3 is a schematic view of a rear structure of a flight cabin.

Fig. 4 is a view showing an opening effect of the parachute of fig. 2.

Fig. 5 is a cross-sectional view taken along line a-a' of fig. 1.

The figure is as follows: the airplane comprises a flying cabin 1, an airplane chassis 2, a parachute 3, an independent propulsion system 4, a parachute storage chamber 5 and a quick interlocking device 6.

Detailed Description

In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention will be described in further detail with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.

As shown in fig. 1-3, the present invention relates to a safety aircraft with a combined structure, which comprises an aircraft body, wherein the aircraft body comprises an aircraft chassis 2 and a separable aircraft cabin 1 arranged on the aircraft chassis, when the lower part of the aircraft is exploded, for example, the wings are hit by missiles, the aircraft chassis is subjected to oil leakage and other accidents, the aircraft cabin can be separated from the aircraft chassis, and the aircraft is prevented from falling down to cause air crash in time, the bottom surface of the aircraft cabin is provided with a sealed cabin, the sealed cabin can float on the water surface with light weight, and the sealed cabin can ensure the safety of passengers; the aircraft cabin comprises an independent propulsion system 4, an oxygen supply guarantee system, a life guarantee system, a driving system and a landing system, wherein the independent propulsion system is designed at the tail of the aircraft cabin, a direct reaction propulsion system or an indirect reaction propulsion system is adopted, and an engine in the independent propulsion system can be a piston type aircraft engine or a turboprop engine or a turboshaft engine; the oxygen supply packaging system comprises an air guarantee system in the passenger cabin of the aircraft and an independently used oxygen supply system, wherein the independently used oxygen supply system consists of an oxygen generator container, an oxygen mask cover and braces, the oxygen mask and the braces are arranged on the front end surface of the oxygen generator container, and the oxygen mask cover is arranged on the oxygen mask; the life support system is designed to be a single spherical device, passengers can be hidden inside the spherical device, and the life support system is internally provided with a breathing device and emergency products such as standby food and drinking water.

Set up quick interlock 6 between aircraft chassis 2 and the aircraft cabin, can realize the quick separation of aircraft through quick interlock, quick interlock removes the locking through the electrical system control by the cockpit to make aircraft cabin and aircraft chassis break away from fast.

The airplane chassis 2 comprises an airplane cargo bin, an airplane flying system, an oil tank, an engine, a tail wing, double wings and a wheel train.

1 back in flight cabin sets up parachute storage room 5, and parachute storage room 5 sets up on flight cabin focus line, and the parachute storage room is the multiunit, sets up parachute 3 that can launch in the parachute storage room, considers the holistic focus position in aircraft cabin in the design.

As shown in fig. 5, the quick-locking device 6 is controlled to release the locking by an electric control system.

When detached, the aircraft cabin may continue to sail through the parachute and the independent propulsion system as shown in FIG. 4.

Claims

1. A kind of combined structure's safe plane, including the organism, characterized by: the aircraft body comprises an aircraft chassis and a separable aircraft cabin arranged on the aircraft chassis, a sealed cabin is arranged on the bottom surface of the aircraft cabin, and the sealed cabin can float on the water surface with a light weight; the aircraft cabin comprises an independent propulsion system, an oxygen supply guarantee system, a life guarantee system, a driving system and a landing system.

2. A safety aircraft of modular construction according to claim 1, wherein: and a quick interlocking device is arranged between the aircraft chassis and the aircraft cabin.

3. A safety aircraft of modular construction according to claim 1, wherein: the airplane chassis comprises an airplane cargo bin, an airplane flying system, an oil tank, an engine, a tail wing, double wings and a wheel train.

4. A safety aircraft of modular construction according to claim 1, wherein: the back of the flight cabin is provided with a parachute storage room which is arranged on a gravity center line of the flight cabin.

5. A safety aircraft of modular construction according to claim 1, wherein: the quick interlocking device is controlled by an electric control system to unlock.