CN201143994Y

CN201143994Y - Disk type aerobus

Info

Publication number: CN201143994Y
Application number: CNU2007201173696U
Authority: CN
Inventors: 李少海
Original assignee: Individual
Current assignee: Individual
Priority date: 2007-11-04
Filing date: 2007-11-04
Publication date: 2008-11-05
Anticipated expiration: 2017-11-04

Abstract

The utility model relates to a disk type passenger aircraft, which mainly overcomes the problems of poor structural strength, no self-help facility and easy break and explosion during forced landing in prior art. The utility model is characterized in that: the two sides of an aircraft body (1) are connected with a canard inclined ladder type flap (2); a twin-finned tailpiece (9) is positioned on the flap (2); an engine is positioned at the rear section of the flap (2); a rotary engine (4) is positioned on the external side of the two flaps (2); a column-shaped buffering gas cell (6) is respectively arranged on the external side and internal side of the flap (2); two main parachutes (3) are positioned respectively on the front section and the rear section on the airship body (1); the main parachute (3) is arranged respectively on the flap (2) at two sides; a spoiler (7) is respectively arranged on the flap (2) at two sides; an emergency control system is positioned inside the airship body. Therefore, the utility model has the advantages of high strength, excellent safety performance, large carrying capacity and fast speed.

Description

Dish formula passenger plane

Technical field:

The utility model relates to a kind of aircraft, particularly relates to a kind of dish formula passenger plane.

Background technology:

At present, it is cylindric that the passenger plane fuselage all is streamline, though empty resistance is little very fragile, it is widely different that external force is born in each position of fuselage, and when generation airplane crash forced landing, because housing construction intensity is low, fracture, blast are unavoidably.

The utility model content:

Low in order to overcome existing passenger plane housing construction intensity, there is not the facility of saving oneself, when the airplane crash forced landing takes place when, the deficiency of body easy fracture, blast, the utility model provides a kind of dish formula passenger plane, and this dish formula passenger plane has passenger plane bulk strength height, safety performance is good, bearing capacity is big, fireballing characteristics.

The technical solution of the utility model is: this dish formula passenger plane, relate to jetliner, the whole connection of the both sides of fuselage plunderred canard inclined ladder shape wing flap, and the twin vertical fin wing is set above the wing flap, driving engine is installed in fuselage or wing flap rear end, and the two wing flaps outside is equipped with can reverse driving engine.

The above-mentioned wing flap inboard and the outside are respectively equipped with the column buffering and hit air bag; Two main chutes are set before and after back; Main chute is set respectively on the wing flap of both sides; Flaps is set respectively on the wing flap of both sides; Emergent control system is installed in aircraft.

The utlity model has following beneficial effect: owing to take such scheme, fuselage designs is become preceding triangle dish formula structure, transfer fuselage to wing, increase the lift area of thrust surface, improve the intensity of aircraft, simultaneously, adopt dish formula fuselage, aerodynamic arrangement's excellence, for aircraft provides more practical space, under the combined action of additional prevention and control system, can realize that modern airliner vertically force-lands, promptly low the damage force-landed.Under states such as no complicated meteorology, landform, can make aircraft micro-damage, personnel not have injures and deaths.Thereby realized fast, efficient, safe beneficial effect.

Description of drawings:

Accompanying drawing 1 is a schematic top plan view of the present utility model;

Accompanying drawing 2 is that master of the present utility model looks scheme drawing;

Accompanying drawing 3 is that scheme drawing is looked on a left side of the present utility model.

1-fuselage among the figure, the 2-wing flap, the 3-main chute, 4-can reverse driving engine, the 5-driving engine, 6-column buffering is hit air bag, 7-flaps, 8-driving engine, the 9-twin vertical fin wing.

The specific embodiment:

The utility model is described in further detail below in conjunction with accompanying drawing:

By Fig. 1 in conjunction with Fig. 2; shown in Figure 3; a kind of dish formula passenger plane; the whole connection of the both sides of fuselage 1 plunderred canard inclined ladder shape wing flap 2; the twin vertical fin wing 9 is set above the wing flap 2; driving engine 8 is installed in fuselage 1 or wing flap 2 rear ends; two wing flaps, 2 outsides are equipped with can reverse driving engine 4; the driving engine of installing with fuselage 1 front end constitutes a dynamic level stabilization system; utilize the discontinuous start and stop or change takeoff output; the realization level is upwards lifted the order ground of aircraft; thereby alleviate passenger plane deadweight pressure, safe parachute-opening is achieved, finally rely on the downward resistance of main chute 3 and the driving engine thrust that makes progress and make passenger plane stable landing ground main chute 3.

Two main chutes 3 are set before and after fuselage 1 top; Main chute 3 is set respectively on the both sides wing flap 2, and the pulling force of main chute 3 can not be held, and mainly depends on driving engine 4 and driving engine 5 actings.But one of effect balance fuselage, the generation rate of minimizing changes in balance vector can slow down the gravity that aircraft is fallen in addition.Flaps 7 is set respectively on the both sides wing flap 2.Sweepforward canard inclined ladder shape wing flap 2 and upper and lower four groups of flaps 7 can promote the short take-off and landing (STOL) performance of passenger plane efficiently and turn to maneuvering performance in the air.Under the emergency episode situation, can reduce the flight speed of a ship or plane fast, and then for vertically lifting passenger plane, slowing down and open emergent main chute 3 pressure.Wing flap 2 inboards and the outside are respectively equipped with the column buffering and hit air bag 6, can increase the empty area that hinders in the second half section of slowing down, and can provide buffering for the forced landing stage again.Serve as the buoyancy airbag during marine the forced landing.Emergent control system is installed in aircraft, can be prevented that passenger plane is controlled by a bad actor.In addition, can make aircraft balanced be decelerated to static relatively or balance converting motion direction, densely populated area, high mountain, forest etc. are avoided in the comparatively safe location of force-landing; Can control simultaneously the unlatching opportunity that the column buffering is hit air bag and main chute, balanced in plane is lifted aircraft and is avoided upset to topple.This control system can reduce to greatest extent controls error and the artificial possibility that causes serious consequence out of control.

Claims

1, a kind of dish formula passenger plane, relate to jetliner, it is characterized in that: the whole connection of the both sides of fuselage (1) plunderred canard inclined ladder shape wing flap (2), the twin vertical fin wing (9) is set above the wing flap (2), driving engine (8) is installed in fuselage (1) or wing flap (2) rear end, and two wing flaps (2) outside is equipped with can reverse driving engine (4).

2, dish formula passenger plane according to claim 1 is characterized in that: wing flap (2) inboard and the outside are respectively equipped with the column buffering and hit air bag (6).

3, dish formula passenger plane according to claim 1 is characterized in that: two main chutes (3) are set before and after fuselage (1) top.

4, dish formula passenger plane according to claim 1 is characterized in that: main chute (3) is set respectively on the both sides wing flap (2).

5, dish formula passenger plane according to claim 1 is characterized in that: flaps (7) is set respectively on the both sides wing flap (2).

6, dish formula passenger plane according to claim 1 is characterized in that: emergent control system is installed in aircraft.