阅读说明：本技术 一种具有安全防护的空中飞行列车 (Aerial flying train with safety protection ) 是由 何彬生 邴萍萍 于 2021-08-11 设计创作，主要内容包括：本发明公开了一种具有安全防护的空中飞行列车,包括飞机本体,飞机本体的顶部设置有承载箱,承载箱的内部固定安装有第一降落伞,飞机本体的内部设置有多个座椅,座椅的底部设置有连接装置,座椅的底部安装有飞行器,座椅的背面安装有第二降落伞,第二降落伞的一侧固定连接有拉环,飞机本体的底部安装有三个支撑轮组,连接装置包括两个第一连接板,第一连接板外壁的底部滑动套接有滑轨。本发明利用第一降落伞、第二降落伞和飞行器的设置方式,当飞机本体遇到突发情况时,第一降落伞可以对飞机本体进行减速下降,第二降落伞和飞行器可以使座椅带动乘客与飞机本体分离,然后进行跳伞降落,从而提高其安全性能。(The invention discloses an aerial flying train with safety protection, which comprises an airplane body, wherein a bearing box is arranged at the top of the airplane body, a first parachute is fixedly arranged inside the bearing box, a plurality of seats are arranged inside the airplane body, a connecting device is arranged at the bottoms of the seats, an aircraft is arranged at the bottom of each seat, a second parachute is arranged at the back of each seat, one side of each second parachute is fixedly connected with a pull ring, three supporting wheel sets are arranged at the bottom of the airplane body, each connecting device comprises two first connecting plates, and a slide rail is sleeved at the bottom of the outer wall of each first connecting plate in a sliding mode. According to the invention, by utilizing the arrangement mode of the first parachute, the second parachute and the aircraft, when the aircraft body meets an emergency, the first parachute can decelerate and descend the aircraft body, and the second parachute and the aircraft can enable the seat to drive the passenger to be separated from the aircraft body and then parachute jumping and landing are carried out, so that the safety performance of the aircraft is improved.)

1. The utility model provides an aerial train with safety protection, includes aircraft body (1), its characterized in that, the top of aircraft body (1) is provided with bearing box (2), the inside fixed mounting of bearing box (2) has first parachute, the inside of aircraft body (1) is provided with a plurality of seats (3), the bottom of seat (3) is provided with connecting device (4), aircraft (8) are installed to the bottom of seat (3), the back mounted of seat (3) has second parachute (6), one side fixedly connected with pull ring (7) of second parachute (6), three support wheelset (5) are installed to the bottom of aircraft body (1).

2. The air-flight train with safety protection according to claim 1, wherein the connecting device (4) comprises two first connecting plates (41), the top of the first connecting plates (41) is fixedly connected with the seat (3), a sliding rail (42) is slidably sleeved at the bottom of the outer wall of the first connecting plates (41), a plurality of positioning rods (43) are slidably and alternately sleeved on one side of the sliding rail (42) at equal intervals, and the outer wall of each positioning rod (43) is slidably and alternately sleeved with the first connecting plates (41).

3. The air-borne flight train with safety protection as claimed in claim 2, wherein mounting plates (44) are arranged on opposite sides of the two slide rails (42), air cylinders (45) are fixedly mounted on opposite sides of the two mounting plates (44), second connecting plates (46) are arranged on opposite sides of the two mounting plates (44), one end of the positioning rod (43) is fixedly connected with the second connecting plates (46), the output end of the air cylinder (45) is in transmission connection with the second connecting plates (46), and a power switch is mounted on one side of the top of one of the slide rails (42).

4. The aerial flying train with safety protection as claimed in claim 3, wherein the bottoms of the two sides of the slide rail (42) are fixedly connected with a plurality of fixing blocks (47) at equal intervals, the top of each fixing block (47) is provided with a first fixing bolt (48), the fixing blocks (47) are fixedly connected with the aircraft body (1) through the first fixing bolts (48), the bottom of the mounting plate (44) is fixedly connected with a first fixing plate (49), four corners of the top of the first fixing plate (49) are provided with second fixing bolts (410), and the first fixing plate (49) is fixedly connected with the aircraft body (1) through the second fixing bolts (410).

5. The aerial flying train with the safety protection function as claimed in claim 1, wherein the supporting wheel set (5) comprises a bracket (51), the top of the bracket (51) is fixedly mounted with the aircraft body (1), a main shaft (52) is arranged at the bottom of the bracket (51), and rollers (53) are rotatably connected to both ends of the outer wall of the main shaft (52).

6. The aerial flying train with safety protection as claimed in claim 5, wherein a bearing groove is formed in the bottom of the support (51), a support rod (54) is slidably sleeved in an inner cavity of the bearing groove, the bottom of the support rod (54) is fixedly connected with the main shaft (52), a positioning sleeve ring (55) is fixedly sleeved in the bottom of the inner cavity of the bearing groove, a limiting sleeve ring (56) is fixedly sleeved on an outer wall of the support rod (54), a spring (57) is slidably sleeved in the bottom of the outer wall of the support rod (54), a tension spring (58) is slidably sleeved in the top of the outer wall of the support rod (54), and a rubber block (511) is fixedly connected to the top of the support rod (54).

7. The aerial flying train with the safety protection function as claimed in claim 6, wherein the bottom of the tension spring (58) is fixedly connected with a limiting sleeve ring (56), the top of the tension spring (58) is fixedly connected with the top of the inner wall of the bearing groove, the spring (57) is located between the limiting sleeve ring (56) and the positioning sleeve ring (55), the outer wall of the limiting sleeve ring (56) is symmetrically and fixedly connected with sliding blocks (59), sliding grooves (510) are symmetrically formed in the bearing groove, and the outer wall of each sliding block (59) is slidably sleeved with the inner cavity of each sliding groove (510).

8. The aerial flying train with the safety protection function as claimed in claim 1, wherein an arc plate (9) is arranged in the middle of the upper surface of the airplane body (1), the top of the arc plate (9) is fixedly connected with the bearing box (2), the bottoms of two sides of the arc plate (9) are fixedly connected with a second fixing plate (10), the top of the second fixing plate (10) is fixedly connected with a reinforcing rib, a plurality of third fixing bolts are equidistantly arranged on two sides of the top of the second fixing plate (10), and the second fixing plate (10) is fixedly connected with the airplane body (1) through the third fixing bolts.

Technical Field

The invention relates to the field of flying trains, in particular to an aerial flying train with safety protection.

Background

The airplane is one of the most important inventions in the beginning of the 20 th century and can be divided into two categories, namely a military airplane and a civil airplane according to the purposes. The invention of the airplane profoundly changes and influences the life of people, increasingly becomes an indispensable vehicle of modern civilization, and when the airplane is used in flight, the airplane has the risk of crash due to various external factors, so that the air train with safety protection is designed, and the safety problem that passengers can be ensured when the airplane is in flight, meets emergency and lands is solved.

Disclosure of Invention

The invention aims to provide an aerial flying train with safety protection, so as to solve the problems in the background technology.

In order to achieve the purpose, the invention provides the following technical scheme: the utility model provides an aerial train with safety protection, includes the aircraft body, the top of aircraft body is provided with the bearing box, the inside fixed mounting of bearing box has first parachute, the inside of aircraft body is provided with a plurality of seats, the bottom of seat is provided with connecting device, the aircraft is installed to the bottom of seat, the back mounted of seat has the second parachute, one side fixedly connected with pull ring of second parachute, three support wheelset is installed to the bottom of aircraft body.

Preferably, the connecting device comprises two first connecting plates, the top of each first connecting plate is fixedly connected with the seat, the bottom of the outer wall of each first connecting plate is slidably sleeved with a sliding rail, a plurality of positioning rods are slidably and alternately sleeved on one side of the sliding rail at equal intervals, and the outer wall of each positioning rod is slidably and alternately sleeved with the first connecting plate.

Preferably, two one side that the slide rail is relative all is provided with the mounting panel, two the equal fixed mounting in one side that the mounting panel is relative has the cylinder, two one side that the mounting panel is carried on the back mutually all is provided with the second connecting plate, the one end and the second connecting plate fixed connection of locating lever, the output and the second connecting plate transmission of cylinder are connected, one of them switch is installed to one side at slide rail top.

Preferably, a plurality of fixed blocks of the equal equidistance fixedly connected with in bottom of slide rail both sides, the top of fixed block is provided with first fixing bolt, the fixed block passes through first fixing bolt and aircraft body fixed connection, the first fixed plate of bottom fixedly connected with of mounting panel, four edges at first fixed plate top all are provided with second fixing bolt, first fixed plate passes through second fixing bolt and aircraft body fixed connection.

Preferably, the support wheel set comprises a support, the top of the support is fixedly mounted with the aircraft body, a main shaft is arranged at the bottom of the support, and two ends of the outer wall of the main shaft are rotatably connected with idler wheels.

Preferably, the bottom of support has been seted up and has been born the weight of the groove, the bracing piece has been cup jointed in the inner chamber slip of bearing the weight of the groove, the bottom and the main shaft fixed connection of bracing piece, the fixed position lantern ring that has cup jointed in bottom of bearing the weight of the inslot inner chamber, the fixed spacing lantern ring that has cup jointed of outer wall of bracing piece, the spring has been cup jointed in the bottom slip of bracing piece outer wall, the extension spring has been cup jointed in the top slip of bracing piece outer wall, the top fixedly connected with block rubber of bracing piece.

Preferably, the bottom and the spacing lantern ring fixed connection of extension spring, the top and the top fixed connection of bearing groove inner wall of extension spring, the spring is located between the spacing lantern ring and the position lantern ring, the outer wall symmetry fixedly connected with slider of the spacing lantern ring, the spout has been seted up to the inside symmetry of bearing groove, the outer wall of slider cup joints with the inner chamber slip of spout.

Preferably, the middle part of aircraft body upper surface is provided with the circular arc board, the top and the bearing box fixed connection of circular arc board, the equal fixedly connected with second fixed plate in bottom of circular arc board both sides, the muscle is reinforceed to the top fixedly connected with of second fixed plate, the equal equidistance in both sides side at second fixed plate top is provided with a plurality of third fixing bolt, the second fixed plate passes through third fixing bolt and aircraft body fixed connection.

The invention has the technical effects and advantages that:

(1) according to the invention, by utilizing the arrangement mode of the first parachute, the second parachute and the aircraft, when the aircraft body meets an emergency, the first parachute can decelerate and descend the aircraft body, the second parachute and the aircraft can enable the seat to drive passengers to be separated from the aircraft body, and then parachute jumping and landing are carried out, so that the safety performance is improved;

(2) the invention utilizes the arrangement mode of the supporting wheel set, and the supporting wheel set comprises the supporting frame, the roller, the supporting rod, the spring and the tension spring, so that the roller can buffer the landing of the airplane body through the supporting rod and the supporting frame, and the landing stability of the airplane body is improved.

Drawings

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

FIG. 2 is a schematic side view of the present invention.

Fig. 3 is a schematic side view of the seat of the present invention.

FIG. 4 is a schematic side view of the internal structure of the stent of the present invention.

In the figure: 1. an aircraft body; 2. a carrying case; 3. a seat; 4. a connecting device; 41. a first connecting plate; 42. a slide rail; 43. positioning a rod; 44. mounting a plate; 45. a cylinder; 46. a second connecting plate; 47. a fixed block; 48. a first fixing bolt; 49. a first fixing plate; 410. a second fixing bolt; 5. a support wheel set; 51. a support; 52. a main shaft; 53. a roller; 54. a support bar; 55. a positioning collar; 56. a limiting lantern ring; 57. a spring; 58. a tension spring; 59. a slider; 510. a chute; 511. a rubber block; 6. a second parachute; 7. a pull ring; 8. an aircraft; 9. a circular arc plate; 10. and a second fixing plate.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

The invention provides an aerial flying train with safety protection as shown in figures 1-4, which comprises an airplane body 1, wherein the manufacturing materials used by the airplane body 1 from inside to outside all belong to light rubber materials, and have the characteristics of fire prevention, explosion prevention and bullet prevention, and the probability of accidents of the airplane can be effectively reduced, the top of the airplane body 1 is provided with a bearing box 2, a first parachute is fixedly arranged inside the bearing box 2, a plurality of seats 3 are arranged inside the airplane body 1, the seats 3 are made of light materials, by utilizing an aircraft 8 and a second parachute 6, free flying landing can be automatically controlled when the airplane body 1 breaks down, even if the airplane falls into a water body, the airplane can utilize buoyancy, does not subside and safely land, the bottom of the seats 3 is provided with a connecting device 4, the bottom of the seats 3 is provided with the aircraft 8, and the back of the seats 3 is provided with the second parachute 6, one side fixedly connected with pull ring 7 of second parachute 6, three support wheelset 5 are installed to the bottom of aircraft body 1.

The connecting device 4 comprises two first connecting plates 41, the top of the first connecting plate 41 is fixedly connected with the seat 3, a slide rail 42 is sleeved at the bottom of the outer wall of the first connecting plate 41 in a sliding manner, a plurality of positioning rods 43 are sleeved at one side of the slide rail 42 in an equidistant sliding manner, the outer wall of each positioning rod 43 is sleeved with the first connecting plate 41 in a sliding manner, mounting plates 44 are arranged at the opposite sides of the two slide rails 42, air cylinders 45 are fixedly mounted at the opposite sides of the two mounting plates 44, a second connecting plate 46 is arranged at the opposite sides of the two mounting plates 44, one end of each positioning rod 43 is fixedly connected with the second connecting plate 46, the output end of each air cylinder 45 is in transmission connection with the second connecting plate 46, a power switch is mounted at one side of the top of one slide rail 42, the air cylinders 45 can be electrified by pressing down the power switch, and the positioning rods 43 are driven to be separated from the first connecting plates 41 by the second connecting plates 46, thereby make the passenger adopt second parachute 6 and aircraft 8 to descend, the equal equidistance a plurality of fixed blocks 47 of fixedly connected with in the bottom of slide rail 42 both sides, the top of fixed block 47 is provided with first fixing bolt 48, fixed block 47 is through first fixing bolt 48 and aircraft body 1 fixed connection, the first fixed plate 49 of bottom fixedly connected with of mounting panel 44, four edges at first fixed plate 49 top all are provided with second fixing bolt 410, first fixed plate 49 is through second fixing bolt 410 and aircraft body 1 fixed connection.

The supporting wheel set 5 comprises a support 51, the top of the support 51 is fixedly installed with the airplane body 1, a main shaft 52 is arranged at the bottom of the support 51, rollers 53 are rotatably connected to both ends of the outer wall of the main shaft 52, a bearing groove is formed in the bottom of the support 51, a supporting rod 54 is slidably sleeved in the inner cavity of the bearing groove, the bottom of the supporting rod 54 is fixedly connected with the main shaft 52, a positioning sleeve ring 55 is fixedly sleeved at the bottom of the inner cavity of the bearing groove, a limiting sleeve ring 56 is fixedly sleeved on the outer wall of the supporting rod 54, a spring 57 is slidably sleeved at the bottom of the outer wall of the supporting rod 54, a tension spring 58 is slidably sleeved on the top of the outer wall of the supporting rod 54, a rubber block 511 is fixedly connected to the top of the tension spring 58, the bottom of the tension spring 58 is fixedly connected with the top of the inner wall of the bearing groove, the spring 57 is positioned between the limiting sleeve ring 56 and the positioning sleeve ring 55, sliders 59 are symmetrically and fixedly connected to the outer wall of the limiting sleeve ring 56, the inside symmetry of bearing groove has seted up spout 510, and the outer wall of slider 59 and the inner chamber sliding sleeve of spout 510 cup joint, meet the accident at aircraft body 1, descend under the effect of first parachute, and gyro wheel 53 has ground contact, makes bracing piece 54 have a holding power to support 51, under the effect of extension spring 58 and spring 57, makes the effort that has a shock attenuation buffering between bracing piece 54 and the support 51 to improve the stability that aircraft body 1 landed.

The middle part of 1 upper surface of aircraft body is provided with circular arc board 9, the top and the bearing box 2 fixed connection of circular arc board 9, the equal fixedly connected with second fixed plate 10 in bottom of circular arc board 9 both sides, the muscle is reinforceed to the top fixedly connected with of second fixed plate 10, the equal equidistance in both sides side at second fixed plate 10 top is provided with a plurality of third fixing bolt, second fixed plate 10 passes through third fixing bolt and 1 fixed connection of aircraft body.

The working principle of the invention is as follows: when the aircraft body 1 flies and lands, the roller 53 is firstly contacted with the ground, so that the support rod 54 has a supporting force for the bracket 51, and under the action of the tension spring 58 and the spring 57, a damping and buffering acting force is formed between the support rod 54 and the bracket 51, so that the landing stability of the aircraft body 1 is improved.

When aircraft body 1 meets emergency, at first can open first parachute, cushion aircraft body 1's parachute, then press power button, make cylinder 45 circular telegram, and then make second connecting plate 46 drive a plurality of locating levers 43 and the separation of first connecting plate 41 to can remove seat 3 to aircraft body 1 outside, then open second parachute 6, and under aircraft 8's effect, make the passenger accomplish the motion of parachuting.

Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments or portions thereof without departing from the spirit and scope of the invention.