CN217386533U

CN217386533U - Novel flight simulation training cabin

Info

Publication number: CN217386533U
Application number: CN202220390311.3U
Authority: CN
Inventors: 李雨生; 罗伟; 王涛; 荣宏; 杨小宇
Original assignee: Sichuan Guanyu Xinrun Technology Co ltd
Current assignee: Sichuan Guanyu Xinrun Technology Co ltd
Priority date: 2022-02-25
Filing date: 2022-02-25
Publication date: 2022-09-06
Anticipated expiration: 2032-02-25

Abstract

The utility model discloses a novel flight emulation training cabin, include the cabin body and set up in the base of cabin body bottom, the bottom of the cabin body is equipped with the ball template, and forms the resistance space between the ball template and the cabin body, the bottom and the base fixed connection of ball core board, be equipped with the counter weight ball that can freely remove on the ball template, still be equipped with the viscous mechanism that produces the resistance to the counter weight ball in the ball template, this novel flight emulation training cabin sets up a spherical ball template through the bottom in the training cabin and constructs a space, has counter weight ball 4 in this space, and when the counter weight ball rocks along with the base at the cabin body, can produce certain inertia volume, simulate out the flight condition under the real environment, and because viscous mechanism's setting makes the counter weight ball can not rock fast and cause the very big condition of rocking to appear, thereby cause the damage of the cabin body.

Description

Novel flight simulation training cabin

Technical Field

The utility model belongs to training cabin field, specifically speaking relates to a novel flight emulation training cabin.

Background

The flight simulator is a satellite flight control closed-loop simulation system based on a component simulator, and is applied to a system comprising a dynamic simulation server, a sensor simulator, an actuator simulator and a satellite-borne computer. The flight simulator is to construct a virtual 'real' flight environment for the pilot. The environment here refers primarily to two parts: on the one hand, the machine environment, i.e. the aircraft cockpit, the plant, etc.; another aspect is the external environment, mainly referring to natural conditions, geographical conditions, etc.

The existing flight training cabin is mainly a cabin body simulated in an airplane control cabin, a control base connected with the cabin body is arranged at the bottom of the cabin body, and the control base is used for changing the inclination angle of the cabin body to enable the cabin body to generate shaking feeling, so that the flying feeling is generated.

SUMMERY OF THE UTILITY MODEL

The utility model discloses the technical problem who solves lies in overcoming prior art not enough, provides a novel flight emulation training cabin, for solving above-mentioned technical problem, the utility model discloses a technical scheme's basic design is:

the utility model provides a novel flight emulation training cabin, includes the cabin body and sets up in the base of cabin body bottom, the bottom of the cabin body is equipped with the ball template, and forms the resistance space between ball template and the cabin body, the bottom and the base fixed connection of ball template, be equipped with the counter weight ball that can freely remove on the ball template, still be equipped with the viscous mechanism to counter weight ball production resistance in the ball template.

The viscous mechanism comprises a magnetic part arranged on the ball-shaped plate, and the counterweight ball is provided with a metal block adsorbed with the magnetic part or is arranged inside the counterweight ball.

The viscous mechanism comprises a first magic tape arranged on the upper surface of the spherical plate, and a second magic tape matched with the first magic tape is arranged on the outer surface of the counterweight ball.

The upper surface of the ball-shaped plate is also provided with an annular groove, and is connected with a limiting ring through the annular groove, and the limiting ring limits the counterweight ball in the inner ring of the counterweight ball.

The counterweight ball is a shot ball, and a buffer layer wrapping the counterweight ball is further arranged between the second magic tape and the counterweight ball.

Compared with the prior art, the utility model following beneficial effect has:

a space is constructed by arranging a spherical ball-shaped plate at the bottom of the training cabin, a counterweight ball is arranged in the space, when the cabin body shakes along with the base, the counterweight ball can generate a certain inertia quantity to simulate the flight condition under the real environment, and the counterweight ball cannot shake quickly to cause the appearance of a large shaking condition due to the arrangement of a viscous mechanism, so that the cabin body is damaged.

The following describes embodiments of the present invention in further detail with reference to the accompanying drawings.

Drawings

In the drawings:

FIG. 1 is a schematic view of the bottom structure of the cabin as a whole;

FIG. 2 is a schematic view of a half-section structure of the bottom of the cabin;

fig. 3 is a development schematic view of the structure on the spherical plate.

In the figure: 1-a cabin body; 2-a base; 3-a spherical plate; 4-a counterweight ball; 5-a viscous mechanism; 6-first magic tape; 7-a second magic tape; 8-an annular groove; 9-a limit ring.

Detailed Description

In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and the following embodiments are used to illustrate the present invention.

As shown in fig. 1 to 3, a novel flight simulation training cabin comprises a cabin body 1 and a base 2 arranged at the bottom of the cabin body 1, wherein a spherical plate 3 is arranged at the bottom of the cabin body 1, a resistance space is formed between the spherical plate 3 and the cabin body 1, the bottom of the spherical plate is fixedly connected with the base 2, a freely movable counterweight ball 4 is arranged on the spherical plate 3, and the counterweight ball 4 has the function of generating certain inertia when the cabin body of the flight training cabin shakes, so that shaking operation in a simulation state is completely derived from telescopic matching of a telescopic rod on the base 2, but in reality, during switching of inclination in different directions, the counterweight ball has inertia, and cannot simulate a real situation to generate an error on the real situation during simulation, so that the simulation training effect is influenced, a viscous mechanism 5 for generating resistance to the counterweight ball 4 is further arranged in the spherical plate 3, and the viscous mechanism 5 has the function of preventing the counterweight ball 4 from rapidly rolling, therefore, inertia is related to the mass of the cabin, but if no resistance exists, the kinetic energy of the cabin is larger and larger, and then larger impact is generated on the bottom of the cabin, so that the inertia effect cannot be achieved, impact can be generated, and the normal use of the cabin is influenced.

Viscous mechanism 5 is including setting up the magnetic part on ball template 3, just counterweight ball 4 itself or inside be equipped with the magnetic part absorptive metal block, the magnetic part refers to mechanisms such as permanent magnet or electro-magnet, and the magnetic part mainly concentrates the intermediate position that sets up in ball template 3, because rocking along with base 1 of ball template 3, can constantly change the position of magnetic part, thereby order about rocking of counterweight ball 4, both rock and can not be completely synchronous, counterweight ball 4 can have the delay, thereby simulate out and have inertial sensation.

The viscous mechanism 5 comprises a first magic tape 6 arranged on the upper surface of the ball-shaped plate 3, a second magic tape 7 matched with the first magic tape 6 is arranged on the outer surface of the counterweight ball 4, the viscous mechanism is different from a magnetic part by adopting a magic tape mode, because the magnetic part may affect the instruments in the training cabin, the magic tapes are adopted, the contact of the two magic tapes can generate viscous force, thereby achieving the same effect, and the magic tape can also avoid the noise generated when the counterweight ball 4 rolls, and avoid the abnormal sound from influencing the judgment of the trainer, the counterweight ball 4 is a shot, and still be equipped with the buffer layer of parcel counter weight ball 4 between second magic subsides 7 and the counter weight ball 4, the effect of buffer layer mainly plays the buffering, prevents to rock too big kinetic energy that causes counter weight ball 4 because making a round trip and produces great impact to cabin body 1, and then causes the damage.

Annular groove 8 has still been seted up to the upper surface of spherical template 3, and is connected with spacing ring 9 through annular groove 8, and spacing ring 9 limits counter weight ball 4 in its inner circle, and annular groove 8 protects as a bank, directly avoids counter weight ball 4 to contact cabin body 1 in the source, and then just can not cause the impact, avoids the problem of striking in the root.

The cabin body 1 of the training cabin shakes under the action of the telescopic rod on the base, the counterweight balls inside the training cabin roll when shaking, and the counterweight balls can move with the cabin body 1 when rolling, so that the flight condition similar to real flight condition is simulated, and the simulation effect of pilots is improved.

Claims

1. The utility model provides a novel flight emulation training cabin, includes the cabin body (1) and sets up in base (2) of the cabin body (1) bottom, its characterized in that, the bottom of the cabin body (1) is equipped with ball template (3), and forms the resistance space between ball template (3) and the cabin body (1), the bottom and base (2) fixed connection of ball template (3), be equipped with counter weight ball (4) that can freely remove on ball template (3), still be equipped with viscous mechanism (5) to counter weight ball (4) production resistance in ball template (3).

2. The novel flight simulation training cabin according to claim 1, wherein the viscous mechanism (5) comprises a magnetic member arranged on the ball-shaped plate (3), and the counterweight ball (4) is provided with a metal block attached to the magnetic member.

3. The novel flight simulation training cabin according to claim 1, wherein the viscous mechanism (5) comprises a first magic tape (6) arranged on the upper surface of the ball shaping plate (3), and a second magic tape (7) matched with the first magic tape (6) is arranged on the outer surface of the counterweight ball (4).

4. The novel flight simulation training cabin according to claim 1, wherein an annular groove (8) is further formed in the upper surface of the ball-shaped plate (3), a limiting ring (9) is connected to the annular groove (8), and the limiting ring (9) limits the counterweight ball (4) to the inner ring of the limiting ring.

5. The novel flight simulation training cabin according to claim 3, wherein the counterweight ball (4) is a shot ball, and a buffer layer wrapping the counterweight ball (4) is further arranged between the second magic tape (7) and the counterweight ball (4).