CN211207601U

CN211207601U - Airplane cockpit model for drilling simulation

Info

Publication number: CN211207601U
Application number: CN201921692916.2U
Authority: CN
Inventors: 梁源; 王瑞; 孙晔; 向新
Original assignee: Air Force Engineering University of PLA
Current assignee: Air Force Engineering University of PLA
Priority date: 2019-10-11
Filing date: 2019-10-11
Publication date: 2020-08-07
Anticipated expiration: 2029-10-11

Abstract

The utility model relates to a flight simulation equipment technical field just discloses an aircraft cockpit model for rehearsal simulation, the on-line screen storage device comprises a base, the rotation groove has been seted up at the top of base, and the inside fixedly connected with of base rotates the motor. This an aircraft cockpit model for rehearsal simulation, it makes the turning block rotate to rotate through rotating the motor circular telegram, the movable rod is on the inclined plane when the turning block rotates, the thru hole, the guide way, reciprocating motion about being under the combined action of guide block and reset spring, the mounting panel is at the activity groove this moment, the combined action of mounting block and movable rod is down moved, the mounting panel is rotatory and reciprocating combined motion from top to bottom with the central point department of putting of activity groove, the jolt of simulation aircraft when flying, make the pilot can adapt to the condition of jolting after the aircraft is last, the device makes the scene of jolting when the flight can be imitated to the cockpit of original stillness through a series of mechanical structure, make pilot training effect better.

Description

Airplane cockpit model for drilling simulation

Technical Field

The utility model relates to a flight simulation equipment technical field specifically is an aircraft cockpit model for rehearsal simulation.

Background

The airplane pilot refers to a person piloting the airplane, and the work content is as follows: the device is in charge of the driving work of the airplane to ensure the safety of navigation; the flight control system is responsible for handling accidents and emergencies on the airplane and changing the course according to the upper-level command to ensure the safety of the airplane when meeting the emergencies, wherein an airplane pilot, namely a pilot, is a technical post in the airplane driving career and is the core human resource of an airline company, the career of the pilot is divided into three stages, namely a flight student, a copilot and a captain, and the flight student stage is the first step of the career of the pilot, receives ground theoretical training and flight training and enjoys welfare assistance and training wage rights; after the university of the aviation, the flight trainee enters an airline company to carry out model modification training, and after the modification training is finished, the flight trainee can go to the seat to observe, pilot the airplane and accumulate experience to become a copilot; the copilot obtains the opportunity of examining the titles of the captain by accumulating flight hours within 5-10 years, and becomes the captain by examination.

The method is characterized in that the metal of the cockpit of the airplane is used for simulating flight when a pilot is in real operation, and the pilot is skillfully operated on the airplane in the mode, so that the accident rate is reduced when the pilot is in real operation, but the cockpit of the airplane on the market cannot simulate the condition of airplane jolting when in use, and the pilot cannot well face the specific condition due to too monotonous flight simulation during real operation, so that the training effect is reduced, and therefore the problem is solved by providing the cockpit model for practicing simulation.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

Not enough to prior art, the utility model provides an aircraft cockpit model for rehearsal simulation possesses advantages such as training effect is good, has solved the not enough problem of training effect.

(II) technical scheme

For realizing the good purpose of above-mentioned training effect, the utility model provides a following technical scheme: an aircraft cockpit model for rehearsal simulation comprises a base, wherein a rotating groove is formed in the top of the base, a rotating motor is fixedly connected inside the base, an output shaft of the rotating motor is fixedly connected with a rotating shaft extending to the inside of the rotating groove, a rotating block positioned inside the rotating groove is fixedly connected to the top of the rotating shaft, a limiting groove is formed in the top of the base, a limiting block extending to the upper part of the base is movably connected to the inside of the limiting groove, a mounting plate is movably connected to the top of the limiting block, a fixing plate is fixedly connected to the inside of the rotating groove, through holes are formed in the top of the fixing plate, guide grooves formed in the fixing plate are formed in the left side wall and the right side wall of each through hole, a movable rod penetrating through the through holes and extending to the lower part of the fixing plate is inserted into the top, the baffle that is located both sides about the fixed plate has been cup jointed to the outside of movable rod, and the upper and lower both sides of movable rod all inlay the rotatory piece that is equipped with respectively and contacts with mounting panel and turning block, upper and lower both sides the reset spring that the equal fixedly connected with in the relative one side of baffle is connected with the fixed plate, and the movable groove has been seted up at the top of fixed plate, and the inside swing joint in movable groove has the installation piece that is connected with the mounting panel, the top fixedly connected with cockpit of mounting panel.

Preferably, the spacing groove is four in total, four the spacing groove is annular equidistance and distributes, and the diameter at spacing groove top is less than the diameter of spacing groove bottom.

Preferably, the limiting block is composed of a vertical rod and a spherical limiting block, the vertical rod is fixedly connected to the top of the spherical limiting block, and the limiting block is larger than the limiting groove in depth.

Preferably, the number of the through holes is four, the four through holes are distributed in a ring shape at equal intervals, and the heights of the four movable rods are different.

Preferably, the rotating block is a cylindrical block, the top of the rotating block is an inclined plane, and the inclined angle of the inclined plane is thirty degrees.

Preferably, the mounting block consists of a cylindrical rod and a spherical block, and the top of the spherical block is fixedly connected with the cylindrical rod.

(III) advantageous effects

Compared with the prior art, the utility model provides an aircraft cockpit model for rehearsal simulation possesses following beneficial effect:

this an aircraft cockpit model for rehearsal simulation, it makes the turning block rotate to rotate through rotating the motor circular telegram rotation, the movable rod is on the inclined plane when the turning block rotates, the thru hole, the guide way, reciprocating motion about being under the combined action of guide block and reset spring, the mounting panel is at the activity groove this moment, the combined action of mounting block and movable rod is down moved, the mounting panel is rotatory and reciprocating combined motion from top to bottom with the central point department of putting of activity groove, the jolt of simulation aircraft when flying, thereby make the pilot can adapt to the condition of jolting after the aircraft is last, the device makes the scene of jolting when the flight can be imitated to the cockpit of original stillness through a series of mechanical structure, thereby make pilot training effect better.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is an enlarged schematic view of the point A in the structure of FIG. 1 of the present invention;

fig. 3 is an enlarged schematic view of the position B in the structure diagram 1 of the present invention.

In the figure: the device comprises a base 1, a rotating groove 2, a rotating motor 3, a rotating shaft 4, a rotating block 5, a fixing plate 6, a movable groove 7, an installation block 8, an installation plate 9, a limiting groove 10, a limiting block 11, a through hole 12, a guide groove 13, a movable rod 14, a guide block 15, a return spring 16, a baffle 17, a rotating block 18 and a cockpit 19.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-3, an airplane cockpit model for rehearsal simulation comprises a base 1, a rotating groove 2 is formed at the top of the base 1, a rotating motor 3 is fixedly connected inside the base 1, the model of the rotating motor 3 can be YE2, an output shaft of the rotating motor 3 is fixedly connected with a rotating shaft 4 extending into the rotating groove 2, a rotating block 5 positioned inside the rotating groove 2 is fixedly connected to the top of the rotating shaft 4, the rotating block 5 is a cylindrical block, the top of the rotating block 5 is an inclined plane, the inclined plane has thirty degrees, a limiting groove 10 is formed at the top of the base 1, four limiting grooves 10 are formed, the four limiting grooves 10 are distributed in an annular equidistant manner, the diameter of the top of the limiting groove 10 is smaller than that of the bottom of the limiting groove 10, a limiting block 11 extending above the base 1 is movably connected inside the limiting groove 10, the limiting block 11 is composed of a vertical rod and a spherical limiting block, the top of the spherical limiting block is fixedly connected with a vertical rod, the height of the limiting block 11 is greater than the depth of the limiting groove 10, the top of the limiting block 11 is movably connected with a mounting plate 9, a fixed plate 6 is fixedly connected in a rotating groove 2, the top of the fixed plate 6 is provided with through holes 12, the through holes 12 are four in total, the four through holes 12 are distributed in an annular equal distance, the heights of the four movable rods 14 are different, the left side wall and the right side wall in the through holes 12 are respectively provided with a guide groove 13 arranged in the fixed plate 6, the top of the fixed plate 6 is inserted with a movable rod 14 which penetrates through the through holes 12 and extends to the lower part of the fixed plate 6, the left side and the right side of the movable rod 14 are respectively fixedly connected with a guide block 15 extending to the inner part of the guide groove 13, the outer part of the movable rod 14 is sleeved with baffle, the opposite sides of the upper side baffle 17 and the lower side baffle 17 are fixedly connected with a return spring 16 connected with the fixed plate 6, the top of the fixed plate 6 is provided with a movable groove 7, the inner part of the movable groove 7 is movably connected with an installation block 8 connected with an installation plate 9, the installation block 8 consists of a cylindrical rod and a spherical block, the top of the spherical block is fixedly connected with the cylindrical rod, the top of the installation plate 9 is fixedly connected with a cockpit 19, the rotating block 5 rotates by electrifying the rotating motor 3, the movable rod 14 moves up and down under the combined action of the inclined surface, the through hole 12 and the guide groove 13 when the rotating block 5 rotates, the guide block 15 and the return spring 16, the installation plate 9 moves under the combined action of the movable groove 7, the installation block 8 and the movable rod 14, the installation plate 9 rotates and moves up and down and back and forth at the central position of the movable groove 7 to simulate the jolt, therefore, the pilot can adapt to the situation of the airplane bumping after the day, and the device enables the originally static cockpit 19 to simulate the scene of bumping during flying through a series of mechanical structures, so that the training effect of the pilot is better.

To sum up, this an aircraft cockpit model for rehearsal simulation, it makes the turning block 5 rotate to rotate through turning motor 3 circular telegram, moving rod 14 is at the inclined plane when turning block 5 rotates, thru hole 12, guide way 13, guide block 15 and reset spring 16's combined action is reciprocating motion from top to bottom, mounting panel 9 is at moving chute 7 this moment, the combined action of mounting block 8 and moving rod 14 is down moved, mounting panel 9 is rotatory and reciprocating combined motion from top to bottom with the central point department of moving chute 7, the jolt of simulation aircraft when the flight, thereby make the pilot can adapt to the condition of jolt in the last day of the aircraft, the device makes the scene of jolt when the flight of cockpit 19 that originally motionless can be imitated through a series of mechanical structure, thereby make the pilot training effect better, the problem that the training effect is not enough has been solved.

It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. An aircraft cockpit model for drilling simulations, comprising a base (1), characterized in that: rotation groove (2) have been seted up at the top of base (1), and the inside fixedly connected with of base (1) rotates motor (3), and the output shaft fixedly connected with of rotating motor (3) extends to and rotates pivot (4) of groove (2) inside, and the top fixedly connected with of pivot (4) is located and rotates turning block (5) of groove (2) inside, spacing groove (10) have been seted up at the top of base (1), and the inside swing joint of spacing groove (10) has stopper (11) that extend to base (1) top, and the top swing joint of stopper (11) has mounting panel (9), rotate groove (2) inslot fixedly connected with fixed plate (6), thru hole (12) have been seted up at the top of fixed plate (6), all install on the downthehole left and right sides wall of thru hole (12) and set up guide way (13) inside fixed plate (6), the top grafting of fixed plate (6) has run through (12) and extend to fixed plate (6) below The utility model discloses a safety device, including movable rod (14), the equal fixedly connected with in the left and right sides of movable rod (14) extends to inside guide block (15) of guide way (13), and baffle (17) that are located both sides about fixed plate (6) have been cup jointed to the outside of movable rod (14), and the upper and lower both sides of movable rod (14) all inlay and be equipped with rotatory piece (18) that contact with mounting panel (9) and turning block (5) respectively, upper and lower both sides the reset spring (16) that the equal fixedly connected with in one side is connected with fixed plate (6) relatively of baffle (17), movable groove (7) have been seted up at the top of fixed plate (6), and the inside swing joint of movable groove (7) has installation piece (8) that are connected with mounting panel (9), top fixedly connected with cockpit (19) of mounting.

2. An aircraft cockpit model for a drilling simulation according to claim 1 where: the limiting groove (10) is four in total, four the limiting groove (10) is distributed in an annular equidistance mode, and the diameter of the top of the limiting groove (10) is smaller than that of the bottom of the limiting groove (10).

3. An aircraft cockpit model for a drilling simulation according to claim 1 where: the limiting block (11) is composed of a vertical rod and a spherical limiting block, the vertical rod is fixedly connected to the top of the spherical limiting block, and the height of the limiting block (11) is larger than the depth of the limiting groove (10).

4. An aircraft cockpit model for a drilling simulation according to claim 1 where: the number of the through holes (12) is four, the four through holes (12) are distributed in a ring shape at equal intervals, and the heights of the four movable rods (14) are different.

5. An aircraft cockpit model for a drilling simulation according to claim 1 where: the rotating block (5) is a cylindrical block, the top of the rotating block (5) is an inclined plane, and the inclined angle of the inclined plane is thirty degrees.

6. An aircraft cockpit model for a drilling simulation according to claim 1 where: the mounting block (8) is composed of a cylindrical rod and a spherical block, and the top of the spherical block is fixedly connected with the cylindrical rod.