阅读说明：本技术 一种逻辑测试用飞行训练器 (Flight training ware is used in logic test ) 是由 黄欢 冯凌志 叶亮 梁琳 沈鑫 于 2021-06-04 设计创作，主要内容包括：本发明涉及一种逻辑测试用飞行训练器,包括安装机构和训练器,所述训练器设置在安装机构设的上方,所述训练器的内部设置有逻辑测试机,所述安装机构包括底板,所述底板的顶部设置有升降杆,所述升降杆的顶部设置有安装板,所述训练器包括训练舱,所述安装板的表面设置有与训练舱活动连接的立板,所述训练舱的表面且位于立板的内部固定安装有转向环,所述安装板的顶部且位于训练舱的底部固定安装有转向电机。该逻辑测试用飞行训练器,只需将逻辑测试机放置上去,利用紧固板下滑,用卡环将其固定即可,逻辑测试机与机舱操控器电连接,让逻辑测试机代替人工测试,由于逻辑测试机没有主观意思,因此检测出来的各方面数据均比人工测试更加准确。(The invention relates to a flight trainer for logic test, which comprises an installation mechanism and a trainer, wherein the trainer is arranged above the installation mechanism, a logic test machine is arranged inside the trainer, the installation mechanism comprises a bottom plate, a lifting rod is arranged at the top of the bottom plate, an installation plate is arranged at the top of the lifting rod, the trainer comprises a training cabin, a vertical plate movably connected with the training cabin is arranged on the surface of the installation plate, a steering ring is fixedly arranged on the surface of the training cabin and inside the vertical plate, and a steering motor is fixedly arranged at the top of the installation plate and at the bottom of the training cabin. This flight training ware is used in logic test only needs to place the logic test machine and go up, utilizes the mounting plate gliding, with the snap ring with its fixed can, the logic test machine is connected with cabin controller electricity, lets the logic test machine replace artifical test, because the logic test machine does not have subjective meaning, therefore all aspects data that detect are all more accurate than artifical test.)

1. A flight trainer for logic test comprises a mounting mechanism and a trainer, and is characterized in that the trainer is arranged above the mounting mechanism, and a logic tester (30) is arranged in the trainer;

installation mechanism includes bottom plate (10), the top of bottom plate (10) is provided with lifter (11), the top of lifter (11) is provided with mounting panel (12), the training ware is including training cabin (20), the surface of mounting panel (12) is provided with riser (21) with training cabin (20) swing joint, the inside fixed mounting that just is located riser (21) on the surface of training cabin (20) has steering ring (22), the bottom fixed mounting that just is located training cabin (20) at the top of mounting panel (12) has steering motor (23).

2. The flight training aid for the logic test according to claim 1, wherein bases are fixedly installed on the periphery of the bottom plate (10), fixing seats (111) rotatably connected with the lifting rod (11) are fixedly installed on the top of the bottom plate (10), and the number of the fixing seats (111) is four and is distributed on the periphery of the top of the bottom plate (10).

3. The flight training aid for the logic test according to claim 2, wherein a controller (13) is arranged at the top of the bottom plate (10) and at the bottom of the mounting plate (12), the controller (13) is electrically connected with the fixed seat (111) and the lifting rod (11), and a sliding seat (112) is movably mounted at the top of the lifting rod (11).

4. The flight training aid for the logic test as claimed in claim 3, wherein the sliding seat (112) is rotatably connected with the lifting rod (11), a limiting plate extending to the inside of the mounting plate (12) is fixedly installed at the top of the sliding seat (112), and the sliding seat (112) is slidably connected with the mounting plate (12) through the limiting plate.

5. The flight training device for the logic test according to claim 4, wherein the bottom of the mounting plate (12) is provided with a sliding groove corresponding to the limiting plate, the cross section of the sliding groove is in a shape of a Chinese character 'tu', a vertical rod (26) is fixedly mounted at the top of the mounting plate (12) and positioned at the left side of the training cabin (20), and a high-definition display (27) is fixedly mounted at the top of the vertical rod (26).

6. The flight training machine for the logic test according to claim 5, wherein the training cabin (20) is circular in side view, a seat (201) is fixedly installed inside the training cabin (20), a fastening plate (204) is movably installed at the top of the seat (201), a cabin manipulator (202) is fixedly installed inside the training cabin (20) and located on the left side of the seat (201), a vacuum air pump (203) is fixedly installed on the back of the seat (201), and a light-transmitting window (205) is fixedly installed on the left side wall of the training cabin (20).

7. The flight training aid for the logic test as claimed in claim 6, wherein the logic tester (30) is installed between the seat (201) and a fastening plate (204), the logic tester (30) is electrically connected with the cabin controller (202) through a lead, two sides of the fastening plate (204) are both fixedly provided with slide bars, and two sides of the seat (201) are both fixedly provided with snap rings in sliding connection with the slide bars.

8. The flight trainer for logic testing as claimed in claim 7, wherein the number of the vertical plates (21) is two, a positioning groove corresponding to the steering ring (22) is formed inside the vertical plate (21), the positioning groove is circular in side view, a limiting ring groove (211) is formed in an inner wall of the positioning groove, the width of the limiting ring groove (211) is half of the width of the positioning groove, and the limiting ring groove (211) is located at the center of the positioning groove.

9. The flight training aid for the logic test according to claim 8, wherein the steering ring (22) is rotatably connected with the vertical plate (21), the steering ring (22) is annular, a limiting ring (221) extending into the limiting ring groove (211) is fixedly mounted on the outer surface of the steering ring (22), and coaxial gear rings (222) are mounted on the opposite sides of the two steering rings (22).

10. The flight training aid for the logic test according to claim 9, wherein the steering motor (23) is a double-shaft motor, a driving shaft rod (24) penetrating through the vertical plate (21) is fixedly installed at the tail end of an output shaft of the steering motor (23), and a driving gear (25) meshed with the coaxial gear ring (222) is fixedly installed at one end, far away from the steering motor (23), of the driving shaft rod (24).

Technical Field

The invention relates to the technical field of flight training simulators, in particular to a flight training device for logic test.

Background

The flight training simulator is a device for training pilots, generally comprises a cockpit, interface equipment and various instruments, a vision system and a training computer, wherein the computer is a control center of the flight training simulator, and students can perform various operations when sitting in the cockpit during training: the electric switch is opened, the accelerator is pushed and pulled, the flight lever and the rudder are operated, various data can be obtained, such as flight speed, travel, position, height, wind direction, wind speed and the like, the vision system can provide scene simulation of a student, the student feels dive, upward movement and spiral movement just like sitting in an airplane during operation, various scenes (cloud, fog, river and building) above and below the airplane can be seen, various flight environments can be set, and various operations with high difficulty and danger can be learned and mastered by comprehensively exercising technology.

In the prior art, after a flight training simulator is produced, logic test needs to be carried out on the flight training simulator, but most of the current flight training simulators can only adopt pilots to carry out experience test in the simulator, the obtained test data is not accurate enough due to different subjective consciousness of each person, and the current flight training simulator cannot carry out high-difficulty actions such as real airplanes similar to rotating bodies, so that the training effect is greatly reduced for some armed pilots, and therefore the flight training simulator for the logic test is provided.

Disclosure of Invention

The invention provides a flight trainer for logic test, aiming at the technical problems in the prior art, and solves the problems in the prior art.

The technical scheme for solving the technical problems is as follows: the flight trainer for the logic test comprises an installation mechanism and a trainer, wherein the trainer is arranged above the installation mechanism, a logic test machine is arranged inside the trainer, the installation mechanism comprises a bottom plate, a lifting rod is arranged at the top of the bottom plate, a mounting plate is arranged at the top of the lifting rod, the trainer comprises a training cabin, a vertical plate movably connected with the training cabin is arranged on the surface of the mounting plate, a steering ring is fixedly arranged on the surface of the training cabin and in the vertical plate, and a steering motor is fixedly arranged at the top of the mounting plate and in the bottom of the training cabin.

On the basis of the technical scheme, the invention can be further improved as follows:

further, all fixed mounting all around of the bottom of bottom plate has the base, and the top fixed mounting of bottom plate has the fixing base of being connected with the lifter rotation, and the quantity of fixing base is four and distributes around the bottom plate top.

Further, the top of bottom plate and the bottom that is located the mounting panel are provided with the controller, and the controller is connected with fixing base and lifter electricity, and the top movable mounting of lifter has the sliding seat.

Further, the sliding seat rotates with the lifter to be connected, and the top fixed mounting of sliding seat has the limiting plate that extends to the mounting panel inside, and the sliding seat passes through limiting plate and mounting panel sliding connection.

Further, the sliding tray that corresponds with the limiting plate is seted up to the bottom of mounting panel, and the cross sectional shape of sliding tray is 'protruding' font, and the top of mounting panel and the left side fixed mounting that is located the training cabin have the pole setting, and the top fixed mounting of pole setting has high definition display.

Further, the shape of looking sideways at of training cabin is circular, and the inside fixed mounting of training cabin has the seat, and the top movable mounting of seat has the mounting plate, and the inside of training cabin and the left side fixed mounting that is located the seat have the cabin controller, and the back fixed mounting of seat has the vacuum air pump, and the left side wall fixed mounting of training cabin has the printing opacity window.

Furthermore, the logic testing machine is installed between the seat and the fastening plate, the logic testing machine is electrically connected with the cabin controller through a lead, sliding rods are fixedly installed on two sides of the fastening plate, and clamping rings connected with the sliding rods in a sliding mode are fixedly installed on two sides of the seat.

Furthermore, the quantity of riser is two, and the inside of riser is seted up and is lain in the groove of settling that the steering ring corresponds, and the shape of looking sideways at of settling the groove is circular, and the inner wall of settling the groove has seted up spacing annular, and the width of spacing annular is for settling half of the width of the groove and spacing annular is located the center of settling the groove.

Further, the steering ring is connected with the vertical plate in a rotating mode, the steering ring is circular, a limiting ring extending into the limiting ring groove is fixedly mounted on the outer surface of the steering ring, and coaxial gear rings are mounted on the opposite sides of the steering ring.

Furthermore, the steering motor is a double-shaft motor, a driving shaft rod penetrating through the vertical plate is fixedly installed at the tail end of an output shaft of the steering motor, and a driving gear meshed with the coaxial gear ring is fixedly installed at one end, far away from the steering motor, of the driving shaft rod.

Compared with the prior art, the technical scheme of the application has the following beneficial technical effects:

1. this flight training ware is used in logic test has set up the seat that is used for the test specially in training cabin inside, in the test, only need place the logic test machine go up, then utilize the mounting plate gliding with the snap ring with it fixed can, be connected with the cabin controller electricity through the logic test machine, let the logic test machine replace artifical test, receive the detection in training cabin, because the logic test machine does not have subjective meaning, consequently, each aspect data that detect out are all more accurate than artifical test.

2. The flight trainer for the logic test is characterized in that the controller controls the extension or contraction of four lifting rods, so as to help the training cabin to realize the motions of diving, pitching and circling, in addition, the driving shaft rod is driven by the steering motor, so that the driving gear drives the coaxial gear ring to rotate, and further the training cabin arranged on the inner wall of the steering ring realizes the axial rotation, so as to finish the motions of a plane with higher difficulty, improve the training effect of armed pilots, and because the logic tester is adopted for testing, the accurate test can be realized, when the plane rotates axially, the real conditions of all parts of the plane can be finally changed by the vacuum air pump, so that the air pressure in the training cabin can be more truly simulated,

drawings

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

FIG. 2 is an enlarged view A of FIG. 1 in accordance with the present invention;

FIG. 3 is a side view of the riser of the present invention;

FIG. 4 is a side cross-sectional view of the steering ring of the present invention.

In the drawings, the components represented by the respective reference numerals are listed below:

10. the device comprises a bottom plate, 11, a lifting rod, 111, a fixed seat, 112, a sliding seat, 12, a mounting plate, 13, a controller, 20, a training cabin, 201, a seat, 202, an engine cabin manipulator, 203, a vacuum air pump, 204, a fastening plate, 205, a light-transmitting window, 21, a vertical plate, 211, a limiting ring groove, 22, a steering ring, 221, a limiting ring, 222, a coaxial gear ring, 23, a steering motor, 24, a driving shaft rod, 25, a driving gear, 26, a vertical rod, 27, a high-definition displayer, 30 and a logic tester.

Detailed Description

The principles and features of this invention are described below in conjunction with the following drawings, which are set forth by way of illustration only and are not intended to limit the scope of the invention.

Referring to fig. 1-4, the flight trainer for logic testing in the present embodiment includes a mounting mechanism and a trainer, the trainer is disposed above the mounting mechanism, a logic testing machine 30 is disposed inside the trainer, a remote signal receiving device is disposed inside the logic testing machine 30, a worker can remotely control the logic testing machine 30, the logic testing machine 30 is used to replace manual testing, with this accuracy that promotes the detection data, installation mechanism includes bottom plate 10, and the top of bottom plate 10 is provided with lifter 11, and the top of lifter 11 is provided with mounting panel 12, and the training ware includes training cabin 20, and the surface of mounting panel 12 is provided with the riser 21 with training cabin 20 swing joint, and the inside fixed mounting that just is located riser 21 on the surface of training cabin 20 has a steering ring 22, and the bottom fixed mounting that just is located training cabin 20 at the top of mounting panel 12 has a steering motor 23.

In this embodiment, all fixed mounting all around of the bottom of bottom plate 10 has the base, and the rubber slipmat is installed to the base bottom, and the top fixed mounting of bottom plate 10 has the fixing base 111 of being connected with the lifter 11 rotation, and the quantity of fixing base 111 is four and distributes around the top of bottom plate 10.

In this embodiment, the top of bottom plate 10 and the bottom that is located mounting panel 12 are provided with controller 13, controller 13 is connected with fixing base 111 and lifter 11 electricity, through the extension shrink of controller 13 control fixing base 111 rotation or lifter 11, let training cabin 20 make the dive, flight actions such as backstroke, the top movable mounting of lifter 11 has sliding seat 112, sliding seat 112 rotates with lifter 11 to be connected, sliding seat 112's top fixed mounting has the limiting plate that extends to the inside of mounting panel 12, sliding seat 112 passes through limiting plate and mounting panel 12 sliding connection.

In this embodiment, the sliding tray that corresponds with the limiting plate is seted up to the bottom of mounting panel 12, and the cross sectional shape of sliding tray is 'protruding' font, and the top of mounting panel 12 and the left side fixed mounting that is located training cabin 20 have pole setting 26, and the top fixed mounting of pole setting 26 has high definition display 27, and high definition display 27 is the curved surface screen, and when simulating out the aircraft flight through high definition display 27, various environments outside the aircraft.

In this embodiment, the side view of the training cabin 20 is circular, a seat 201 is fixedly installed inside the training cabin 20, a latex cushion is installed on the top of the seat 201 to reduce the vibration applied to the logic tester 30 and prevent the logic tester 30 from being disconnected, a fastening plate 204 is movably installed on the top of the seat 201, slide bars are fixedly installed on both sides of the fastening plate 204, snap rings slidably connected with the slide bars are fixedly installed on both sides of the seat 201, a cabin controller 202 is fixedly installed inside the training cabin 20 and on the left side of the seat 201, it can be understood that a safety belt or other protection device can be equipped on the side of the seat 201, a vacuum air pump 203 is fixedly installed on the back of the seat 201, the air pressure inside the training cabin 20 is changed by the vacuum air pump 203 to simulate the state inside the flight under various conditions, a light-transmitting window 205 is fixedly installed on the left side wall of the training cabin 20, the logic tester 30 is installed between the seat 201 and the fastening plate 204, the logic tester 30 is electrically connected to the nacelle controller 202 through a wire, and the nacelle controller 202 is in signal connection with the controller 13.

In this embodiment, the number of the vertical plates 21 is two, a positioning groove corresponding to the steering ring 22 is formed in the vertical plate 21, the positioning groove is circular in side view shape, a limiting ring groove 211 is formed in the inner wall of the positioning groove, the width of the limiting ring groove 211 is half of the width of the positioning groove, the limiting ring groove 211 is located in the center of the positioning groove, the steering ring 22 is rotatably connected with the vertical plate 21, the steering ring 22 is circular, a limiting ring 221 extending into the limiting ring groove 211 is fixedly installed on the outer surface of the steering ring 22, coaxial gear rings 222 are installed on the opposite sides of the two steering rings 22, the diameters of the coaxial gear rings 222 and the steering ring 22 are equal, the steering motor 23 is a dual-shaft motor, a driving shaft rod 24 penetrating through the vertical plate 21 is fixedly installed at the tail end of an output shaft of the steering motor 23, a driving gear 25 engaged with the coaxial gear rings 222 is fixedly installed at one end of the driving shaft rod 24 far away from the steering motor 23, the steering motor 23 is used for driving the driving shaft lever 24 to rotate, then the driving gear 25 drives the coaxial gear ring 222 to rotate, the coaxial gear ring 222 rotates to enable the steering ring 22 to synchronously rotate, and the high-difficulty action of axial rotation of the training cabin 20 is realized through axial rotation of the steering ring 22.

Compared with the prior art, this flight training ware is used in logic test has set up the seat 201 that is used for the test specially in training cabin 20, during the test, only need to place logic test machine 30 on, then utilize mounting plate 204 gliding to fix it with the snap ring can, be connected with cabin controller 202 electricity through logic test machine 30, let logic test machine 30 replace manual test, receive the detection in training cabin 20, because logic test machine 30 does not have subjective meaning, therefore each aspect data that detect are all more accurate than manual test.

And, this flight training ware is used in logic test, by the extension or the shrink of four lifter 11 of controller 13 control, thereby help training cabin 20 to realize dive, move up and spiral action, in addition, drive axostylus axostyle 24 through turning to motor 23 drive, then make drive gear 25 drive coaxial gear ring 222 and rotate, and then let the training cabin 20 of installing at the inner wall of steering ring 22 realize axial rotation, thereby accomplish the aircraft action of higher difficulty, can promote the training effect of armed pilot, and owing to adopt logic test machine 30 to test, therefore can accurate test, the aircraft is when doing axial rotation, the true condition of each part of aircraft, finally, can change the inside atmospheric pressure of training cabin 20 through vacuum air pump 203, thereby simulate out the state that aircraft cabin pressure is out of balance more truthfully.

The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents, improvements and the like that fall within the spirit and principle of the present invention are intended to be included therein.