CN216861839U

CN216861839U - Airborne pod simulation device with auxiliary monitoring effect

Info

Publication number: CN216861839U
Application number: CN202122866646.6U
Authority: CN
Inventors: 朱学伟; 陈海峰
Original assignee: Wuhan Joho Technology Co ltd
Current assignee: Wuhan Joho Technology Co ltd
Priority date: 2021-11-22
Filing date: 2021-11-22
Publication date: 2022-07-01
Anticipated expiration: 2031-11-22

Abstract

The utility model discloses an airborne pod simulation device with an auxiliary monitoring effect, which belongs to the technical field of airborne pods and comprises an airborne pod body, wherein two connecting ends are arranged on the outer surface of the airborne pod body, two installers are arranged on the outer surface of the airborne pod body, and the connecting ends are sleeved in the installers. This airborne nacelle analogue means with supplementary effect of monitoring, through setting up first transfer line, when the erector is installed with the link, rotate the knob earlier, the knob drives first transfer line and gear rotation, two first drivers drive two second drivers and expand to both sides, this mode can be fast with airborne nacelle body install or dismantle fast, the effectual link of having avoided takes place loose condition after long-time simultaneously, and the effectual in use airborne nacelle body of having avoided takes place the possibility that drops, thereby the improvement security of airborne nacelle body.

Description

Airborne pod simulation device with auxiliary monitoring effect

Technical Field

The utility model belongs to the technical field of airborne pods, and particularly relates to an airborne pod simulation device with an auxiliary monitoring effect.

Background

The pod is a streamline short cabin section which is provided with certain airborne equipment or weapons and is hung under a fuselage or wings. Can be fixedly mounted (such as an engine pod) and can be detached (such as a weapon pod). The addition of the pod allows the aircraft to have functions not available in itself, which usually requires support from onboard electronics and takes into account the overall aerodynamics of the aircraft. The traditional connection mode of the existing airborne pod is inconvenient to install and detach and is easy to loosen after long time, so that the possibility that the airborne pod body falls off during operation can be caused.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

In order to overcome the defects of the prior art, the utility model provides an airborne pod simulation device with an auxiliary monitoring effect, which solves the problems that the traditional connection mode of the existing airborne pod is inconvenient to install and detach and is easy to loosen after a long time, so that the possibility that the airborne pod body falls off in the operation process is possibly caused, and the traditional installation mode is complex in operation and inconvenient for technicians to detach the airborne pod body in the process of maintenance.

(II) technical scheme

In order to achieve the purpose, the utility model provides the following technical scheme: the utility model provides an airborne nacelle analogue means with supplementary monitoring effect, includes airborne nacelle body, the surface of airborne nacelle body is provided with two links, the surface of airborne nacelle body is provided with two erectors, the link cup joints in the erector, fixedly connected with baffle in the erector, be provided with first rotation pole in the erector, the surface of first rotation pole is provided with the coil spring, be provided with the gear in the erector, the left end of first rotation pole and the right flank fixed connection of gear.

Be provided with two second dwangs in the erector, the top and the bottom of second dwang and the inner wall fixed connection of erector, first driver has all been cup jointed to the surface of two second dwangs, and the opposite face of two first drivers meshes with the surface of same gear mutually, be provided with two second drivers in the erector, the right flank of second driver meshes with the left surface of first driver mutually, the mounting groove has been seted up to the surface of link.

As a further scheme of the utility model: two telescopic rods are arranged in the mounting device, and one end of the back of each telescopic rod is fixedly connected with the front of the second driver.

As a further scheme of the utility model: two pushing rods are arranged in the mounting device, two sliding grooves are formed in the right side face of the partition plate, and the pushing rods are clamped in the sliding grooves.

As a further scheme of the utility model: the loader-mounted nacelle is characterized in that a bearing is arranged in the installer, two rotating buttons are arranged on the outer surface of the loader-mounted nacelle, and the right end of the first rotating rod penetrates through the installer and is fixedly connected with the left side face of each rotating button.

As a further scheme of the utility model: the erector is internally provided with two limiting blocks, the left end of the push rod is fixedly connected with the outer surfaces of the limiting blocks, and the limiting blocks are clamped in the mounting grooves.

As a further scheme of the utility model: the outer surface of the airborne pod body is provided with a support, and one end of the front surface of the support is fixedly connected with the outer surface of the installer.

As a further scheme of the utility model: the upper surface of the support is fixedly connected with a fixed rod, the outer surface of the airborne pod body is provided with a rotating ring, and the top end of the fixed rod is fixedly connected with the lower surface of the rotating ring.

(III) advantageous effects

Compared with the prior art, the utility model has the beneficial effects that:

1. the airborne pod simulation device with the auxiliary monitoring effect comprises a first rotating rod, a gear, a first driver and a second driver, wherein when an installer and a connecting end are installed, a rotating knob is rotated firstly and drives the first rotating rod and the gear to rotate, so that the two first drivers drive the two second drivers to expand towards two sides, the second drivers drive a push rod and a limiting block to move simultaneously during moving, then the installer is clamped with the connecting end, the rotating knob is loosened, the first rotating rod is driven to rotate under the action of the elastic force of a coil spring, so that the limiting block is clamped with a mounting groove, compared with the original mode, the airborne pod simulation device is simple in installation operation mode, the airborne pod body can be quickly installed or detached, meanwhile, the situation that the connecting end is loosened after a long time is effectively avoided, and the possibility that the airborne pod body falls off during use is effectively avoided, thereby improving the safety of the airborne pod body.

2. This airborne nacelle analogue means with supplementary effect of monitoring, through setting up first transmission ware and second transmission ware, the gear drives two first transmission wares and reciprocates through first dwang in the opposite direction in rotating, two first transmission wares drive two second transmission wares and expand to both sides in moving, the second transmission ware drives the catch bar simultaneously and moves in moving, its first transmission ware and second driven stability is better, the effectual circumstances of avoiding the catch bar to take place skew in moving, thereby make the catch bar more stable in use.

3. This airborne nacelle analogue means with supplementary effect of keeping watch on, through setting up the stopper, the knob, drive the catch bar under the spring action of wind spring, the catch bar drives the stopper and carries out the joint with the mounting groove, form a circular behind its two stopper joints, be less than the mounting groove, the surface is comparatively smooth, from not influencing the rotation of link, spacing effect has simultaneously, the surface of knob has dull polish texture, the user is difficult for taking place the condition of skidding in rotating the knob.

Drawings

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

FIG. 2 is a schematic view of the structure of the gear explosion of the present invention;

FIG. 3 is a schematic cross-sectional view of an installer in accordance with the present invention;

fig. 4 is a schematic cross-sectional view of a top view of the mounter according to the present invention;

in the figure: the device comprises an airborne pod body 1, a connecting end 2, a mounting device 3, a partition plate 4, a first rotating rod 5, a coil spring 6, a gear 7, a first rotating rod 8, a first driver 9, a second driver 10, a telescopic rod 11, a pushing rod 12, a sliding groove 13, a limiting block 14, a rotating knob 15, a bearing 16, a support 17, a fixing rod 18, a rotating ring 19 and a mounting groove 20.

Detailed Description

The technical solution of the present patent will be described in further detail with reference to the following embodiments.

As shown in fig. 1 to 4, the present invention provides a technical solution: the utility model provides an airborne nacelle analogue means with supplementary monitoring effect, including airborne nacelle body 1, the surface of airborne nacelle body 1 is provided with two links 2, through setting up link 2, two links 2 have increased the stability of airborne nacelle body 1, link 2 has better mobility simultaneously, thereby make the difficult condition that takes place the card pause of airborne nacelle body 1 in the rotation, the surface of airborne nacelle body 1 is provided with two erectors 3, link 2 cup joints in erector 3, fixedly connected with baffle 4 in the erector 3, be provided with first rotation pole 5 in the erector 3, the surface of first rotation pole 5 is provided with coil spring 6, be provided with gear 7 in the erector 3, the left end of first rotation pole 5 and the right flank fixed connection of gear 7.

Two second rotating rods 8 are arranged in the mounting device 3, and the second rotating rods 8 have the function of limiting through the arrangement of the second rotating rods 8, thereby enabling the first transmission gear 9 to move up and down regularly without deviation, the top end and the bottom end of the second rotating rod 8 are fixedly connected with the inner wall of the mounting device 3, the outer surfaces of the two second rotating rods 8 are sleeved with the first transmission gear 9, through the arrangement of the first transmission gear 9, the first transmission device 9 has better stability, so that the second transmission device 10 is not easy to fall off during moving, the opposite surfaces of the two first drivers 9 are meshed with the outer surface of the same gear 7, two second drivers 10 are arranged in the mounting device 3, the right side surfaces of the second drivers 10 are meshed with the left side surfaces of the first drivers 9, and the outer surface of the connecting end 2 is provided with a mounting groove 20.

Specifically, as shown in fig. 1, a support 17 is provided on the outer surface of the onboard pod body 1, one end of the front surface of the support 17 is fixedly connected with the outer surface of the mounter 3, a fixing rod 18 is fixedly connected to the upper surface of the support 17, a rotating ring 19 is provided on the outer surface of the onboard pod body 1, and the top end of the fixing rod 18 is fixedly connected with the lower surface of the rotating ring 19.

Specifically, as shown in fig. 2, two telescopic rods 11 are arranged in the mounting device 3, one end of the back of each telescopic rod 11 is fixedly connected with the front of the second driver 10, two push rods 12 are arranged in the mounting device 3, two sliding grooves 13 are formed in the right side of the partition plate 4, and the push rods 12 are clamped in the sliding grooves 13.

Specifically, as shown in fig. 4, a bearing 16 is arranged in the mounter 3, two rotating knobs 15 are arranged on the outer surface of the airborne pod, the rotating knobs 15 are arranged, the surface of the rotating knobs 15 has frosted textures, a user is not prone to slipping during rotation, and therefore people can rotate conveniently, the right end of the first rotating rod 5 penetrates through the mounter 3 and is fixedly connected with the left side face of the rotating knobs 15, two limiting blocks 14 are arranged in the mounter 3, the limiting blocks 14 are arranged through the limiting blocks 14, the connecting end 2 is not prone to slipping and jamming during rotation, rotation is smooth, the left end of the push rod 12 is fixedly connected with the outer surfaces of the limiting blocks 14, and the limiting blocks 14 are clamped in the mounting grooves 20.

The working principle of the utility model is as follows:

when the mounting device 3 and the connecting end 2 are mounted, the rotating knob 15 is rotated, the rotating knob 15 is forced to drive the first rotating rod 5 to rotate, the first rotating rod 5 drives the gear 7, so that the two first drivers 9 move up and down in opposite directions through the second rotating rod 8, the two first drivers 9 drive the two second drivers 10 to expand towards two sides in movement, the second drivers 10 push the telescopic rods 11 to contract in expansion, the second drivers 10 drive the push rods 12 simultaneously in movement, the push rods 12 drive the limit blocks 14 to move through the sliding grooves 13 and the partition plates 4, then the mounting device 3 is clamped with the connecting end 2, the rotating knob 15 is loosened after the connecting end 2 is clamped with the bearing 16, the first rotating rod 5 is driven to rotate under the elastic force of the coil spring 6, so that the limiting block 14 is clamped with the mounting groove 20, a rotating ring 19 above a fixed rod 18 connected through a bracket 17 is installed with an external device.

In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art through specific situations.

Although the preferred embodiments of the present patent have been described in detail, the present patent is not limited to the above embodiments, and various changes can be made without departing from the spirit of the present patent within the knowledge of those skilled in the art.

Claims

1. An airborne pod simulation device with auxiliary monitoring effect, comprising an airborne pod body (1), characterized in that: the outer surface of the airborne nacelle body (1) is provided with two connecting ends (2), the outer surface of the airborne nacelle body (1) is provided with two erectors (3), the connecting ends (2) are sleeved in the erectors (3), a partition plate (4) is fixedly connected in the erectors (3), a first rotating rod (5) is arranged in the erectors (3), the outer surface of the first rotating rod (5) is provided with a coil spring (6), gears (7) are arranged in the erectors (3), and the left end of the first rotating rod (5) is fixedly connected with the right side face of the gears (7);

be provided with two second dwangs (8) in erector (3), the top and the bottom of second dwang (8) and the inner wall fixed connection of erector (3), first transmission ware (9) have all been cup jointed to the surface of two second dwangs (8), and the opposite face of two first transmission ware (9) meshes with the surface of same gear (7) mutually, be provided with two second transmission ware (10) in erector (3), the right flank of second transmission ware (10) meshes with the left flank of first transmission ware (9) mutually, mounting groove (20) have been seted up to the surface of link (2).

2. The on-board pod simulation apparatus with auxiliary monitoring effect according to claim 1, wherein: two telescopic rods (11) are arranged in the mounting device (3), and one end of the back of each telescopic rod (11) is fixedly connected with the front of the second driver (10).

3. The on-board pod simulation apparatus with auxiliary monitoring effect according to claim 1, wherein: two pushing rods (12) are arranged in the installer (3), two sliding grooves (13) are formed in the right side face of the partition plate (4), and the pushing rods (12) are clamped in the sliding grooves (13).

4. The on-board pod simulation apparatus with auxiliary monitoring effect according to claim 1, wherein: the aircraft-mounted nacelle is characterized in that a bearing (16) is arranged in the installer (3), two rotating buttons (15) are arranged on the outer surface of the aircraft-mounted nacelle, and the right end of the first rotating rod (5) penetrates through the installer (3) to be fixedly connected with the left side face of each rotating button (15).

5. An on-board pod simulation apparatus with auxiliary surveillance effect according to claim 3, wherein: two limiting blocks (14) are arranged in the installer (3), the left end of the push rod (12) is fixedly connected with the outer surfaces of the limiting blocks (14), and the limiting blocks (14) are clamped in the mounting grooves (20).

6. The on-board pod simulation apparatus with auxiliary monitoring effect according to claim 1, wherein: the outer surface of the airborne nacelle body (1) is provided with a support (17), and one end of the front surface of the support (17) is fixedly connected with the outer surface of the installer (3).

7. The on-board pod simulation apparatus with auxiliary monitoring effect according to claim 6, wherein: the upper surface of the support (17) is fixedly connected with a fixing rod (18), the outer surface of the airborne pod body (1) is provided with a rotating ring (19), and the top end of the fixing rod (18) is fixedly connected with the lower surface of the rotating ring (19).