CN212448132U

CN212448132U - Monitoring device mounting structure for general aircraft

Info

Publication number: CN212448132U
Application number: CN202020591740.8U
Authority: CN
Inventors: 朱颂华; 梁飞; 刘韬; 慕文龙
Original assignee: Shanghai Guanyi General Aircraft Co ltd; Jiangxi Guanyi Aviation Co ltd
Current assignee: Shanghai Guanyi General Aircraft Co ltd; Jiangxi Guanyi Aviation Co ltd
Priority date: 2020-04-20
Filing date: 2020-04-20
Publication date: 2021-02-02
Anticipated expiration: 2030-04-20

Abstract

The utility model discloses a general aircraft is with monitoring device mounting structure, which comprises a fixing block, the fixed block bottom is equipped with the connecting block, the connecting block bottom is equipped with the camera, both sides are equipped with fixed establishment respectively in the connecting block, a plurality of screw has been seted up all around to the fixed block, the draw-in groove has been seted up respectively to fixed block bottom both sides, two first fixed slot has been seted up respectively on the top inner wall in the draw-in groove, top surface is equipped with the rubber pad respectively with the bottom surface in the first fixed slot, fixed establishment symmetry is equipped with two arc pieces respectively in the recess of both sides in the connecting block. A monitoring device mounting structure for general aircraft, but through setting traditional surveillance camera device into two structures of split to can be with the camera through fixed establishment under the condition not with the help of external instrument, can be quick carry out a dismantlement or installation to it, very big improvement supervisory equipment's maintenance convenience.

Description

Monitoring device mounting structure for general aircraft

Technical Field

The utility model relates to a supervisory equipment technical field, in particular to monitoring device mounting structure for general aircraft.

Background

The hemisphere camera, the name is exactly the shape is a hemisphere, only name to the appearance, hemisphere type camera is because small in size, and is aesthetic in appearance, relatively be fit for office space and the place that the fitment grade is high to use, also can be provided with a plurality of hemisphere camera in the cabin of some general aircraft, in order to realize a monitoring effect to the cabin condition, but because the aircraft can produce certain shake when the aircraft receives the air current effect or descends in the high altitude flight, lead to the connecting wire of camera can often appear not hard up or the condition that drops, influence the normal use of its equipment, but traditional camera is fixed through many screw snap-on in the cabin, it is comparatively troublesome when dismantling, and need prepare the instrument constantly and dismantle or install it, when not having the instrument, it is more inconvenient to dismantle it.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a monitoring device mounting structure for general aircraft can effectively solve the problem in the background art.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

the utility model provides a monitoring device mounting structure for general aircraft, includes the fixed block, the fixed block bottom is equipped with the connecting block, the connecting block bottom is equipped with the camera, both sides are equipped with fixed establishment respectively in the connecting block.

Preferably, a plurality of screw has been seted up all around to the fixed block, the draw-in groove has been seted up respectively to fixed block bottom both sides, two first fixed slot has been seted up respectively on the top inner wall in the draw-in groove, top surface and bottom surface are equipped with the rubber pad respectively in the first fixed slot, and through the rubber pad setting in the first fixed slot, can the more firm installation of fixture block in the draw-in groove.

Preferably, the fixing mechanism is symmetrically provided with two arc blocks in the grooves on the two sides in the connecting block respectively, the outer wall above the arc blocks is provided with a clamping block respectively, a jacking mechanism is arranged between the two arc blocks, and the switching function of the two arc blocks in the clamping groove can be realized through the arrangement of the jacking mechanism.

Preferably, the top bracing mechanism comprises two connecting rods, one side of each of the two connecting rods is respectively provided with a first stop block, the connecting rods are inserted and installed in fixing holes on one corresponding side in the connecting blocks through the first stop blocks, the two connecting rods are respectively provided with a compression spring, the compression springs are positioned on the connecting rods between the arc-shaped blocks and the inner walls of the grooves of the connecting blocks, tooth grooves are respectively formed in one sides of the two connecting rods in opposite directions, second fixing grooves are respectively formed in the front ends and the rear ends of one sides of the two connecting rods, a gear is arranged between the two tooth grooves, the front end and the rear end of the gear are respectively provided with a connecting mechanism, a first connecting shaft is arranged in the middle position of the front end of the gear, the first connecting shaft penetrates through the connecting mechanism to be fixedly connected with the gear, a second connecting shaft is arranged in the middle position of the rear end of, the front end of the first connecting shaft is provided with a loop bar.

Preferably, coupling mechanism is equipped with the third fixed slot respectively, two at gear front end and rear end be equipped with the retainer plate in the third fixed slot respectively, retainer plate one side is equipped with the rand, the retainer plate alternates through the rand and installs in the third fixed slot, the retainer plate opposite side is equipped with the fixed plate, fixed plate one side top is equipped with spacing axle respectively with the below, and two spacing axles alternate respectively and install in the second fixed slot that corresponds, through coupling mechanism's setting, can make the gear fix spacing between two tooth's sockets, prevent to break away from.

Preferably, the loop bar is provided with a limiting mechanism, the limiting mechanism is provided with a ratchet wheel on the outer wall of the corresponding loop bar, the ratchet gear is positioned in the mounting cavity at one side of the connecting block, the limiting mechanism is also provided with a second stop block at the top surface in the mounting cavity at one side of the connecting block, the second stop block is inserted and installed in a groove of the inner cavity of the connecting block through a fixed shaft at the top, a first telescopic groove is also formed in one side of the inner side of the loop bar of the limiting mechanism, the first connecting shaft is inserted and installed in the first telescopic groove, and one side of the first connecting shaft is provided with a second telescopic groove, a tension spring is arranged in the second telescopic groove, one side of the tension spring is fixedly arranged in the second telescopic groove, the other side of the tension spring is fixedly arranged on one side in the first telescopic groove, through stop gear's setting, can realize when removing two arc pieces from the draw-in groove for the ratchet wheel that the loop bar drove breaks away from the second dog.

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

a monitoring device mounting structure for general aircraft, but through setting traditional surveillance camera device into two structures of split to can be with the camera through fixed establishment under the condition not with the help of external instrument, can be quick carry out a dismantlement or installation to it, very big improvement supervisory equipment's maintenance convenience.

Drawings

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

fig. 2 is a sectional view of the fixing block and the connecting block of the present invention;

FIG. 3 is an enlarged view taken at A in FIG. 2;

FIG. 4 is a schematic structural view of the top bracing mechanism of the present invention;

FIG. 5 is a structural exploded view of the connecting mechanism of the present invention;

fig. 6 is a cross-sectional view of the first connecting shaft and the loop bar of the present invention.

In the figure: 1. a fixed block; 2. connecting blocks; 3. a camera; 4. a fixing mechanism; 5. a screw hole; 6. a card slot; 7. a first fixing groove; 8. a rubber pad; 9. an arc-shaped block; 10. a clamping block; 11. a shoring mechanism; 12. A connecting rod; 13. a first stopper; 14. a compression spring; 15. a tooth socket; 16. a second fixing groove; 17. A gear; 18. a connecting mechanism; 19. a first connecting shaft; 20. a second connecting shaft; 21. a loop bar; 22. a third fixing groove; 23. a stationary ring; 24. a collar; 25. a fixing plate; 26. a limiting shaft; 27. a limiting mechanism; 28. a ratchet gear; 29. a second stopper; 30. a first telescopic slot; 31. a second telescopic slot; 32. A tension spring.

Detailed Description

In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.

In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element to which the reference is made must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, and for example, "connected" may be either fixedly connected or detachably connected, or integrally connected; 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 in specific cases to those skilled in the art.

As shown in fig. 1-5, the utility model provides a pair of general monitoring device mounting structure for aircraft, including

fixed block

1, 1 bottom of fixed block is equipped with connecting

block

2, and 2 bottoms of connecting block are equipped with camera 3, and both sides are equipped with fixed establishment 4 respectively in the connecting block 2.

The periphery of a fixed block 1 is provided with a plurality of screw holes 5, two sides of the bottom of the fixed block 1 are respectively provided with a clamping groove 6, the inner walls of the tops of the two clamping grooves 6 are respectively provided with a first fixed groove 7, the inner top surface and the bottom surface of the first fixed groove 7 are respectively provided with a rubber pad 8, a fixed mechanism 4 is respectively and symmetrically provided with two arc-shaped blocks 9 in grooves of the two sides of a connecting block 2, the outer walls above the two arc-shaped blocks 9 are respectively provided with a clamping block 10, a jacking mechanism 11 is arranged between the two arc-shaped blocks 9, the jacking mechanism 11 comprises two connecting rods 12, one side of each connecting rod 12 is respectively provided with a first stop 13, the connecting rods 12 are inserted and installed in fixed holes of the corresponding side of the connecting block 2 through the first stop 13, the two connecting rods 12 are respectively provided with a compression spring 14, the compression spring 14 is positioned, the two connecting rods 12 are respectively provided with a second fixing groove 16 at the front end and the rear end of one side, a gear 17 is arranged between two tooth grooves 15, the front end and the rear end of the gear 17 are respectively provided with a connecting mechanism 18, the middle position of the front end of the gear 17 is provided with a first connecting shaft 19, the first connecting shaft 19 penetrates through the connecting mechanism 18 and is fixedly connected with the gear 17, the middle position of the rear end of the gear 17 is provided with a second connecting shaft 20, the other side of the second connecting shaft 20 is inserted and installed in a fixing hole in a groove of the connecting block 2, the front end of the first connecting shaft 19 is provided with a loop bar 21, the connecting mechanism 18 is respectively provided with a third fixing groove 22 at the front end and the rear end of the gear 17, two third fixing grooves 22 are respectively provided with a fixing ring 23, one side of the fixing ring 23 is provided with a retainer ring 24, the fixing ring 23 is inserted and installed in the third fixing groove 22 through, two spacing axles 26 alternate respectively and install in corresponding second fixed slot 16, be equipped with stop gear 27 on loop bar 21, stop gear 27 is equipped with ratchet wheel 28 on the loop bar 21 outer wall that corresponds, ratchet wheel 28 is located the installation cavity of connecting block 2 one side, stop gear 27 still is equipped with second dog 29 at the internal top surface of installation cavity of connecting block 2 one side, second dog 29 alternates through the fixed axle at top and installs in the recess of cavity in connecting block 2, stop gear 27 still has seted up first flexible groove 30 in loop bar 21 one side, first connecting axle 19 alternates and installs in first flexible groove 30, and second flexible groove 31 has been seted up to first connecting axle 19 one side, be equipped with tension spring 32 in the flexible groove 31 of second, tension spring 32 one side fixed mounting is in the flexible groove 31 of second, opposite side fixed mounting is in first flexible inslot 30 one side.

It should be noted that, when the monitoring device mounting structure for a general-purpose aircraft is used, when the camera 3 needs to be detached, the loop bar 21 is firstly pulled outwards, the loop bar 21 slides on the first connecting shaft 19 through the tension spring 32, and the ratchet wheel 28 moves to one side through the loop bar 21, so that the ratchet wheel 28 is separated from the second stop 29, and then, after the first stops 13 on the two connecting rods 12 are not blocked, the corresponding arc blocks 9 are respectively pushed towards the middle, so that the two arc blocks 9 drive the corresponding fixture blocks 10 to move to one side, and then the two fixture blocks 10 are separated from the first fixing groove 7, and then the loop bar 21 on the other side is operated by analogy, so that the connecting block 2 can be separated from the fixing block 1, and then the camera 3 is detached, when the camera 3 needs to be mounted on the fixing block 1, not dragging loop bar 21, directly rotate loop bar 21, and then drive ratchet wheel 28 and rotate, and then make ratchet wheel 28 unidirectional rotation on second dog 29, and then drive first connecting axle 19 through loop bar 21 and rotate, and then drive gear 17 through first connecting axle 19 and rotate, and then drive two tooth's socket 15 through gear 17 and move its connecting rod 12 that corresponds to one side, and then move corresponding arc piece 9 to one side through the baffle on connecting rod 12, and then crowd into first fixed slot 7 with fixture block 10 on arc piece 9, and then with connecting block 2 fixed mounting on fixed block 1, and then with camera 3 fixed mounting.

The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims

1. The utility model provides a monitoring device mounting structure for general aircraft which characterized in that: including fixed block (1), fixed block (1) bottom is equipped with connecting block (2), connecting block (2) bottom is equipped with camera (3), both sides are equipped with fixed establishment (4) respectively in connecting block (2).

2. A monitor mounting structure for a general-purpose aircraft according to claim 1, wherein: a plurality of screw holes (5) are formed in the periphery of the fixed block (1), clamping grooves (6) are formed in two sides of the bottom of the fixed block (1) respectively, first fixing grooves (7) are formed in the inner wall of the inner top of each clamping groove (6) respectively, and rubber pads (8) are arranged on the inner top face and the bottom face of each first fixing groove (7).

3. A monitor mounting structure for a general-purpose aircraft according to claim 1, wherein: the fixing mechanism (4) is symmetrically provided with two arc blocks (9) in grooves on two sides in the connecting block (2), the outer wall above the arc blocks (9) is provided with a clamping block (10), and a top support mechanism (11) is arranged between the two arc blocks (9).

4. A monitor mounting structure for a general-purpose aircraft according to claim 3, wherein: the top support mechanism (11) comprises two connecting rods (12), one side of each of the two connecting rods (12) is provided with a first stop block (13), the connecting rods (12) are installed in fixing holes in the connecting block (2) corresponding to one side in an inserting mode through the first stop blocks (13), compression springs (14) are arranged on the two connecting rods (12) respectively, the compression springs (14) are located on the connecting rods (12) between the arc-shaped blocks (9) and the inner wall of the groove of the connecting block (2), tooth grooves (15) are formed in one sides of the two connecting rods (12) in a relative direction respectively, second fixing grooves (16) are formed in the front ends and the rear ends of the two connecting rods (12) respectively, a gear (17) is arranged between the two tooth grooves (15), the front end and the rear end of the gear (17) are provided with connecting mechanisms (18) respectively, a first connecting shaft (19) is arranged in the middle position of the, first connecting axle (19) pass coupling mechanism (18) and gear (17) fixed connection, gear (17) rear end intermediate position is equipped with second connecting axle (20), second connecting axle (20) opposite side alternates to be installed in the fixed orifices in connecting block (2) recess, first connecting axle (19) front end is equipped with loop bar (21).

5. A monitor mounting structure for a general-purpose aircraft according to claim 4, wherein: coupling mechanism (18) are equipped with third fixed slot (22), two respectively at gear (17) front end and rear end be equipped with retainer plate (23) in third fixed slot (22) respectively, retainer plate (23) one side is equipped with rand (24), retainer plate (23) are installed in third fixed slot (22) through rand (24) interlude, retainer plate (23) opposite side is equipped with fixed plate (25), fixed plate (25) one side top is equipped with spacing axle (26) respectively with the below, and two spacing axles (26) are installed in corresponding second fixed slot (16) of interlude respectively.

6. A monitor mounting structure for a general-purpose aircraft according to claim 4, wherein: the sleeve rod (21) is provided with a limiting mechanism (27), the limiting mechanism (27) is provided with a ratchet gear (28) on the outer wall of the corresponding sleeve rod (21), the ratchet gear (28) is positioned in an installation cavity on one side of the connecting block (2), the limiting mechanism (27) is also provided with a second stop block (29) on the inner top surface of the installation cavity on one side of the connecting block (2), the second stop block (29) is inserted and installed in a groove of the inner cavity of the connecting block (2) through a fixed shaft on the top, the limiting mechanism (27) is also provided with a first telescopic groove (30) on one side in the sleeve rod (21), the first connecting shaft (19) is inserted and installed in the first telescopic groove (30), a second telescopic groove (31) is formed on one side of the first connecting shaft (19), a tension spring (32) is arranged in the second telescopic groove (31), one side of the tension spring (32) is fixedly installed in the second telescopic groove (31), the other side is fixedly arranged at one side in the first telescopic groove (30).