CN219192577U

CN219192577U - Unmanned aerial vehicle time domain avionics pod receiver stores pylon device

Info

Publication number: CN219192577U
Application number: CN202320807854.5U
Authority: CN
Inventors: 何强; 夏祖爱; 王启权; 闫涵; 陈龙
Original assignee: Anhui Aiifei General Aviation Co ltd
Current assignee: Anhui Aiifei General Aviation Co ltd
Priority date: 2023-04-13
Filing date: 2023-04-13
Publication date: 2023-06-16
Anticipated expiration: 2033-04-13

Abstract

The utility model discloses an unmanned aerial vehicle time domain avionics pod receiver hanging frame device, bolts are threaded through four corners of the top of a top hanging plate, a limiting cover is fixedly arranged in the middle of the bottom of the top hanging plate, a connecting ball is rotatably arranged in the limiting cover, and a T-shaped plate is fixedly arranged in the middle of the bottom of the connecting ball. This unmanned aerial vehicle time domain avionics pod receiver stores pylon device through the cooperation of limiting cover, engagement ball, loading board and arc splint subassembly, carries unmanned aerial vehicle time domain avionics pod receiver on unmanned aerial vehicle, because limiting cover rotates with engagement ball to be connected, unmanned aerial vehicle takes place askew in the flight in-process, engagement ball and unmanned aerial vehicle time domain avionics pod receiver also can be because of self gravity effect vertical downward, keeps vertical steady state constantly, can not influence the secondary electromagnetic field that the response vortex produced in the receipt comes from the underground conductor, guarantees result of use.

Description

Unmanned aerial vehicle time domain avionics pod receiver stores pylon device

Technical Field

The utility model relates to the technical field of aviation electromagnetic measurement, in particular to an unmanned aerial vehicle time domain avionics pod receiver hanging frame device.

Background

The existing unmanned aerial vehicle time domain avionics pod receiver hanging frame device is used for hanging an unmanned aerial vehicle time domain avionics pod receiver on an unmanned aerial vehicle body, and the unmanned aerial vehicle cannot keep a horizontal stable state in the flying process, so that the hanging pod receiver is also deflected accordingly, the secondary electromagnetic field generated by the induction vortex in an underground conductor is influenced, and the using effect is influenced.

Disclosure of Invention

Aiming at the defects of the prior art, the utility model provides a hanging device of an unmanned aerial vehicle time domain navigation electric pod receiver, which solves the problems that the unmanned aerial vehicle cannot keep a horizontal stable state in the flying process, so that the mounted electric pod receiver is deflected accordingly, the secondary electromagnetic field generated by the induction vortex in an underground conductor is influenced to be received, and the using effect is influenced.

In order to achieve the above purpose, the utility model is realized by the following technical scheme: the utility model provides an unmanned aerial vehicle time domain avionics pod receiver stores pylon device, includes the top link plate, the equal screw thread in top four corners of top link plate runs through there is the bolt, the fixed limiting cover that is provided with in the middle of the bottom of top link plate, the inside rotation of limiting cover is provided with the joint ball, the fixed T template that is provided with in the middle of the bottom of joint ball, movable groove has all been seted up to the bottom left and right sides of T template, two the inside in movable groove all slides and is provided with square linking slider, two square linking slider's bottom is all fixed and is provided with the loading board, two the equal fixed arc splint subassembly that is provided with in one side lower part that the loading board is close to each other, the equal screw thread in the left and right sides of T template runs through there is the lead screw, evenly fixedly in the middle of the bottom of T template is provided with a plurality of expansion springs, a plurality of fixedly between the bottom of expansion springs.

Preferably, one ends of the two screw rods, which are close to each other, are respectively and rotatably connected to the side walls of the adjacent square connecting sliding blocks.

Preferably, unmanned aerial vehicle time domain avionics pod receivers are arranged among the two bearing plates, the two arc-shaped clamping plate assemblies and the lower pressing plate.

Preferably, the two arc-shaped clamping plate assemblies comprise arc-shaped clamping plate bodies, and the arc-shaped clamping plate bodies are fixedly connected to the side walls of the corresponding bearing plates.

Preferably, the inner wall of the arc-shaped clamping plate body is fixedly provided with a protection pad, and an elastic tensioning belt is fixedly arranged between the front end and the rear end of the inner cavity of the arc-shaped clamping plate body.

Preferably, the top of the arc-shaped clamping plate body is uniformly and fixedly provided with a plurality of anti-skid lugs.

Advantageous effects

The utility model provides an unmanned aerial vehicle time domain avionics pod receiver hanging frame device. Compared with the prior art, the method has the following beneficial effects:

(1) This unmanned aerial vehicle time domain avionics pod receiver stores pylon device, mutually support through the limiting cover, the joining ball, loading board and arc splint subassembly between, carry unmanned aerial vehicle time domain avionics pod receiver on unmanned aerial vehicle, because the limiting cover rotates with the joining ball to be connected, even unmanned aerial vehicle takes place askew in the flight process, the joining ball also can be because of self gravity effect vertical downward with unmanned aerial vehicle time domain avionics pod receiver, constantly keep vertical steady state, can not influence the secondary electromagnetic field that the response vortex produced in the receipt comes from the underground conductor, guarantee the result of use.

(2) This unmanned aerial vehicle time domain avionics pod receiver stores pylon device through on the lateral wall of arc splint body fixed connection at corresponding loading board, the fixed protection pad that is provided with of inner wall of arc splint body, fixedly between the inner chamber front and back end of arc splint body, the even fixed a plurality of antiskid lugs that are provided with in top of arc splint body, through the mutual cooperation between movable groove, the lead screw, elasticity tensioning belt and the holding down plate, can carry out spacing clamp to the unmanned aerial vehicle time domain avionics pod receiver of equidimension not, and then can carry the unmanned aerial vehicle time domain avionics pod receiver of equidimension not on unmanned aerial vehicle, application scope is more extensive.

Drawings

FIG. 1 is a front view of the present utility model;

FIG. 2 is a cross-sectional view of the present utility model;

fig. 3 is a top view of the arcuate clamping plate assembly of the present utility model.

In the figure: 1. a top hanging plate; 2. a bolt; 3. a limiting cover; 4. a connecting ball; 5. t-shaped plates; 6. a movable groove; 7. square connecting sliding blocks; 8. a carrying plate; 9. an arcuate cleat assembly; 91. an arc-shaped splint body; 92. a protective pad; 93. elastically tensioning the belt; 94. an anti-slip bump; 10. a screw rod; 11. a telescopic spring; 12. a lower pressing plate; 13. unmanned aerial vehicle time domain avionics pod receiver.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

The utility model provides two technical schemes:

a first embodiment is shown in fig. 1-2: the utility model provides an unmanned aerial vehicle time domain avionics pod receiver stores pylon device, including top link plate 1, the equal screw thread in top four corners of top link plate 1 runs through there is bolt 2, the fixed limiting cover 3 that is provided with in the middle of the bottom of top link plate 1, the inside rotation of limiting cover 3 is provided with the linking ball 4, the fixed T template 5 that is provided with in the middle of the bottom of linking ball 4, movable groove 6 has all been seted up to the bottom left and right sides of T template 5, the inside of two movable grooves 6 all slides and is provided with square linking slider 7, the bottom of two square linking sliders 7 is all fixed and is provided with loading board 8, the equal screw thread in the left and right sides of one side lower part that two loading board 8 are close to each other is fixed and is provided with arc splint subassembly 9, evenly fixed being provided with a plurality of expansion springs 11 in the middle of the bottom of T template 5, fixedly be provided with holding down plate 12 between the bottom of a plurality of expansion springs 11.

Through mutually supporting between limiting cover 3, linking ball 4, loading board 8 and the arc splint subassembly 9, carry unmanned aerial vehicle time domain avionics pod receiver 13 on unmanned aerial vehicle, because limiting cover 3 rotates with linking ball 4 to be connected, even unmanned aerial vehicle takes place askew at flight in-process, linking ball 4 and unmanned aerial vehicle time domain avionics pod receiver 13 also can be because of self gravity effect vertical downward, keep vertical steady state constantly, can not influence the secondary electromagnetic field that the response vortex produced in the receipt comes from the underground conductor, guarantee the result of use.

The second embodiment, shown in fig. 1 and 3, differs from the first embodiment mainly in that: the utility model provides an unmanned aerial vehicle time domain avionics pod receiver stores pylon device, the one end that two lead screws 10 are close to each other rotates respectively to be connected on adjacent square linking slider 7's lateral wall, be provided with unmanned aerial vehicle time domain avionics pod receiver 13 between two loading board 8, two arc splint subassembly 9 and holding down plate 12, two arc splint subassembly 9 all include arc splint body 91, arc splint body 91 fixed connection is on corresponding loading board 8's lateral wall, the fixed protection pad 92 that is provided with of inner wall of arc splint body 91, fixed being provided with elasticity tensioning belt 93 between the inner chamber front and back end of arc splint body 91, the even fixed a plurality of anti-skidding lugs 94 that are provided with in top of arc splint body 91.

Through mutually supporting between movable groove 6, lead screw 10, elasticity tensioning belt 93 and holding down plate 12, can carry out spacing clamp to unmanned aerial vehicle time domain avionics pod receiver 13 of equidimension not, and then can carry unmanned aerial vehicle time domain avionics pod receiver 13 of equidimension not on unmanned aerial vehicle, application scope is more extensive.

And all that is not described in detail in this specification is well known to those skilled in the art.

During the use, utilize bolt 2 to connect top link plate 1 on unmanned aerial vehicle, then two lead screw 10 are controlled to carry out the knob to it about holding, two square linking slider 7 follow along movable slot 6 slides, adjust two square linking slider 7 to the one side of keeping away from each other, make about two arc splint subassembly 9 keep away from each other, then place the unmanned aerial vehicle time domain avionics pod receiver 13 that waits to mount between controlling two arc splint bodies 91, make the top of unmanned aerial vehicle time domain avionics pod receiver 13 be located between the upper portion of two arc splint bodies 91, then reverse screw lead screw 10, adjust two square linking slider 7 to the one side that is close to each other, two loading board 8 are then close to each other, two arc splint bodies 91 are also close to each other, two elastic tension belts 93 paste on the outer wall of unmanned aerial vehicle time domain avionics pod receiver 13, two arc splint bodies 91 finally realize pressing from both sides of unmanned aerial vehicle time domain avionics pod receiver 13, stop screwing down lead screw 10 after the elastic clamping spring clamp 11 effect down, the unmanned aerial vehicle time domain avionics pod receiver 13 is carried down to the top at the end.

It is noted that relational terms such as first and second, and the like are 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. Moreover, 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.

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

Claims

1. Unmanned aerial vehicle time domain avionics pod receiver stores pylon device, including top link plate (1), its characterized in that: the utility model discloses a roof link plate, including top link plate (1), fixed cover (3), fixed cover (5) that is provided with in the middle of the top four corners of top link plate (1) all screw thread run through bolt (2), fixed cover (3) that is provided with in the middle of the bottom of cover (3), fixed T template (5) that are provided with in the middle of the bottom of connecting ball (4), movable groove (6) have all been seted up on the bottom left and right sides of T template (5), two the inside of movable groove (6) all slides and is provided with square linking slider (7), two the bottom of square linking slider (7) is all fixed and is provided with loading board (8), two the one side lower part that loading board (8) are close to each other is all fixed and is provided with arc splint subassembly (9), the equal screw thread in the left and right sides of T template (5) runs through lead screw (10), evenly be provided with a plurality of telescopic spring (11) in the middle of the bottom of T template (5), a plurality of telescopic spring (11) are fixed down clamp plate (12) between the bottom.

2. An unmanned aerial vehicle time domain avionics pod receiver pylon device according to claim 1, wherein: one ends of the two screw rods (10) which are close to each other are respectively connected to the side walls of the adjacent square connecting sliding blocks (7) in a rotating way.

3. An unmanned aerial vehicle time domain avionics pod receiver pylon device according to claim 1, wherein: an unmanned aerial vehicle time domain avionics pod receiver (13) is arranged between the two bearing plates (8), the two arc-shaped clamping plate assemblies (9) and the lower pressure plate (12).

4. An unmanned aerial vehicle time domain avionics pod receiver pylon device according to claim 1, wherein: both the arc clamping plate assemblies (9) comprise arc clamping plate bodies (91), and the arc clamping plate bodies (91) are fixedly connected to the side walls of the corresponding bearing plates (8).

5. The unmanned aerial vehicle time domain avionics pod receiver pylon apparatus of claim 4, wherein: the inner wall of arc splint body (91) is fixed to be provided with protection pad (92), fixedly be provided with elasticity tensioning belt (93) between the inner chamber front and back end of arc splint body (91).

6. The unmanned aerial vehicle time domain avionics pod receiver pylon apparatus of claim 4, wherein: the top of the arc-shaped clamping plate body (91) is uniformly and fixedly provided with a plurality of anti-slip convex blocks (94).