CN212260273U

CN212260273U - Shock wave launching gun

Info

Publication number: CN212260273U
Application number: CN202020369033.4U
Authority: CN
Inventors: 郑玉勇; 沙艳
Original assignee: Dalian Huixin Technology Co ltd
Current assignee: Dalian Huixin Technology Co ltd
Priority date: 2020-03-23
Filing date: 2020-03-23
Publication date: 2021-01-01
Anticipated expiration: 2030-03-23

Abstract

The utility model discloses a shock wave launches big gun, including launching big gun main part, the rotating turret, buffering subassembly, the support column, the main support, a fixed base, the engaging lug, the mount, the electric cabinet, the fuel jar, first telescopic link, first subframe, rag bolt, second telescopic link and second subframe, buffering subassembly is by fixed casing, the dashpot, first connecting plate, buffer spring, the sleeve, the connecting block, the sliding block, the spout, first compression spring, second compression spring and second connecting plate are constituteed, this novel, can expel 90% birds and external wild animal, shock waves such as hawk, wild goose, aigrette, sparrow class and wild duck that the airport can't be driven away in the past can all be driven away from it, and these birds that are driven away and external wild animal can't adapt to it, can not produce the tolerance; the installation mode is nimble, and the angle of adjustment of being convenient for, and the adjustment process is stable, has brought revolutionary change for driving bird work in airport.

Description

Shock wave launching gun

Technical Field

The utility model relates to a bird equipment technical field is driven in the airport specifically is a shock wave transmission big gun.

Background

Bird repelling is also called bird repelling, and English is called bird repellent. In a broad sense, all the means for preventing harmful birds from invading the land of a farm, an orchard, a wind power plant, a military and civil airport and the like, so that the harm to the labor result or the equipment safety are called to drive the birds; in narrow sense, the term of bird repelling refers to all means such as auditory scaring, visual frightening, direct killing, chemical, ecological or radar early warning and the like for preventing birds from invading in key flight areas of airports, especially runways or taxiways for taking off and landing airplanes, in order to protect the taking off and landing safety of aircrafts and prevent the birds from being sucked into airplane engines or impacting airplane bodies such as airplane bodies, landing gears, empennages, windshields and the like when the airplanes take off and land at high speed. However, the existing bird repelling equipment is easy to cause the birds to have tolerance, and the using effect is greatly reduced, so that the design of the shock wave launching gun is necessary.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a shock wave launches big gun to solve the problem that proposes among the above-mentioned background art.

In order to solve the technical problem, the utility model provides a following technical scheme: a shock wave launching gun comprises a launching gun body, a rotating frame, a buffering assembly, a supporting column, a main support, a fixed seat, a connecting lug, a fixed frame, an electric cabinet, a fuel tank, a first telescopic rod, a first auxiliary support, a foundation bolt, a second telescopic rod and a second auxiliary support, wherein the rotating frame is rotatably installed in the middle of the side face of the launching gun body through a pin shaft and is welded and fixed in the center of the top end of the supporting column, the buffering assembly is arranged on each of two sides of the top end of the supporting column, the buffering assembly consists of a fixed shell, a buffering groove, a first connecting plate, a buffering spring, a sleeve, a connecting block, a sliding groove, a first compression spring, a second compression spring and a second connecting plate, the buffering groove is formed in the top of the fixed shell, the first connecting plate is welded and fixed in the center of the bottom of the buffering groove, and the buffer spring is sleeved with a sleeve, the tops of the two sides of the sleeve are fixedly welded with connecting blocks, the connecting blocks are matched and slidably connected with sliding grooves through sliding blocks, the sliding grooves are correspondingly arranged on the two sides of the inner wall of the buffer groove, the sliding grooves are vertically arranged, the top end of the buffer spring is fixedly connected with the bottom of a second connecting plate, the top of the second connecting plate is movably connected with the bottom of the side surface of the launching gun main body through hinges, the side surface of the supporting column is fixedly welded with a fixing frame, the two sides of the top of the fixing frame are fixedly provided with an electric control box and a fuel tank correspondingly, the bottom of the supporting column is fixedly welded at the center of the top of the fixing base, the side surface of the supporting column is also fixedly welded with a main support, the bottom of the main support is fixedly welded at the top of the fixing, and the first telescopic rod and the second telescopic rod are vertically welded and fixed on the first auxiliary support and the second auxiliary support respectively.

Furthermore, the top four corners of fixing base all welded fastening has the engaging lug, and rag bolt is still installed at the top of fixing base.

Further, the electric cabinet and the fuel tank are connected with the fixing frame through bolts, liquefied gas or ethylene is filled in the fuel tank, and the electric cabinet and the fuel tank are respectively connected with the launching gun main body through electric wires and pipelines.

Furthermore, a first compression spring and a second compression spring are vertically fixed at the bottom end and the top end of the sliding groove respectively.

Compared with the prior art, the utility model discloses the beneficial effect who reaches is: the shock wave launching gun can effectively solve the problem of bird repelling in airports, can repel 90% of birds and foreign wild animals, can repel hawks, wild gooses, aigrens, sparrows, wild ducks and other shock waves which cannot be repelled from airports in the past, cannot adapt to the repelled birds and the foreign wild animals, and cannot generate tolerance; this novel mounting means is nimble, and the angle of adjustment of being convenient for, and adjustment process is stable, and the bird work of driving for the airport has brought revolutionary change, will become the bird sharp ware that drives that new generation is indispensable, can't be substituted in the airport.

Drawings

The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention.

In the drawings:

fig. 1 is a schematic view of the overall plane structure of the present invention;

FIG. 2 is a schematic structural view of the cushion assembly of the present invention;

in the figure: 1. launching a cannon main body; 2. a rotating frame; 3. a buffer assembly; 4. a support pillar; 5. a main support; 6. a fixed seat; 7. connecting lugs; 8. a fixed mount; 9. an electric cabinet; 10. a fuel tank; 11. a first telescopic rod; 12. a first sub-mount; 13. anchor bolts; 14. a second telescopic rod; 15. a second subframe; 31. a stationary housing; 32. a buffer tank; 33. a first connecting plate; 34. a buffer spring; 35. a sleeve; 36. connecting blocks; 37. a slider; 38. a chute; 39. a first compression spring; 310. a second compression spring; 311. a second connecting plate.

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. 1-2, the present invention provides a technical solution: a shock wave launching gun comprises a launching gun body 1, a rotating frame 2, a buffer component 3, a supporting column 4, a main support 5, a fixed seat 6, a connecting lug 7, a fixed frame 8, an electric cabinet 9, a fuel tank 10, a first telescopic rod 11, a first auxiliary support 12, an anchor bolt 13, a second telescopic rod 14 and a second auxiliary support 15, wherein the rotating frame 2 is rotatably installed in the middle of the side face of the launching gun body 1 through a pin shaft, the rotating frame 2 is fixedly welded in the center of the top end of the supporting column 4, the buffer component 3 is arranged on both sides of the top end of the supporting column 4, the buffer component 3 comprises a fixed shell 31, a buffer groove 32, a first connecting plate 33, a buffer spring 34, a sleeve 35, a connecting block 36, a sliding block 37, a sliding groove 38, a first compression spring 39, a second compression spring 310 and a second connecting plate 311, the buffer groove 32 is formed in the top of the fixed shell 31, and the first connecting plate, the top of the first connecting plate 33 is fixedly connected with the bottom end of the buffer spring 34, the buffer spring 34 is sleeved with a sleeve 35, the tops of two sides of the sleeve 35 are respectively welded and fixed with a connecting block 36, the connecting block 36 is matched and slidably connected with a sliding groove 38 through a sliding block 37, the sliding grooves 38 are correspondingly arranged on two sides of the inner wall of the buffer groove 32, the sliding grooves 38 are vertically arranged, the bottom end and the top end of the sliding groove 38 are respectively vertically fixed with a first compression spring 39 and a second compression spring 310, so as to buffer the pressure of the connecting position, the top end of the buffer spring 34 is fixedly connected with the bottom of a second connecting plate 311, the top of the second connecting plate 311 is movably connected with the bottom of the side surface of the launching cannon main body 1 through a hinge, the side surface of the supporting column 4 is welded and fixed with a fixing frame 8, the two sides of the top of the fixing frame 8 are correspondingly and, liquefied gas or ethylene is filled in the fuel tank 10, the electric cabinet 9 and the fuel tank 10 are respectively connected with the launching gun main body 1 through an electric wire and a pipeline, the use is convenient, the bottom of the supporting column 4 is welded and fixed at the center of the top of the fixing seat 6, the main support 5 is also welded and fixed on the side surface of the supporting column 4, four corners of the top of the fixing seat 6 are respectively welded and fixed with connecting lugs 7, foundation bolts 13 are further installed at the top of the fixing seat 6 and are convenient to connect, the bottom of the main support 5 is welded and fixed at the top of the fixing seat 6, two sides of the bottom of the launching gun main body 1 are respectively movably connected with output ends of a first telescopic rod 11 and a second telescopic rod 14, and the first telescopic rod 11 and the second telescopic rod 14; when the utility model is used, the device can be fixedly arranged on both sides of the runway through the fixed seat 6 and the foundation bolt 13, and can also be arranged on the bird-repelling vehicle through the fixed seat 6 and the connecting lug 7, and the mounting mode is flexible; the angle of launching big gun main part 1 is changed through the height of adjusting first telescopic link 11 and second telescopic link 14, simultaneously at angle of adjustment's in-process, launching big gun main part 1 oppresses buffer spring 34 through second connecting plate 311, utilize buffer spring 34's elastic force, the stability of adjustment process has been guaranteed, buffer spring 34's compression displacement drives sleeve 35 and removes, sleeve 35 drives sliding block 37 through connecting block 36 and slides from top to bottom in spout 38 is inside, first compression spring 39 and second compression spring 310 can cushion the impact force of sliding block 37 to spout 38 both ends, the stationarity has further been increased, do benefit to the use.

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.

Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. The utility model provides a shock wave transmission big gun, includes transmission big gun main part (1), rotating turret (2), buffering subassembly (3), support column (4), main support (5), fixing base (6), engaging lug (7), mount (8), electric cabinet (9), fuel jar (10), first telescopic link (11), first auxiliary support (12), rag bolt (13), second telescopic link (14) and second auxiliary support (15), its characterized in that: the launching gun comprises a launching gun body (1), wherein a rotating frame (2) is rotatably arranged in the middle of the side face of the launching gun body (1) through a pin shaft, the rotating frame (2) is fixedly welded at the center of the top end of a supporting column (4), buffering components (3) are arranged on two sides of the top end of the supporting column (4), each buffering component (3) consists of a fixed shell (31), a buffering groove (32), a first connecting plate (33), a buffering spring (34), a sleeve (35), a connecting block (36), a sliding block (37), a sliding groove (38), a first compression spring (39), a second compression spring (310) and a second connecting plate (311), the buffering groove (32) is formed in the top of the fixed shell (31), the first connecting plate (33) is fixedly welded at the center of the bottom of the buffering groove (32), the top of the first connecting plate (33) is fixedly connected with the bottom end of the buffering spring (34), and the sleeve (35, the top parts of two sides of the sleeve (35) are respectively welded and fixed with a connecting block (36), the connecting blocks (36) are matched and slidably connected with sliding grooves (38) through sliding blocks (37), the sliding grooves (38) are correspondingly arranged on two sides of the inner wall of the buffer groove (32), the sliding grooves (38) are vertically arranged, the top ends of the buffer springs (34) are fixedly connected with the bottom of a second connecting plate (311), the top of the second connecting plate (311) is movably connected with the bottom of the side surface of the launching gun main body (1) through hinges, a fixing frame (8) is welded and fixed on the side surface of the supporting column (4), an electric cabinet (9) and a fuel tank (10) are correspondingly and fixedly installed on two sides of the top of the fixing frame (8), the bottom of the supporting column (4) is welded and fixed at the center of the top of the fixing seat (6), and a main support (5) is further, the bottom welded fastening of main support (5) is at the top of fixing base (6), the bottom both sides of launching big gun main part (1) respectively with the output swing joint of first telescopic link (11) and second telescopic link (14), and first telescopic link (11) and second telescopic link (14) vertical welded fastening respectively on first auxiliary support (12) and second auxiliary support (15).

2. The shockwave launching gun according to claim 1, wherein: the top four corners of fixing base (6) all welded fastening has engaging lug (7), and rag bolt (13) are still installed at the top of fixing base (6).

3. The shockwave launching gun according to claim 1, wherein: the electric cabinet (9) and the fuel tank (10) are connected with the fixing frame (8) through bolts, liquefied gas or ethylene is filled in the fuel tank (10), and the electric cabinet (9) and the fuel tank (10) are respectively connected with the launching gun main body (1) through electric wires and pipelines.

4. The shockwave launching gun according to claim 1, wherein: and a first compression spring (39) and a second compression spring (310) are respectively and vertically fixed at the bottom end and the top end of the sliding chute (38).