CN115140430A - High-reliability aviation case with auxiliary locking function - Google Patents

Abstract

The invention discloses a high-reliability aviation case with an auxiliary locking function, which comprises a case body and a case door positioned at an opening of the case body, wherein an iron shaft is fixedly connected to the outer wall of the case door, a case body is fixedly connected to the outer wall of the case door, the case body is symmetrically connected with two insertion rods through a rebounding mechanism, a connecting seat is integrally formed at the position, corresponding to the end parts of the iron shaft and the insertion rods, of the outer wall of the opening of the case body, and a jack matched with the iron shaft and the insertion rods is arranged on the connecting seat in a penetrating manner; according to the invention, when the aviation case is used for transporting pets, the aviation case can be matched with the corresponding iron shaft or the threaded end of the inserted link by rotating the hand-screwed bolt so as to lock the iron shaft and the inserted link, so that the connection stability of the case door and the case body is effectively improved, the case door is prevented from being automatically opened in the transportation process, the operation is simple and convenient, and the inserted link can be operated through the protruding part if the hand-screwed bolt is not screwed down, so that the case door can be quickly opened and closed.

Description

High reliability aviation case with supplementary locking function

Technical Field

The invention relates to a pet flight case, in particular to a high-reliability flight case with an auxiliary locking function.

Background

At present, the conventional pet flight case is generally locked by inserting two up-and-down movable inserting rods into corresponding inserting holes in the case body, and the mode is simple and direct, but in the transportation process of animals or pets, the firmness is poor and needs to be improved.

Disclosure of Invention

The invention aims to provide a high-reliability aviation case with an auxiliary locking function, so as to solve the problems in the background technology.

In order to achieve the purpose, the invention provides the following technical scheme:

the utility model provides a high reliability aviation case with supplementary locking function, includes the box and is located the chamber door of box opening part, the outer wall fixedly connected with iron axle of chamber door, the outer wall fixedly connected with box body of chamber door, the box body has two inserted bars through resilient means symmetric connection, the opening part outer wall of box has the connecting seat with the homogeneous shaping of the department that corresponds of the tip of iron axle and inserted bar, run through on the connecting seat be provided with the jack of iron axle and inserted bar looks adaptation, the jack is the toper flaring setting towards the one end of chamber door, the outer wall joint of connecting seat has the switching seat, the activity runs through on the switching seat and is provided with the hand and twists the nut, the both ends of iron axle and the one end that the box body was kept away from to the inserted bar all are provided with the external screw thread, the screw thread end of iron axle, inserted bar is located the connecting seat that corresponds and twists nut looks adaptation with the hand.

As a further scheme of the invention: the resilience mechanism is including being located the spring of box body, the both ends of spring all are provided with the connecting plate, the one end of inserted bar runs through behind the outer wall of box body and the connecting plate fixed connection who corresponds.

As a further scheme of the invention: the outer wall of the inserted bar, which is close to the box body, is bent to form a protruding portion, the outer wall is sleeved with a guide sleeve in a sliding mode, and the guide sleeve is fixedly connected with the box door.

As a further scheme of the invention: the outer wall of adapter is provided with a plurality of buckles, the draw-in groove of looks adaptation is all seted up with the department that corresponds of buckle to the outer wall of connecting seat.

As a still further scheme of the invention: the hand is twisted the one end outer wall that the nut is located the adapter and is gone out integrated into one piece and is had the toper boss, set up the perforation with hand nut-screwing looks adaptation on the adapter, the external diameter that the toper boss is close to the perforation end is greater than fenestrate aperture.

Compared with the prior art, the invention has the beneficial effects that:

1. according to the invention, when the aviation case is used for transporting pets, the aviation case can be matched with the corresponding iron shaft or the threaded end of the inserted link by rotating the hand-screwed bolt so as to lock the iron shaft and the inserted link, so that the connection stability of the case door and the case body is effectively improved, the case door is prevented from being automatically opened in the transportation process, the operation is simple and convenient, and the inserted link can be operated through the protruding part if the hand-screwed bolt is not screwed down, so that the case door can be quickly opened and closed.

2. According to the invention, the jack with the conical flaring on the connecting seat can guide the end part of the inserted bar in the inserting process of the inserted bar, so that the inserted bar can be inserted into the corresponding jack more conveniently.

Drawings

Fig. 1 is a schematic structural diagram of a high-reliability aviation case with an auxiliary locking function.

Fig. 2 is a schematic cross-sectional view of a connection seat in a high reliability aviation case having an auxiliary locking function.

Fig. 3 is a partial exploded view of a high reliability aviation case with an auxiliary locking function.

Fig. 4 is an enlarged view of a point a in fig. 1.

The box comprises a box body 1, a box door 2, an iron shaft 3, an inserting rod 4, a protruding part 5, a box body 6, a connecting plate 7, a spring 8, a guide sleeve 9, a connecting seat 10, an adapter 11, a buckle 12 and a hand-screwed nut 13.

Detailed Description

In order to make the technical problems, technical solutions and advantageous effects to be solved by the present invention more apparent, the present invention will be further described in detail with reference to the following embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.

It will be understood that when an element is referred to as being "secured to" or "disposed on" another element, it can be directly on the other element or be indirectly on the other element. When an element is referred to as being "connected to" another element, it can be directly connected to the other element or be indirectly connected to the other element.

It will be understood that the terms "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships that are based on the orientations or positional relationships shown in the drawings, are used merely to facilitate description of the present invention and to simplify description, and do not indicate or imply that the referenced devices or elements must have the particular orientations, configurations and operations described in the specification, and therefore are not to be considered limiting.

Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or to implicitly indicate the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature.

Referring to fig. 1 to 4, in the embodiment of the invention, a high-reliability aviation case with an auxiliary locking function includes a case body 1 and a case door 2 located at an opening of the case body 1, an iron shaft 3 is fixedly connected to an outer wall of the case door 2, a case body 6 is fixedly connected to an outer wall of the case door 2, the case body 6 is symmetrically connected to two insertion rods 4 through a rebounding mechanism, a connection seat 10 is integrally formed at a position, corresponding to end portions of the iron shaft 3 and the insertion rods 4, of an outer wall of the opening of the case body 1, a jack matched with the iron shaft 3 and the insertion rods 4 penetrates through the connection seat 10, one end, facing the case door 2, of the jack is in a conical flaring shape, an adapter seat 11 is clamped to an outer wall of the connection seat 10, a hand-screwed nut 13 is movably arranged on the adapter seat 11 in a penetrating manner, external threads are arranged at two ends of the iron shaft 3 and one end, far away from the case body 6, of the insertion rods 4 are located in the corresponding connection seat 10 and matched with the hand-screwed nut 13.

The resilience mechanism is including being located the spring 8 of box body 6, the both ends of spring 8 all are provided with connecting plate 7, the one end of inserted bar 4 runs through behind the outer wall of box body 6 with the connecting plate 7 fixed connection that corresponds.

Through the cooperation of spring 8 and two connecting plates 7, can utilize spring 8 to promote two inserted bars 4 simultaneously.

The outer wall of the inserted bar 4 close to the box body 6 is provided with a protruding part 5 in a bending mode, the outer wall of the inserted bar 4 is sleeved with a guide sleeve 9 in a sliding mode, and the guide sleeve 9 is fixedly connected with the box door 2.

Through the setting of bellying 5, be convenient for operate inserted bar 4, guide pin bushing 9 can play the retaining effect to inserted bar 4, can improve the stability when inserted bar 4 removes simultaneously.

The outer wall of adapter 11 is provided with a plurality of buckles 12, the draw-in groove of looks adaptation is all seted up with buckle 12's the department that corresponds to the outer wall of connecting seat 10.

The matching of the buckle 12 and the clamping groove facilitates the assembly of the connecting seat 11 on the connecting seat 10.

Hand is twisted nut 13 and is located the one end outer wall of adapter 11 and goes out integrated into one piece and have the toper boss, set up on the adapter 11 with the perforation of hand-screwed nut 13 looks adaptation, the external diameter that the toper boss is close to the perforation end is greater than fenestrate aperture, in the perforation that inserts the correspondence with toper hand-screwed bolt 13 for the convenience when the assembly, hand-screwed bolt 13 and adapter 11 all adopt the plastics material that has certain elasticity.

Through the setting of toper boss, can play limiting displacement to hand on adapter 11 and twist bolt 13 to avoid hand to twist bolt 13 and drop by adapter 11.

The working principle of the invention is as follows:

in the invention, when the aviation case is used for transporting pets, the manual screwing bolt 13 can be rotated to be matched with the corresponding threaded end of the iron shaft 3 or the corresponding threaded end of the inserted rod 4 so as to lock the iron shaft 3 and the inserted rod 4, so that the connection stability of the case door 2 and the case body 1 is effectively improved, the case door 2 is prevented from being automatically opened in the transportation process, the operation is simple and convenient, and if the manual screwing bolt 13 is not screwed, the inserted rod 4 can be operated through the bulge part 5, so that the case door 2 can be quickly opened and closed.

The insertion holes with the conical flares on the connecting seat 10 can play a role in guiding the end portions of the insertion rods 4 in the insertion process of the insertion rods 4, so that the insertion rods 4 can be inserted into the corresponding insertion holes more conveniently.

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.

Claims (5)

1. The utility model provides a high reliability aviation case with supplementary locking function which characterized in that: including box (1) and chamber door (2) that are located box (1) opening part, the outer wall fixedly connected with iron axle (3) of chamber door (2), outer wall fixedly connected with box body (6) of chamber door (2), box body (6) have two inserted bars (4) through resilient means symmetrical connection, the opening part outer wall of box (1) has connecting seat (10) with the homogeneous shaping of the department of correspondence of the tip of iron axle (3) and inserted bar (4), it is provided with the jack with iron axle (3) and inserted bar (4) looks adaptation to run through on connecting seat (10), the jack is the toper flaring setting towards the one end of chamber door (2), the outer wall joint of connecting seat (10) has switching seat (11), the activity runs through on switching seat (11) is provided with hand screw nut (13), the both ends of iron axle (3) and the one end that box body (6) was kept away from in inserted bar (4) all are provided with the external screw thread, the screw end of iron axle (3), inserted bar (4) be located corresponding connecting seat (10) and screw nut (13) looks adaptation with hand screw nut (13).

2. The high-reliability aviation case with the auxiliary locking function as claimed in claim 1, wherein: the resilience mechanism is including spring (8) that is located box body (6), the both ends of spring (8) all are provided with connecting plate (7), the one end of inserted bar (4) run through behind the outer wall of box body (6) with connecting plate (7) fixed connection that corresponds.

3. The high-reliability aviation case with the auxiliary locking function as claimed in claim 1, wherein: the outer wall of the inserted bar (4) close to the box body (6) is provided with a protruding portion (5) in a bent mode, the outer wall of the inserted bar (4) is sleeved with a guide sleeve (9) in a sliding mode, and the guide sleeve (9) is fixedly connected with the box door (2).

4. The high-reliability aviation case with the auxiliary locking function as claimed in claim 1, wherein: the outer wall of adapter (11) is provided with a plurality of buckles (12), the draw-in groove of looks adaptation is all seted up with the department that corresponds of buckle (12) to the outer wall of connecting seat (10).

5. A high reliability flight box with auxiliary locking function according to claim 1, characterized in that: the hand is twisted nut (13) and is located the one end outer wall of adapter (11) and go out integrated into one piece and have the toper boss, set up the perforation with hand is twisted nut (13) looks adaptation on adapter (11), the external diameter that the toper boss is close to the perforation end is greater than the fenestrate aperture.

Images