Airplane trunk top hoisting mechanism

Abstract

The utility model discloses an airplane trunk top hoisting mechanism, and particularly relates to the field of airplane trunk structures. The side face connecting assembly comprises a side plate support, a first toothed plate and a second toothed plate, the side plate support is fixed to the luggage case, and teeth located on the first toothed plate and teeth located on the second toothed plate are meshed with each other and fixed to the side plate support through a quick release part; one end of the vertical connecting assembly is connected with the second toothed plate, the other end of the vertical connecting assembly is connected with the machine body, the damping assembly comprises a lining, damping rubber, a metal inner ring and a rubber hoop, the lining is connected into the second toothed plate in an embedded mode, the damping rubber is sleeved with the lining, the metal inner ring is sleeved with the damping rubber, and the rubber hoop is buckled on the lining. The first toothed plate and the second toothed plate can be firmly fixed to the side plate support through the fixing effect of the tooth meshing structure matched with the screws, so that the stability of connection between the luggage case and the machine body is improved, and the probability of collision and abnormal sound can be reduced when the luggage case is vibrated in the flying process through the damping assembly.

Description

TECHNICAL FIELD

[0001] The utility model relates to the field of aircraft luggage case structure, more specifically, the utility model relates to an aircraft luggage case top hoisting mechanism. BACKGROUND

[0002] The load capacity of the luggage case of a civil aircraft needs to be designed to be large, and needs to simultaneously bear the related loads of flight conditions, ground conditions and emergency landing conditions, so the luggage case and the aircraft body structure must be firmly connected.

[0003] The existing connection mode is not high in stability, mainly because the bolt connection is susceptible to fastening failure and tightening abnormality, the thread groove is prone to wear during multiple screwing, leading to loose connection. In addition, the stability of the bolt connection is affected by factors such as material quality, design rationality and manufacturing process, and the sheet metal part itself is relatively thin, so the traditional connection mode is prone to damage of the connecting part, affecting the overall stability. SUMMARY

[0004] In order to overcome the above-mentioned defects of the prior art, the embodiments of the utility model provide an aircraft luggage case top hoisting mechanism, and the technical problem to be solved by the utility model is how to improve the installation stability of the luggage case of a civil aircraft.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical scheme: an aircraft luggage case top hoisting mechanism, comprising a luggage case; a side surface connecting assembly, comprising a side plate support, a toothed plate one and a toothed plate two, the side plate support is fixed with the luggage case, the teeth on the toothed plate one and the toothed plate two are engaged with each other, and the toothed plate one is fixed with the side plate support through a quick release part; a vertical connecting assembly, one end of which is connected with the toothed plate two, and the other end is connected with an aircraft body.

[0006] In a preferred embodiment, the direction of the teeth is perpendicular to the vertical direction.

[0007] In a preferred embodiment, the distance between adjacent teeth is 0.6mm.

[0008] In a preferred embodiment, the quick release part comprises a nut base, a nut buckle, a clamp and a screw, the nut base is fixed on the toothed plate two, the screw is sequentially inserted into the side wall of the luggage case, the toothed plate one and the toothed plate two, and then connected with the nut buckle, and the clamp is clamped outside the nut buckle to limit the nut buckle.

[0009] In a preferred embodiment, a slot hole is formed in the side plate support and the toothed plate one, a bushing is rotatably connected in the slot hole in an embedded manner, an open slot is formed in the bushing, and the screw can move in the long axis direction of the open slot.

[0010] In a preferred embodiment, the vertical connecting assembly comprises a pull rod, a connecting bracket, a sliding block and a sliding rail, the sliding rail is fixed on the machine body, the connecting bracket is connected with the pull rod and the second toothed plate through rotation, the sliding block is fixedly connected with the connecting bracket, and the sliding block is slidably connected with the sliding rail.

[0011] In a preferred embodiment, the lower end of the pull rod is embedded with a universal shaft, and the pin shaft penetrates through the universal shaft and the side plate bracket and is limited by the latch.

[0012] In a preferred embodiment, two adjacent luggage cases are connected to the machine body by the same vertical connecting assembly.

[0013] In a preferred embodiment, the mechanism further comprises a damping assembly, which comprises a bushing, damping rubber, a metal inner ring and a rubber clamp, the bushing is embeddedly connected in the second toothed plate, the damping rubber is sleeved in the bushing, the metal inner ring is sleeved in the damping rubber, and the rubber clamp is buckled on the bushing.

[0014] The technical effects and advantages of the utility model are as follows:

[0015] 1. The tooth engagement structure in the side connecting assembly increases the friction in the vertical direction, and the tooth engagement structure in cooperation with the fixing effect of the screw can firmly fix the first toothed plate and the second toothed plate on the side plate bracket, so that the stability of the connection between the luggage case and the machine body is improved.

[0016] 2. The tooth engagement structure of the first toothed plate and the second toothed plate also facilitates the adjustment of the positional relationship between the two in the vertical direction during installation, and the adjustment accuracy is high.

[0017] 3. The fixed nut buckle on the second toothed plate can be quickly disassembled, which is convenient for disassembly and replacement.

[0018] 4. The pull rod is provided with a universal shaft assembly, which increases the assembly tolerance of the assembly.

[0019] 5. The damping assembly can reduce the probability of collision and abnormal sound when the luggage case is subjected to vibration during flight. DRAWINGS

[0020] The drawings are used to provide a further understanding of the technical scheme of the utility model, and form a part of the utility model. The embodiments of the utility model and the description thereof are used to explain the utility model, and do not constitute an improper limitation on the utility model.

[0021] Figure 1 It is a schematic view of the hoisting mechanism of the utility model.

[0022] Figure 2 It is Figure 1 It is an enlarged view of A in the figure.

[0023] Figure 3 It is an exploded view of the hoisting mechanism of the utility model.

[0024] Figure 4 For Figure 3 Enlarged view of B.

[0025] Figure 5 For the lifting mechanism structure diagram in the utility model.

[0026] The figure mark is: 10, the suitcase;20, side face connecting assembly;21, side plate support;22, toothed plate one;23, toothed plate two;30, vertical connecting assembly;31, pull rod;32, connecting support;33, sliding block;34, slide rail;40, damping assembly;41, bushing;42, damping rubber;43, metal inner ring;44, rubber clamp. DETAILED DESCRIPTION

[0027] Example implementations will now be described more fully with reference to the accompanying drawings. Example implementations may, however, be implemented in many different forms and should not be construed as limited to the examples set forth herein; rather, these example implementations are provided so that this disclosure will be thorough and complete, and will fully convey the scope of example implementations to those skilled in the art. The accompanying drawings are included to provide a further understanding of the disclosure and are incorporated in and constitute a part of this disclosure. The drawings are not intended to be restrictive in any way.

[0028] In addition, the described features, structures, or characteristics can be combined in any suitable manner in one or more example implementations. In the following description, numerous specific details are provided to give a thorough understanding of example implementations of the disclosure. One skilled in the relevant art will recognize, however, that the techniques of the disclosure can be practiced without one or more of the specific details, or with other methods, components, materials, and so forth. In other instances, well-known structures, materials, or operations are not shown or described in detail in order to avoid obscuring aspects of the disclosure.

[0029] EMBODIMENTS

[0030] As Figures 1-5 A plane suitcase top lifting mechanism, comprising a suitcase 10, a side face connecting assembly 20, a vertical connecting assembly 30 and a damping assembly 40.

[0031] The suitcase 10 comprises all the components necessary for a suitcase itself, and is itself prior art, so no further description is given.

[0032] The side face connecting assembly 20 serves as a strong support component for improving the stability of the suitcase 10 connected to the body.

[0033] The vertical connecting assembly 30 can improve the flexibility of movement of the suitcase 10 on the body.

[0034] The shock absorbing assembly 40 can reduce the shock suffered by the luggage case 10 when the flight state of the aircraft changes.

[0035] The side connecting assembly 20 includes a side plate support 21, a toothed plate one 22, a toothed plate two 23, and a plurality of connecting components, including commonly used connecting components such as bushings, screws, gaskets, nut seats, etc. Without special instructions, the connecting components can be used by those skilled in the art to complete common connections.

[0036] The side plate support 21 is fixed to the side wall of the luggage case 10 by screws, gaskets, and bushings. The toothed plate one 22 and the toothed plate two 23 are arranged on one side of the side plate support 21. The nut seat is fixed to the toothed plate two 23 by rivets. The side plate support 21 and the toothed plate one 22 are both provided with a slot hole, and a bushing is embedded in the slot hole. An open slot is formed in the bushing. By determining the position of the bushing in the slot hole and changing the axis position of the open slot, the screw can move in the open slot. The screw threaded through the toothed plate one 22 is connected with the nut buckle on the toothed plate two 23. The nut buckle is fixed to the nut seat by a clamp to stabilize and limit the position of the toothed plate one 22 and the toothed plate two 23 on the side of the side plate support 21. Because the axis length of the open slot in the bushing is greater than the diameter of the screw, the toothed plate two 23 can move up and down relative to the toothed plate one 22 to adjust the connection position relationship.

[0037] The contact surface of the toothed plate one 22 and the toothed plate two 23 is provided with teeth. The teeth on the toothed plate one 22 and the toothed plate two 23 are engaged with each other, which improves the convenience of installing the toothed plate one 22 and the toothed plate two 23 and improves the friction between the toothed plate one 22 and the toothed plate two 23.

[0038] If only the screw is used to fasten the toothed plate one 22 and the toothed plate two 23, there is a risk of loosening. However, the combination of the screw and the tooth engagement structure can firmly fix the toothed plate one 22 and the toothed plate two 23 to the luggage case side support, thereby improving the stability of the connection.

[0039] Preferably, the distance between the teeth is 0.6 mm.

[0040] Preferably, the direction of the teeth is perpendicular to the vertical direction.

[0041] In this embodiment, the side plate support 21 is first fixed to the side wall of the luggage case 10, and then the position relationship of the toothed plate one 22 and the toothed plate two 23 is determined. Finally, the toothed plate one 22 and the toothed plate two 23 are fixed to one side of the side plate support 21.

[0042] The vertical connecting assembly 30 comprises a pull rod 31, a connecting bracket 32, a sliding block 33 and a sliding rail 34. One end of the pull rod 31 is embedded with a universal shaft, a pin shaft penetrates through the universal shaft, the rear of the side plate bracket 21 and extends into the inner wall of the luggage case 10, and is limited by a latch; after the other end is aligned with the connecting bracket 32, another pin shaft penetrates through the pull rod 31 and the connecting bracket 32, and the pin shaft is limited by a corresponding latch. In this way, the two ends of the pull rod 31 are rotatably connected with the side plate bracket 21 and the connecting bracket 32 respectively, and the connecting bracket 32 is fixed by a nut, a gasket and the sliding block 33. When in use, the sliding block 33 can slide into the sliding rail 34 from the side to drive the entire luggage case 10 to slide on the sliding rail 34 to adjust the left and right positions. The sliding rail 34 is fixed to the body.

[0043] When installed, the gap positions of the two luggage cases 10 are taken, the side plate bracket 21 is fixed to the corresponding positions of the two adjacent luggage cases 10, a pin shaft penetrates through the side connecting assembly 20 on one side, the vertical connecting assembly 30 and the side connecting assembly 20 on the other side in sequence, and finally a latch is inserted to prevent falling off.

[0044] Further, the damping assembly 40 comprises a bushing 41, a damping rubber 42, a metal inner ring 43 and a rubber clamp 44. The damping rubber 42 is sleeved in the bushing 41, the metal inner ring 43 is sleeved in the damping rubber 42, and the rubber clamp 44 is buckled on the bushing 41 to prevent the damping rubber 42 from falling off. The metal inner ring 43 is sleeved on the pin shaft penetrating through the universal shaft.

[0045] When the aircraft is shaken during operation, no matter where the vibration comes from, the body vibration is transmitted to the damping assembly 40 through the vertical connecting assembly 30. The damping rubber 42 in the damping assembly 40 can play a damping role to reduce the amplitude of the vibration further transmitted to the luggage case 10, thereby achieving the damping purpose and improving the stability of the luggage case 10 placed in the body.

[0046] In summary, the benefits of the present application are:

[0047] 1. The tooth meshing structure in the side connecting assembly 20 increases the friction in the vertical direction. The tooth meshing structure in combination with the fixing effect of the screw can firmly fix the tooth plate one 22 and the tooth plate two 23 on the side plate bracket 21, thereby improving the stability of the connection between the luggage case 10 and the body.

[0048] 2. The tooth meshing structure of the tooth plate one 22 and the tooth plate two 23 also facilitates the adjustment of the positional relationship between the two in the vertical direction during installation, and the adjustment accuracy is high.

[0049] 3. The fixed nut buckle on the tooth plate two 23 can be quickly disassembled, which is convenient for disassembly and replacement.

[0050] 4. The pull rod 31 is provided with a universal shaft assembly, which increases the assembly tolerance of the assembly.

[0051] 5. The shock absorbing assembly 40 reduces the probability of impact and abnormal sound when the luggage 10 is subjected to shock during flight.

[0052] The above merely describes certain exemplary embodiments of the present application by way of illustration, and it is needless to say that those skilled in the art can modify the described embodiments in various ways without departing from the spirit and scope of the present application. Therefore, the above drawings and descriptions are illustrative in nature and should not be construed as limiting the scope of protection of the present application.

[0053] Finally, it should be noted that: first, in the description of the present application, it should be pointed out that unless otherwise specified and limited, the terms "mounting", "connection", "connection" should be understood broadly, which can be mechanical connection or electrical connection, or the communication between two elements, or direct connection, "up", "down", "left", "right" and the like are only used to represent the relative positional relationship, when the absolute position of the described object changes, the relative positional relationship may change;

[0054] Secondly: the utility model discloses the embodiment figure, only relate to the structure of the embodiment of the present disclosure, other structures can refer to the usual design, under the condition of not conflicting, the same embodiment and different embodiments of the utility model can be combined with each other.

[0055] Finally: the above only is the preferred embodiment of the present application, and does not limit the present application, and any modification, equivalent replacement, improvement, etc. within the spirit and principle of the present application should be included in the protection scope of the present application.

Claims

1. An aircraft luggage bin overhead hoist mechanism, characterized by include: Suitcase (10); The side connection assembly (20) includes a side plate bracket (21), a toothed plate one (22) and a toothed plate two (23). The side plate bracket (21) is fixed to the luggage box (10). The teeth on the toothed plate one (22) and the toothed plate two (23) mesh with each other and are fixed to the side plate bracket (21) by quick release parts. The vertical connecting component (30) is connected to the toothed plate (23) at one end and to the body at the other end.

2. An aircraft overhead stowage mechanism according to claim 1, wherein: The direction of the teeth is perpendicular to the vertical direction.

3. An aircraft overhead stowage mechanism according to claim 1, wherein: The distance between adjacent teeth is 0.6 mm.

4. An aircraft overhead stowage mechanism according to claim 1, wherein: The quick-release component includes a nut base, a nut buckle, a clamp, and a screw. The nut base is fixed on the second toothed plate (23). The screw passes through the side wall of the suitcase (10), the first toothed plate (22), and the second toothed plate (23) in sequence and then connects to the nut buckle. The clamp is placed on the outside of the nut buckle to limit its position.

5. An aircraft luggage container top hoist mechanism according to claim 4, characterised in that: The side plate bracket (21) and the toothed plate (22) are both provided with slots, and a bushing is embedded in the slot for rotational connection. The bushing is provided with an open slot, and the screw can move in the direction of the long axis of the open slot.

6. An aircraft overhead stowage mechanism according to claim 1, wherein: The vertical connection assembly (30) includes a pull rod (31), a connecting bracket (32), a slider (33), and a slide rail (34). The slide rail (34) is fixed to the machine body. The connecting bracket (32) is rotatably connected to the pull rod (31) and the toothed plate (23). The slider (33) is fixedly connected to the connecting bracket (32), and the slider (33) is slidably connected to the slide rail (34).

7. An aircraft luggage container top hoist mechanism according to claim 6, characterised in that: The lower end of the pull rod (31) is internally connected to a universal joint, and the pin passes through the universal joint and the side plate bracket (21) and is limited by the pin.

8. An aircraft overhead stowage mechanism according to claim 1 or 6, wherein: The two adjacent suitcases (10) are connected to the body by the same vertical connecting component (30).

9. An aircraft overhead stowage bin mechanism according to claim 1, wherein: The mechanism is also provided with a shock-absorbing component (40), including a bushing (41), a shock-absorbing rubber (42), a metal inner ring (43), and a rubber clamp (44). The bushing (41) is embedded in the toothed plate (23), the shock-absorbing rubber (42) is fitted inside the bushing (41), the metal inner ring (43) is fitted inside the shock-absorbing rubber (42), and the rubber clamp (44) is fastened to the bushing (41).

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