Airplane trunk door lock structure
By using a double-spring locking component in the aircraft suitcase door lock structure, the problem of handle rebound causing harm to passengers is solved, achieving higher protection effect and convenient user experience.
Patent Information
- Application Number
- CN202421544751.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-07-02
- Publication Date
- 2025-05-06
- Estimated Expiration
- 2034-07-02
AI Technical Summary
The existing aircraft suitcase door lock structure is prone to rebound when closing the box door, which may cause harm to passengers.
The locking component adopts a double spring structure. When the box door is closed, the lock hook is fastened with the latch itself and does not interact with the handle to prevent the handle from rebounding.
Effectively prevent the handle from rebounding, improve the protection level of passengers' hands and the convenience of use, and avoid the damage caused by rebounding of the handle to passengers.
Smart Images
Figure CN222835538U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the field of luggage case structures, and more specifically, to an aircraft luggage case door lock structure. Background Art
[0002] In most existing luggage structures, the handle and the lock hook of the luggage are fixedly connected, so that as long as the handle is slightly turned, the lock hook can be driven to rotate, and then the lock hook is opened from the latch, so that the door and the box body are separated, and the purpose of opening the luggage is achieved.
[0003] In the aerospace field, the door handle and lock hook of a suitcase are also connected in a fixed manner. The rotation of the lock hook drives the handle to rotate. In this way, when closing the door, the passenger needs to move his hand away from the handle to prevent the rebounding handle from injuring the passenger during the closing process. The handle is generally located in the middle of the door, which is convenient for applying force to close the door. Therefore, when closing the door, the passenger can only choose between saving effort and safety. Utility Model Content
[0004] In order to overcome the above-mentioned defects of the prior art, an embodiment of the utility model provides an aircraft luggage compartment door lock structure. The technical problem to be solved by the utility model is: how to prevent the handle from rebounding during the process of closing the compartment door.
[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: an aircraft luggage compartment door lock structure, comprising a box body, installed in the cabin; a box door, rotatably connected to the box body; a door lock assembly, comprising a latch connected to the box body; a locking assembly, comprising a lock seat, a handle, a rotating shaft, a cam and a lock hook, the latch and the lock hook cooperate with each other, the lock seat is installed on the box door, the handle is elastically rotatably connected to the lock seat, the cam and the lock hook respectively located on the inner and outer sides of the lock seat rotate synchronously, a slot is provided at the side end of the handle, a block is fixed at the side end of the cam, the block is placed in the slot and the slot length of the slot is greater than the length of the block.
[0006] In a preferred embodiment, the latch is located on the moving path of the top end of the lock hook. When the lock hook and the latch collide, the lock hook slides against the latch and rotates upward until the lock hook catches the latch.
[0007] In a preferred embodiment, the handle is elastically rotatably connected to the lock seat via a handle spring, and a groove one is provided at corresponding positions of the lock seat and the handle, and two ends of the handle spring are respectively clamped in the corresponding groove one.
[0008] In a preferred embodiment, the lock hook is connected to the cam via a rotating shaft, the rotating shaft includes an integrally formed cylindrical section and a prismatic section, the cylindrical section is inserted into the rolled handle spring, and the cam and the lock hook are respectively sleeved on both ends of the prismatic section.
[0009] In a preferred embodiment, a second groove is provided at corresponding positions of the lock seat and the lock hook, two ends of the lock hook spring are respectively clamped in the second groove, and the prismatic section of the rotating shaft is inserted into the rolled lock hook spring.
[0010] In a preferred embodiment, two locking hooks are respectively arranged on both sides of the handle, and each locking hook is tightly matched with a corresponding locking latch.
[0011] In a preferred embodiment, the door lock assembly further comprises a latch cover, a clearance groove is provided on the latch cover, and when the latch cover is connected to the box body, the latch passes through the clearance groove.
[0012] In a preferred embodiment, an opening is retained on one side of the box body, and the top of the box door is rotatably connected to the top of the opening.
[0013] In a preferred embodiment, the lock seat and the handle are both in an inverted U shape with both sides tilted outwards.
[0014] In a preferred embodiment, a slot for allowing a user's finger to pass through is reserved between the lock seat and the handle, and the rotation centers of the lock seat and the handle are arranged away from the slot.
[0015] Technical effects and advantages of the utility model:
[0016] Compared with the prior art, this application has the following advantages:
[0017] 1. Both sides of the locking assembly adopt a double spring structure. When the door is closed, the lock hook can automatically fasten with the latch without being linked to the handle, thus avoiding damage to passengers caused by the rebound of the handle.
[0018] 2. The door lock adopts a double lock hook form, with a simple internal structure and reliable mechanical properties, and can be applied to various types of flip-up suitcases. BRIEF DESCRIPTION OF THE DRAWINGS
[0019] The accompanying drawings are used to provide a further understanding of the technical solution of the present utility model and constitute a part of the present utility model. The embodiments of the present utility model and their descriptions are used to explain the present utility model and do not constitute an improper limitation on the present utility model.
[0020] Figure 1 The utility model is a structural diagram of an aircraft luggage case.
[0021] Figure 2 This is a structural diagram of a part of the interior of the suitcase in the present invention.
[0022] Figure 3 It is a schematic diagram of the door lock structure in the utility model.
[0023] Figure 4 for Figure 3 A partial enlarged view of middle A.
[0024] Figure 5 It is an exploded view of the locking assembly in the present utility model.
[0025] The figures are marked as follows: 1. box body; 2. box door; 3. door lock assembly; 31. latch; 32. latch cover; 4. locking assembly; 41. lock seat; 42. handle; 43. rotating shaft; 44. cam; 45. lock hook; 46. handle spring; 47. lock hook spring. DETAILED DESCRIPTION
[0026] Example embodiments will now be described more fully with reference to the accompanying drawings. However, example embodiments can be implemented in a variety of forms and should not be construed as limited to the examples set forth herein; rather, these example embodiments are provided so that the description of the present disclosure will be more comprehensive and complete and the concepts of the example embodiments will be fully conveyed to those skilled in the art. The accompanying drawings are only schematic illustrations of the present disclosure and are not necessarily drawn to scale. The same reference numerals in the figures represent the same or similar parts, and thus their repeated description will be omitted.
[0027] In addition, the described features, structures or characteristics may be combined in one or more example embodiments in any suitable manner. In the following description, many specific details are provided to provide a full understanding of the example embodiments of the present disclosure. However, those skilled in the art will appreciate that the technical solutions of the present disclosure may be practiced while omitting one or more of the specific details, or other methods, components, steps, etc. may be adopted. In other cases, well-known structures, methods, implementations or operations are not shown or described in detail to avoid obscuring various aspects of the present disclosure.
[0028] Example
[0029] like Figure 1 - Figure 5 The utility model provides an aircraft luggage compartment door lock structure, which mainly includes a compartment body 1, a compartment door 2, a door lock assembly 3 and a locking assembly 4.
[0030] The box body 1 is installed on the upper part of both sides of the cabin of the aircraft and is used to store the luggage of passengers. An opening is reserved on one side of the box body 1 facing the cabin corridor.
[0031] The upper edge of the door 2 is rotatably connected to the upper edge of the opening to form a flip-up suitcase.
[0032] The locking function between the box body 1 and the box door 2 is achieved through the door lock assembly 3 and the locking assembly 4.
[0033] The door lock assembly 3 includes a latch 31 and a latch cover 32. The two latches 31 are fixed on the lower edge of the opening. A clearance groove is provided on the latch cover 32. When the latch cover 32 covers the lower edge of the opening, the latch 31 passes through the clearance groove and is exposed to the outside of the latch cover 32 to facilitate connection with the locking assembly 4.
[0034] The locking assembly 4 includes a lock seat 41, a handle 42, a rotating shaft 43, a cam 44, a lock hook 45, a handle spring 46, and a lock hook spring 47. The linkage design between the handle 42 and the lock hook 45 is mainly to prevent the lock hook 45 from being linked with the handle 42 when the box door 2 is closed, thereby preventing the handle 42 from popping out.
[0035] Specifically, the lock seat 41 is detachably connected to the lower edge side of the door 2 by bolt fasteners, and the lock seat 41 and the handle 42 are elastically rotatably connected by a handle spring 46. A groove 1 is provided on the corresponding ends of the lock seat 41 and the handle 42, and the two ends of the handle spring 46 are respectively stuck in the groove 1 of the lock seat 41 and the handle 42; when the handle 42 is rotated outward relative to the lock seat 41, the handle spring 46 is pulled, and when the force applied to the handle 42 is removed, the handle spring 46 drives the handle 42 to reset, thereby realizing the self-closing of the handle 42.
[0036] Preferably, when the handle 42 is closed, the handle 42 is pulled by the handle spring 46 and rotates and fits onto the lock seat 41 , a space is reserved between the lock seat 41 and the handle 42 for the user to insert his fingers to pick up the handle 42 .
[0037] The rotating shaft 43 includes two sections, one is a cylindrical section and the other is a prismatic section. The two sections are integrally formed and fixed to each other. The cylindrical section passes through the handle spring 46 to improve the stability of the position of the handle spring 46. The two ends of the prismatic section are respectively provided with a cam 44 and a lock hook 45. The edges of the prism enable the rotating shaft 43, the cam 44 and the lock hook 45 to rotate synchronously.
[0038] The rotating shaft 43 is horizontally rotatably connected to the lock base 41, the cam 44 and the lock hook 45 are respectively located on the inner and outer sides of the lock base 41, and both ends of the handle 42 are provided with a card slot. A card block is fixed on the cam 44, and the length of the card slot is greater than the length of the card block. The card block is placed in the card slot. In this way, the card block can move freely in the card slot until the card block hits the side wall of the card slot, which allows the cam 44 and the handle 42 to produce a joint movement.
[0039] Among them, the lock hook 45 and the lock seat 41 are elastically rotatably connected by a lock hook spring 47, that is, a groove 2 is provided on the lock hook 45 and the lock seat 41, and the two ends of the lock hook spring 47 are respectively clamped in the corresponding groove 2, and the prism section is penetrated in the lock hook spring 47 to improve the stability of the lock hook spring 47. When the lock hook 45 rotates upward, the lock hook 45 leaves the latch 31. When the external force on the lock hook 45 is withdrawn, the lock hook spring 47 drives the lock hook 45 to reset, allowing the lock hook 45 to rotate inward and buckle the latch 31 to achieve the locking purpose.
[0040] It should be noted that the latch 31 is located on the moving path of the lock hook 45. When the top of the lock hook 45 contacts the latch 31, the top of the lock hook 45 and the latch 31 will slide relative to each other, prompting the lock hook 45 to rotate upward to further lock the latch 31.
[0041] Here is a brief description of the working principle of the locking assembly 4:
[0042] In the stage of opening the door 2: the passenger buckles the handle 42 to drive the handle 42 to rotate. At this time, the card block and one side wall of the card slot are in contact. Therefore, the handle 42 can drive the lock hook 45 to rotate upward through the rotating shaft 43 and the cam 44 at the moment of rotation. The lock hook 45 and the latch 31 are separated, so that the door 2 can be opened easily.
[0043] When closing the door 2, the handle 42 retracts into the lock seat 41 under the reset action of the handle spring 46, and the passenger presses the outside of the handle 42 with his hand and presses it downward to close the door 2. During this process, when the lock hook 45 contacts the latch 31, the lock hook 45 will slide against the upper part of the latch 31, and the lock hook 45 rotates upward. At this time, the lock hook 45 drives the card block to rotate in the card slot through the rotating shaft 43 and the cam 44. During this process, the card block does not interfere with any side wall of the card slot, so there is no linkage relationship between the cam 44 and the handle 42. When the lock hook 45 rotates upward and buckles the latch 31, the handle 42 will not bounce up, thereby improving the protection of the passenger's hands.
[0044] In summary, compared with the prior art, this application has the following innovations and advantages:
[0045] 1. Both sides of the locking assembly 4 adopt a double spring structure. When the door 2 is closed, the lock hook 45 can be fastened with the latch 31 by itself without being linked with the handle 42, thereby improving the degree of protection for passengers and the convenience of use.
[0046] 2. The door lock adopts two symmetrical lock hooks 45, has a simple internal structure and reliable mechanical properties, and can be applied to various types of flip-up suitcases, not limited to the field of aircraft suitcases.
[0047] The above only describes some exemplary embodiments of the present invention by way of illustration. It is undoubted that those skilled in the art can modify the described embodiments in various ways without departing from the spirit and scope of the present invention. Therefore, the above drawings and descriptions are illustrative in nature and should not be construed as limiting the scope of protection of the claims of the present invention.
[0048] Finally, a few points should be explained: First, in the description of this application, it should be noted that, unless otherwise specified and limited, the terms "installed", "connected", and "connected" should be understood in a broad sense, which may refer to mechanical connection or electrical connection, or internal communication between two components, or direct connection. "upper", "lower", "left", "right", etc. are only used to indicate relative positional relationships. When the absolute position of the object being described changes, the relative positional relationship may change;
[0049] Secondly: In the drawings of the embodiments disclosed in the present utility model, only the structures related to the embodiments disclosed in the present utility model are involved, and other structures can refer to the general design. In the absence of conflict, the same embodiment and different embodiments of the present utility model can be combined with each other;
[0050] Finally: The above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present utility model should be included in the protection scope of the present utility model.
Claims
1. An aircraft luggage compartment door lock structure, characterized in that include: A box (1) is installed in the cabin; A box door (2) is rotatably connected to the box body (1); A door lock assembly (3) comprising a latch (31) connected to the box body (1); The locking assembly (4) comprises a lock seat (41), a handle (42), a rotating shaft (43), a cam (44) and a lock hook (45). The lock latch (31) and the lock hook (45) cooperate with each other. The lock seat (41) is installed on the box door (2). The handle (42) is elastically rotatably connected to the lock seat (41). The cam (44) and the lock hook (45) located inside and outside the lock seat (41) rotate synchronously. A card slot is provided at the side end of the handle (42). A card block is fixed at the side end of the cam (44). The card block is placed in the card slot and the slot length of the card slot is greater than the length of the card block.
2. The aircraft luggage compartment door lock structure according to claim 1, characterized in that: The lock latch (31) is located on the moving path of the top end of the lock hook (45). When the lock hook (45) and the lock latch (31) collide with each other, the lock hook (45) slides against the lock latch (31) and rotates upward until the lock hook (45) locks the lock latch (31).
3. The aircraft luggage compartment door lock structure according to claim 1, characterized in that: The handle (42) is elastically rotatably connected to the lock seat (41) via a handle spring (46); a groove (1) is provided at corresponding positions of the lock seat (41) and the handle (42); and two ends of the handle spring (46) are respectively clamped in the corresponding groove (1).
4. The aircraft luggage compartment door lock structure according to claim 1, characterized in that: The lock hook (45) is connected to the cam (44) via a rotating shaft (43). The rotating shaft (43) comprises an integrally formed cylindrical section and a prism section. The cylindrical section is inserted into a rolled handle spring (46). The cam (44) and the lock hook (45) are respectively sleeved on both ends of the prism section.
5. The aircraft luggage compartment door lock structure according to claim 3, characterized in that: A second groove is provided at corresponding positions of the lock seat (41) and the lock hook (45), and two ends of the lock hook spring (47) are respectively clamped in the second groove, and the prism section of the rotating shaft (43) is inserted into the rolled lock hook spring (47).
6. An aircraft luggage compartment door lock structure according to any one of claims 1 to 5, characterized in that: The two locking hooks (45) are respectively arranged on both sides of the handle (42), and each locking hook (45) is tightly matched with the corresponding locking latch (31).
7. The aircraft luggage compartment door lock structure according to claim 1, characterized in that: The door lock assembly (3) further comprises a latch cover (32), on which a clearance groove is provided. When the latch cover (32) is connected to the box body (1), the latch (31) passes through the clearance groove.
8. The aircraft luggage compartment door lock structure according to claim 1, characterized in that: An opening is retained on one side of the box body (1), and the top of the box door (2) is rotatably connected to the top of the opening.
9. The aircraft luggage compartment door lock structure according to claim 1, characterized in that: The lock seat (41) and the handle (42) are both in an inverted U shape with both sides tilted outwards.
10. An aircraft luggage compartment door lock structure according to claim 1 or 9, characterized in that: A slot for allowing a user's finger to pass through is reserved between the lock seat (41) and the handle (42), and the rotation centers of the lock seat (41) and the handle (42) are arranged away from the slot.