Movable space capsule for hotel accommodation

Abstract

The invention relates to the technical field of space cabins, and discloses a movable space cabin for hotel accommodation, comprising: a space cabin body for establishing a living space and generating a basis for carrying furniture; the two supporting assemblies are mounted at the lower end of the space capsule body, are symmetrically arranged front and back, are used for stably supporting the space capsule at a single position and assisting in moving during position conversion, and comprise abutting columns mounted at the lower end of the space capsule body; the lower end of the abutting column is provided with an adjusting piece for switching supporting and moving states. And the lifting piece and the supporting assembly are arranged at the lower end of the space capsule body in a staggered mode. The problem that movement of an existing space capsule completely depends on hoisting equipment is solved.

Description

Technical Field

[0001] The invention relates to the technical field of space cabin rooms, in particular to a movable space cabin room for hotel accommodation. Background Art

[0002] A space capsule disclosed in the utility model with authorization announcement number CN206653979U includes a frame, which includes an upper frame, two side frames, a support rod, and a lower frame. The upper frame and the lower frame are respectively fixed to the two side frames and the support rod by cross-slot pan head bolts; the inner surface of the upper frame is provided with a leather soft bag, and a solid wood decorative panel is fixed to the upper frame; the inner surface of the side frame is provided with a leather soft bag, and a leather soft bag is fixed to the side frame.

[0003] During the application of this technical solution, the space capsule is installed or moved by hoisting. The installation or transfer cost is too high and it is easy to cause damage to the space capsule. There are also technical problems such as the inability to conveniently and quickly transfer the space capsule and ensure the stability of the space capsule before and after transfer. Summary of the invention

[0004] In view of the deficiencies of the prior art, the present invention provides a movable space capsule room for hotel accommodation, which solves the problem that the movement of the existing space capsule is completely dependent on hoisting equipment.

[0005] To achieve the above object, the present invention provides the following technical solution: a movable space capsule room for hotel accommodation, comprising:

[0006] The space cabin body, which establishes the living space and forms the basis for the furniture;

[0007] A support assembly, which is installed at the lower end of the space cabin body and is symmetrically arranged in two groups, used to provide stable support for the space cabin at a single position and auxiliary movement during position conversion, and includes an abutment column installed at the lower end of the space cabin body, and an adjustment member for converting support and movement state is arranged at the lower end of the abutment column;

[0008] A lifting member, which is arranged at the lower end of the space cabin body in a displaced manner with the supporting assembly;

[0009] The lifting member is used to support the space cabin body to adjust its own height and establish an adjustment member to change the space for the function conversion of the space cabin body.

[0010] In a specific embodiment, the adjusting member includes an adjusting plate rotatably connected to the abutting column, a brake wheel for assisting the movement of the space cabin body is installed on the adjusting plate, and a support member for assisting the space cabin body to be stabilized on a preset placement surface is arranged on the adjusting plate misaligned with the mounting position of the brake wheel;

[0011] The support member is composed of a support rod and a support sleeve. A cavity for accommodating the support rod is opened inside the support sleeve. A convex column is arranged on the bottom plate of the inner cavity. An inner groove for accommodating the convex column is installed on the support rod. The port width of the cavity is larger than its internal width. The extension depth of the support rod into the support sleeve is greater than the height of the support rod itself. A hooking member for interacting with the inner wall of the support sleeve is installed on the side wall of the support rod.

[0012] In a specific embodiment, the brake wheel includes a wheel body and a connecting block disposed between the wheel body and the abutment column, wherein the connecting block extends a connection point between the wheel body and the abutment column;

[0013] A port is provided at one end of the support sleeve, the width of the port is equal to the width of the connecting block, and the length of the port on the support sleeve is equal to the diameter of the brake disc.

[0014] In a specific embodiment, the hooking member includes a clamping end arranged in the inner groove, and the clamping end is symmetrically arranged in the inner wall of the support rod with the axis of the inner groove as the symmetry center line, and two cones with different diameters that are mirror-symmetrical in upper and lower directions are installed on the convex column.

[0015] In a specific embodiment, the clamping end extends outward or retracts in the receiving groove, and a compression spring connected to the wall of the receiving groove is installed on the free end of the clamping end that moves in the receiving groove.

[0016] In a specific embodiment, the support rod structure is provided with a receiving groove connected to the inner groove, the lifting member includes a lifting end and a supporting end, the lifting end is retracted inside the supporting end or extends outward, and the supporting end and the supporting sleeve are both provided with connecting ends, and the connecting end of the supporting sleeve is installed at the bottom thereof.

[0017] In a specific embodiment, it is described that the end surface where the clamping end meets the frustum is triangular in shape, and its inclination angle is adapted to the inclination of the side wall of the frustum.

[0018] In a specific embodiment, it is described that the installation position of the brake wheel on the adjustment disk is at an angle of ninety degrees to the support member.

[0019] Compared with the prior art, the present invention provides a movable space capsule room for hotel accommodation. Based on the current situation that the movement of the existing space capsule is completely dependent on the hoisting equipment, the present invention has the following beneficial effects:

[0020] In the technical solution disclosed in the present invention, a support assembly is provided, which produces two state conversions for the space cabin room body. When the space cabin room body is located at a preset stop position, the support assembly produces a supporting effect on the space cabin room body to assist the space cabin room body in maintaining a stable state. When the space cabin room needs to be adjusted to a lower position, the position of the support member and the brake wheel is converted by using an adjusting disk, thereby producing a mobile foundation for the space cabin room body. That is, by using the support assembly, two different effects can be produced on the space cabin room body under switching between two different states, effectively reducing the dependence of the space cabin room body on the lifting equipment when moving.

[0021] On the basis of the setting of the support assembly, in order to reduce the state transition between the two states caused by non-adjustment force, the support member is divided into a support rod and a support sleeve, wherein the extension length of the support rod into the interior of the support sleeve is greater than its own height. Therefore, in the process of the support sleeve extending upward along the support column, the adjustment disk is gradually wrapped in the support sleeve. As a result, when in the supported state, the adjustment disk cannot be rotated by external force.

[0022] Based on the fact that the support assembly can switch between two action states, a slot is provided at one end of the support sleeve, and the position of the slot is adapted to the width of the connecting block between the wheel body and the abutment column. Therefore, the support sleeve will extend upward, and the position of the connecting plate will be limited by the slot. Based on the connection between the connecting plate and the wheel body, the wheel body will not be able to produce relative position changes even if it is subjected to an action force, thereby further limiting the active force for switching between the two states, reducing the unexpected adjustments caused by the non-active force, and enhancing the controllability of the support assembly and the stability of the space cabin body. BRIEF DESCRIPTION OF THE DRAWINGS

[0023] Figure 1 This is a schematic diagram of the overall structure of a movable space cabin for hotel accommodation in the present invention in a supporting state;

[0024] Figure 2 This is a schematic diagram of the overall structure of a movable space cabin for hotel accommodation in the present invention in a moving state;

[0025] Figure 3 This is a schematic diagram of the structural decomposition of a supporting assembly of a movable space cabin for hotel accommodation according to the present invention;

[0026] Figure 4 for Figure 3 Structural diagram of A in the middle

[0027] Figure 5 This is a schematic diagram of the supporting structure of a movable space cabin for hotel accommodation according to the present invention;

[0028] Figure 6The present invention is a schematic diagram of the conversion of the sleeve connection state and the hook connection state of the support parts of a movable space cabin room for hotel accommodation.

[0029] In the figure: 1. Space capsule body; 2. Support assembly; 3. Abutment column; 4. Adjustment member; 41. Adjustment disk; 42. Brake wheel; 421. Wheel body; 422. Connecting block; 43. Support member; 44. Support rod; 45. Support sleeve; 46. Boss; 47. Hooking member; 471. Clamping end; 472. Compression spring; 473. Cone; 48. Port; 5. Lifting member; 51. Lifting end; 52. Support end. DETAILED DESCRIPTION

[0030] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0031] See also Figure 1-Figure 6 The specific problem addressed by the solution provided by the embodiment of the present invention is based on a space capsule disclosed in the utility model with the authorization announcement number CN206653979U. In the application process, the space capsule is installed or moved by hoisting, which is too expensive and easy to cause damage to the space capsule. There are technical problems such as the inability to conveniently and quickly transfer the space capsule and ensure the stability of the space capsule before and after the transfer. Based on the current situation that the movement of existing space capsules is completely dependent on lifting equipment, this solution describes a movable space capsule room for hotel accommodation, which is provided with a support assembly 2, which produces two state conversions for the space capsule room body 1. When the space capsule room body 1 is located at a preset stop position, the support assembly 2 produces a temporary supporting effect on the space capsule room body 1, assisting the space capsule room body 1 to maintain a stable state. When the space capsule room needs to be adjusted to a next position, the adjustment disk 41 is used to convert the positions of the support member 43 and the brake wheel 42, thereby generating a moving foundation for the space capsule room body 1. That is, by using the support assembly 2, two different effects on the space capsule room body 1 can be generated under the switching of two different states, effectively reducing the dependence of the space capsule room body 1 on the lifting equipment when moving.

[0032] A movable space cabin room for hotel accommodation is described, in which a support assembly 2 is specifically arranged on the basis of a space cabin room body 1, and two groups of support components 2 are symmetrically installed at the lower end of the space cabin room body 1, and a lifting member 5 is arranged at the installation position offset from the support assembly 2. First, the lifting member 5 provides a supporting force to the space cabin room body 1 and lifts it to adjust its height, thereby reducing the pressure of the space cabin room body 1 on the support assembly 2, enabling the support assembly 2 to generate a state conversion space under the support of the lifting member 5, and then the support assembly 2 is converted from a supporting state to a pushable movable state.

[0033] In order to reduce the reliance of the space cabin body 1 on the lifting equipment when the position needs to be changed, on the basis of the space cabin body 1 establishing the living space and producing the carried furniture, the support assembly 2 is installed at the lower end of the space cabin body 1 for providing stable support for the space cabin in a single position and assisting the movement during the position change. The support assembly 2 includes an abutment column 3 installed at the lower end of the space cabin body 1, and an adjustment member 4 for converting the support and moving state is arranged at the lower end of the abutment column 3. The adjustment member 4 is arranged in an L-shape and connected to the abutment column 3. The adjustment member 4 includes an adjustment disk 41 rotatably connected to the abutment column 3, and a brake is installed on the adjustment to assist the movement of the space cabin body 1. Wheel 42, and an adjustment disk 41 offset from the installation position of the brake wheel 42 is provided with a support member 43 for assisting the space cabin body 1 to be stabilized on a preset placement surface. The support member 43 is composed of a support rod 44 and a support sleeve 45. The support sleeve 45 is used to stabilize the single mode switching. A cavity for accommodating the support rod 44 is opened inside the support sleeve 45, and a boss 46 is provided on the bottom plate of the inner cavity. An inner groove for accommodating the boss 46 is installed on the support rod 44. The width of the port 48 of the cavity is greater than its internal width. The extension depth of the support rod 44 into the support sleeve 45 is greater than the height of the support rod 44 itself, and a hook 47 for interacting with the inner wall of the support sleeve 45 is installed on the side wall of the support rod 44. The hooking member 47 includes a clamping end 471 disposed in the inner groove, and the clamping end 471 is symmetrically disposed in the inner wall of the support rod 44 with the inner groove axis as the symmetry center line. Two frustums 473 with different diameters are installed on the convex column 46, and the diameter of the frustum 473 at the lower end is smaller than that of the frustum 473 at the upper end. The support rod 44 structure is provided with a receiving groove connected to the inner groove, and the receiving groove is vertically arranged with the inner groove. The clamping end 471 extends outward or retracts in the receiving groove, and a compression spring 472 connected to the groove wall of the receiving groove is installed on the free end of the clamping end 471 that moves in the receiving groove. The end surface of the clamping end 471 connected to the frustum 473 is triangular, and its inclination angle is adapted to the inclination of the side wall of the frustum 473.When in the supporting state, the brake wheel 42 and the abutment column 3 are at an angle of ninety degrees, and the support rod 44 and the support sleeve 45 are in contact with the ground. Then, during the extension of the support rod 44 into the interior of the support platform, the clamping end 471 first gradually moves downward along the inclined surfaces of the two cones 473. Under the pressure of the space cabin body 1, the support rod 44 is always located inside the support sleeve 45 and has an existing connection depth. Then, when it is necessary to change from the supporting state to the moving state, the lifting member 5 is used to lift the space cabin body 1 upward. During the lifting process of the space cabin body 1, the abutment column 3 lifts the space cabin body 1, and then the support rod 44 is generated in the support sleeve The withdrawal action in 45, the abutment moves upward along the cone 473 at the lower end and gradually connects with the cone 473 at the upper end. The diameter difference between the two cones 473 causes the movement of the abutment column 3 to stagnate. After the abutment column 3 is blocked by the bottom structure of the cone 473 at the upper end, the withdrawal action stops and the support sleeve 45 moves upward synchronously. At this time, the adjusting disk 41 is manually rotated 90 degrees to make the brake wheel 42 located at the lower end of the abutment column 3, and the support member 43 at this time is 90 degrees with the abutment column 3. Therefore, when the lifting member 5 moves downward and returns to the initial state, the brake wheel 42 is connected to the bottom surface. At this time, the space cabin body 1 can be pushed to move.

[0034] In order to maintain the stability of the adjusting member 4 in a single state, the brake wheel 42 includes a wheel body 421 and a connecting block 422 arranged between the wheel body 421 and the abutment column 3. The connecting block 422 extends the connection point between the wheel body 421 and the abutment column 3. A port 48 is opened at one end of the support sleeve 45. The width of the port 48 is equal to the width of the connecting block 422, and the opening length of the port 48 on the support sleeve 45 is equal to the diameter of the brake disc. Therefore, on the basis of the upward extension of the support sleeve 45, the position of the connecting plate is limited by the notch, and based on the connection plate and the wheel body 42 1, so that the wheel body 421 cannot produce relative position change even if it is subjected to the force, thereby further limiting the active force for switching between the two states, reducing the unexpected adjustment caused by the non-active force, enhancing the controllability of the support assembly 2 and the stability of the space cabin body 1, and the extension length of the support rod 44 into the support sleeve 45 is greater than its own height. Therefore, in the process of the support sleeve 45 extending upward along the support column, the adjustment disk 41 is gradually wrapped in the support sleeve 45. As a result, when in the supported state, the adjustment disk 41 cannot be rotated by external force.

[0035] The lifting member 5 is arranged at the lower end of the space cabin body 1 in a displaced manner from the supporting assembly 2, and is used to support the space cabin body 1 to adjust its own height to establish a space for the adjusting member 4 to change the function conversion of the space cabin body 1. The lifting member 5 includes a lifting end 51 and a supporting end 52, and the lifting end 51 retracts or extends outwards in the supporting end 52. The supporting end 52 and the supporting sleeve 45 are both provided with connecting ends. The supporting ends 52 on both sides are rotated toward the center line of the space cabin body 1 after the adjusting disk 41 is manually rotated, and then the supporting end 52 and the supporting sleeve 45 are connected through the connecting end by a cable or a rope to enhance the smoothness during the movement. The connecting end of the supporting sleeve 45 is installed at its bottom. The effect of the lifting member 5 in this scheme is to push up the space cabin body 1 or drive the space cabin body 1 to lower its height. Therefore, the cylinder in the existing performance machinery can be used to achieve the above required effect.

[0036] The control method of the electrical components appearing in this article is to automatically control through a controller. The control circuit of the controller can be implemented by simple programming by technicians in this field. The provision of power is also common knowledge in this field. The present invention is mainly used to protect mechanical devices, so the present invention will no longer explain the control method and circuit connection in detail.

[0037] It should be noted that, in this article, relational terms such as first and second, etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device.

[0038] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A movable space cabin room for hotel accommodation, characterized in that: include: The space cabin body (1) establishes the living space and forms the basis for the furniture; A support assembly (2) is installed at the lower end of the space cabin body (1) and is provided with two groups symmetrically in front and back, and is used to generate stable support for the space cabin at a single position and assist movement during position conversion. The support assembly (2) includes an abutment column (3) installed at the lower end of the space cabin body (1), and an adjustment member (4) for converting the support and movement state is provided at the lower end of the abutment column (3); A lifting member (5) is arranged at the lower end of the space cabin body (1) in a manner offset from the supporting assembly (2); The lifting member (5) is used to support the space cabin body (1) to adjust its own height and to establish the adjustment member (4) to change the space for functional conversion of the space cabin body (1).

2. The movable space cabin room for hotel accommodation according to claim 1, characterized in that: The adjusting member (4) comprises an adjusting plate (41) rotatably connected to the abutting column (3), a brake wheel (42) for assisting the movement of the space cabin body (1) being installed on the adjusting plate, and a supporting member (43) for assisting the space cabin body (1) to be stabilized on a preset placement surface being arranged on the adjusting plate (41) offset from the installation position of the brake wheel (42); The support member (43) is composed of a support rod (44) and a support sleeve (45). A cavity for accommodating the support rod (44) is provided inside the support sleeve (45). A convex column (46) is provided on the bottom plate of the inner cavity. An inner groove for accommodating the convex column (46) is installed on the support rod (44). The width of the port (48) of the cavity is greater than the inner width thereof. The extension depth of the support rod (44) into the support sleeve (45) is greater than the height of the support rod (44) itself. A hooking member (47) for interacting with the inner wall of the support sleeve (45) is installed on the side wall of the support rod (44).

3. The movable space cabin room for hotel accommodation according to claim 2, characterized in that: The brake wheel (42) comprises a wheel body (421) and a connecting block (422) arranged between the wheel body (421) and the abutting column (3), wherein the connecting block (422) extends the connection point between the wheel body (421) and the abutting column (3); A port (48) is provided at one end of the support sleeve (45), the width of the port (48) is equal to the width of the connection block (422), and the length of the port (48) on the support sleeve (45) is equal to the diameter of the brake disc.

4. The movable space cabin room for hotel accommodation according to claim 2, characterized in that: The hooking member (47) includes a clamping end (471) arranged in the inner groove, and the clamping end (471) is symmetrically arranged in the inner wall of the support rod (44) with the axis of the inner groove as the symmetry center line. Two frustums (473) with different diameters are installed on the convex column (46) in upper and lower mirror symmetry.

5. The movable space cabin room for hotel accommodation according to claim 4, characterized in that: The support rod (44) structure is provided with a receiving groove connected to the inner groove, the clamping end (471) extends outward or retracts in the receiving groove, and a compression spring (472) connected to the wall of the receiving groove is installed on the free end of the clamping end (471) that moves in the receiving groove.

6. The movable space cabin room for hotel accommodation according to claim 1, characterized in that: The lifting member (5) comprises a lifting end (51) and a supporting end (52), wherein the lifting end (51) is retracted inside the supporting end (52) or extends outwardly, and connecting ends are provided on the supporting end (52) and the supporting sleeve (45), and the connecting end provided on the supporting sleeve (45) is installed at the bottom thereof.

7. The movable space cabin room for hotel accommodation according to claim 5, characterized in that: The end surface where the clamping end (471) connects to the frustum (473) is triangular in shape, and its inclination angle is adapted to the inclination of the side wall of the frustum (473).

8. The movable space cabin room for hotel accommodation according to claim 3, characterized in that: The installation position of the brake wheel (42) on the adjustment disk (41) forms an angle of ninety degrees with the support member (43).

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