阅读说明：本技术 一种自控飞机教学设备 (Self-control airplane teaching equipment ) 是由 富阳 李勇 李永亮 崔伟全 黄育杏 林婷 刘艳华 吴阳 许金超 张娟 褚钟锴 于 2021-06-18 设计创作，主要内容包括：本发明公开了一种自控飞机教学设备,包括主控模块、基座、升降机构、支撑机构以及至少一个座舱,所述升降机构分别与所述基座以及所述座舱连接,所述主控模块与所述升降机构电性连接以能够控制所述升降机构驱使所述座舱上升或者下降,所述支撑机构与所述座舱连接以能够承托所述座舱。其中,支撑机构能够承托座舱,提高维护检修过程的安全性,同时给操作人员进行维护检修带来便利。(The invention discloses self-control aircraft teaching equipment which comprises a main control module, a base, a lifting mechanism, a supporting mechanism and at least one cabin, wherein the lifting mechanism is respectively connected with the base and the cabin, the main control module is electrically connected with the lifting mechanism so as to control the lifting mechanism to drive the cabin to ascend or descend, and the supporting mechanism is connected with the cabin so as to support the cabin. Wherein, supporting mechanism can bearing passenger cabin, improves the security of maintaining the maintenance and overhaul process, and it brings the facility to maintain to overhaul for operating personnel simultaneously.)

1. The self-control aircraft teaching device is characterized by comprising a main control module (1), a base (2), a lifting mechanism (3), a supporting mechanism (4) and at least one cabin (5), wherein the lifting mechanism (3) is respectively connected with the base (2) and the cabin (5), the main control module (1) is electrically connected with the lifting mechanism (3) to control the lifting mechanism (3) to drive the cabin (5) to ascend or descend, and the supporting mechanism (4) is connected with the cabin (5) to support the cabin (5).

2. An autonomous aircraft teaching device as claimed in claim 1 wherein: the supporting mechanism (4) comprises a movable supporting component (41), the movable supporting component (41) is connected with the capsule (5), and the movable supporting component (41) can extend or contract to hold the capsules (5) at different heights.

3. An autonomous aircraft teaching device as claimed in claim 2 wherein: the movable supporting assembly (41) comprises a telescopic loop bar (411) and a supporting base (412), one end of the telescopic loop bar (411) is connected with the bottom of the cabin (5) in a detachable mode through a magnetic attraction structure (6), the other end of the telescopic loop bar (411) is connected with the supporting base (412), the supporting base (412) can move, and the telescopic loop bar (411) can extend or retract.

4. An autonomous aircraft teaching device as claimed in claim 3 wherein: the magnetic attraction structure (6) comprises a first magnetic block (61) and a second magnetic block (62), the first magnetic block (61) is arranged at the bottom of the cabin (5), the second magnetic block (62) is arranged at one end, deviating from the supporting base (412), of the telescopic sleeve rod (411), and the first magnetic block (61) can be attracted with the second magnetic block (62).

5. An autonomous aircraft teaching device as claimed in claim 3 wherein: flexible loop bar (411) include first sleeve pipe (4111) and second sleeve pipe (4112) at least, first sleeve pipe (4111) with second sleeve pipe (4112) cup joints each other, first sleeve pipe (4111) with be provided with between second sleeve pipe (4112) locating part (4113), locating part (4113) can limit first sleeve pipe (4111) with second sleeve pipe (4112) separation.

6. An autonomous aircraft teaching device as claimed in claim 3 wherein: the bottom of the supporting base (412) is provided with a plurality of universal wheels (4121), and the universal wheels (4121) can drive the supporting base (412) to move.

7. An autonomous aircraft teaching device as claimed in claim 2 wherein: the lifting mechanism (3) comprises a driving part (31) and a swinging arm (32), the main control module (1) is electrically connected with the driving part (31), one end of the swinging arm (32) is rotatably connected with the base (2), the other end of the swinging arm (32) is connected with the cabin (5), the driving part (31) is connected with the swinging arm (32) to drive the swinging arm (32) to swing, the supporting mechanism (4) further comprises an auxiliary supporting part (42), and the auxiliary supporting part (42) is connected with the swinging arm (32) to support the swinging arm (32).

8. An autonomous aircraft teaching device as claimed in claim 7 wherein: the auxiliary support (42) is flexible, the auxiliary support (42) can be wound on the swing arm (32), and the auxiliary support (42) can be stretched from the swing arm (32) by applying force to the auxiliary support (42) to form a supporting structure.

9. An autonomous aircraft teaching device as claimed in claim 1 wherein: the cabin (5) is provided with a sensing component (51), and the main control module (1) is electrically connected with the sensing component (51) so that the sensing component (51) can detect the height above the ground of the cabin (5).

Technical Field

The invention relates to the field of amusement equipment, in particular to self-control airplane teaching equipment.

Background

As a common amusement device, an autonomous aircraft generally comprises a base and a plurality of cabins connected to the base, wherein the base can rotate around a central shaft, and the cabins can freely lift and lower relative to the base.

The automatic control aircraft teaching equipment is a model manufactured by reducing an automatic control aircraft according to a certain proportion, and generally comprises a base, a lifting mechanism, a rotating mechanism and a plurality of cabins, wherein the base is respectively connected with each cabin through the lifting mechanism, and the rotating mechanism is arranged on the base. The operator needs to maintain the self-control aircraft teaching equipment at ordinary times, wherein when the cockpit is maintained, the cockpit needs to be additionally supported by the aid of the supporting device so as to perform related maintenance operation, but the operator may lack the supporting device when maintaining the self-control aircraft teaching equipment, which brings inconvenience to maintenance.

Disclosure of Invention

The invention aims to solve one of the prior technical problems, and therefore the invention provides the self-control airplane teaching equipment, the supporting mechanism can support a cockpit, the safety of the maintenance and repair process is improved, and meanwhile, convenience is brought to maintenance and repair of operators.

The self-control aircraft teaching device comprises a main control module, a base, a lifting mechanism, a supporting mechanism and at least one cabin, wherein the lifting mechanism is respectively connected with the base and the cabin, the main control module is electrically connected with the lifting mechanism so as to control the lifting mechanism to drive the cabin to ascend or descend, and the supporting mechanism is connected with the cabin so as to support the cabin.

The self-control airplane teaching equipment at least has the following beneficial effects:

according to the self-control aircraft teaching equipment, when an operator maintains and overhauls the self-control aircraft teaching equipment, the supporting mechanism can support the cabin, the operator can contact parts on the cabin in the maintenance and overhaul process, even if the operator contacts the parts to cause the connection part of the lifting mechanism and the cabin to be loosened, the supporting mechanism can prevent the cabin from falling off, and the safety of the operator in the maintenance and overhaul process is improved. Meanwhile, because the self-control aircraft teaching equipment comprises the supporting mechanism, an operator can use the supporting mechanism at any time in the maintenance and repair process without an external supporting device, and convenience is brought to maintenance and repair.

According to some embodiments of the invention, the support mechanism comprises a movable support member connected to the pods, the movable support member being capable of extension or retraction to hold the pods at different heights.

According to some embodiments of the invention, the movable support assembly comprises a telescopic loop bar and a support base, one end of the telescopic loop bar is detachably connected with the bottom of the cabin through a magnetic attraction structure, the other end of the telescopic loop bar is connected with the support base, the support base can move, and the telescopic loop bar can extend or retract.

According to some embodiments of the invention, the magnetic attraction structure comprises a first magnetic block and a second magnetic block, the first magnetic block is arranged at the bottom of the cabin, the second magnetic block is arranged at one end of the telescopic sleeve rod, which is far away from the supporting base, and the first magnetic block can be attracted with the second magnetic block.

According to some embodiments of the present invention, the telescopic rod includes at least a first sleeve and a second sleeve, the first sleeve and the second sleeve are sleeved with each other, a limiting member is disposed between the first sleeve and the second sleeve, and the limiting member can limit the first sleeve from separating from the second sleeve.

According to some embodiments of the invention, the bottom of the support base is provided with a plurality of universal wheels, and the universal wheels can drive the support base to move.

According to some embodiments of the present invention, the lifting mechanism includes a driving part and a swing arm, the main control module is electrically connected to the driving part, one end of the swing arm is pivotally connected to the base, the other end of the swing arm is connected to the cabin, the driving part is connected to the swing arm so as to be able to drive the swing arm to swing, and the supporting mechanism further includes an auxiliary support connected to the swing arm so as to be able to support the swing arm.

According to some embodiments of the invention, the auxiliary support is flexible, the auxiliary support is capable of being wound around the swing arm, and applying a force to the auxiliary support enables the auxiliary support to extend from the swing arm to form a support structure.

According to some embodiments of the invention, the cabin is provided with a sensing unit, and the main control module is electrically connected with the sensing unit so that the sensing unit can detect the height above the ground of the cabin.

Additional aspects and advantages of the invention will be set forth in part in the description which follows and, in part, will be obvious from the description, or may be learned by practice of the invention.

Drawings

The above and/or additional aspects and advantages of the present invention will become apparent and readily appreciated from the following description of the embodiments, taken in conjunction with the accompanying drawings of which:

FIG. 1 is a block diagram of the self-controlled aircraft teaching apparatus of the present invention;

FIG. 2 is another block diagram of the autonomous aircraft teaching apparatus of the present invention;

FIG. 3 is a cross-sectional view of the autonomous aircraft teaching apparatus of the present invention;

FIG. 4 is a block diagram of the movable support assembly;

FIG. 5 is a block diagram of the autonomous aircraft teaching apparatus of the present invention.

Reference numerals:

the main control module 1, the base 2, the accommodating cavity 21, the lifting mechanism 3, the driving part 31, the swing arm 32, the supporting mechanism 4, the movable supporting component 41, the telescopic rod 411, the first sleeve 4111, the second sleeve 4112, the limiting part 4113, the supporting base 412, the universal wheel 4121, the auxiliary supporting part 42, the cabin 5, the sensing part 51, the magnetic attraction structure 6, the first magnetic block 61, the second magnetic block 62, and the rotating mechanism 7.

Detailed Description

Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the accompanying drawings are illustrative only for the purpose of explaining the present invention, and are not to be construed as limiting the present invention.

In the description of the present invention, it is to be understood that directional descriptions, such as the terms "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc., refer to the directional or positional relationships illustrated in the drawings, and are intended to facilitate the description of the invention and to simplify the description, but do not indicate or imply that the elements referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the invention.

In the description of the present invention, the meaning of a plurality of means is one or more, the meaning of a plurality of means is two or more, and larger, smaller, larger, etc. are understood as excluding the number, and larger, smaller, inner, etc. are understood as including the number. If the first and second are described for the purpose of distinguishing technical features, they are not to be understood as indicating or implying relative importance or implicitly indicating the number of technical features indicated or implicitly indicating the precedence of the technical features indicated.

In the description of the present invention, it should be noted that unless otherwise explicitly stated or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.

In the description herein, references to the description of the term "one embodiment," "some embodiments," "an illustrative embodiment," "an example," "a specific example," or "some examples" or the like mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.

The self-control aircraft teaching device according to the present invention, as shown in fig. 1-5, comprises a main control module 1, a base 2, a lifting mechanism 3, a support mechanism 4 and at least one cockpit 5, wherein the lifting mechanism 3 is respectively connected with the base 2 and the cockpit 5, the main control module 1 is electrically connected with the lifting mechanism 3 to control the lifting mechanism 3 to drive the cockpit 5 to ascend or descend, and the support mechanism 4 is connected with the cockpit 5 to support the cockpit 5.

According to the self-control aircraft teaching equipment, when an operator maintains and overhauls the self-control aircraft teaching equipment, the supporting mechanism 4 can support the cabin 5, the operator can contact parts on the cabin 5 in the maintenance and overhauling process, even if the operator contacts the parts to cause the connection part of the lifting mechanism 3 and the cabin 5 to be loosened, the supporting mechanism 4 can prevent the cabin 5 from falling off, and the safety of the operator in the maintenance and overhauling process is improved. Meanwhile, because the self-control aircraft teaching equipment comprises the supporting mechanism 4, an operator can use the supporting mechanism 4 at any time in the maintenance and repair process without an external supporting device, and convenience is brought to maintenance and repair.

Specifically, the main control module 1 may include a PLC control chip, and may also include an MCU micro-processing unit. The shape of the base 2 may be a rectangular parallelepiped, a cylinder, or another shape. In addition, since the support mechanism 4 is in contact with the cabin 5 on one hand and the floor on the other hand when supporting the cabin 5, the support mechanism 4 can provide a supporting force to the cabin 5 and prevent the cabin 5 from falling off due to the action of gravity during maintenance and inspection.

In some embodiments of the invention, as shown in figures 1-3, the support mechanism 4 comprises a movable support member 41, the movable support member 41 being connected to the capsule 5, the movable support member 41 being capable of extension or retraction to hold capsules 5 at different heights.

In particular, the movable support assembly 41 generally has a plurality of use configurations, and since the lifting mechanism 3 can drive the cabin 5 to ascend or descend, the operator can adjust the movable support assembly 41 to adapt to the height of the cabin 5 from the ground during maintenance and inspection.

In some embodiments of the present invention, as shown in fig. 4, the movable supporting assembly 41 includes a telescopic rod 411 and a supporting base 412, one end of the telescopic rod 411 is detachably connected to the bottom of the cabin 5 through the magnetic attraction structure 6, the other end of the telescopic rod 411 is connected to the supporting base 412, the supporting base 412 can move, and the telescopic rod 411 can extend or retract.

Specifically, the magnetic attraction structure 6 is simple in structure and convenient to use. The telescopic rods 411 can be extended or retracted so that the movable support assembly 41 can support the cabins 5 at different heights for the operator to operate. Support base 412 is movable so that an operator does not have to expend manpower or material resources moving support base 412. When the self-control aircraft teaching equipment needs to be maintained and overhauled, an operator can move the supporting base 412 to the position below the cabin 5, then adjust the telescopic degree of the telescopic loop bar 411, and then connect the telescopic loop bar 411 with the bottom of the cabin 5 by using the magnetic attraction structure 6, so that the operator can start to maintain and overhaul the self-control aircraft teaching equipment after the operation is completed; after the maintenance and overhaul of the self-control airplane teaching equipment are completed by an operator, the operator can overcome the magnetic force of the magnetic attraction structure 6 to detach the telescopic loop bar 411 from the cabin 5, and then the operator can remove the support base 412 after properly adjusting the telescopic loop bar 411.

In some embodiments of the present invention, as shown in fig. 1 to 4, the magnetic attraction structure 6 includes a first magnetic block 61 and a second magnetic block 62, the first magnetic block 61 is disposed at the bottom of the cabin 5, the second magnetic block 62 is disposed at an end of the telescopic bar 411 away from the supporting base 412, and the first magnetic block 61 can attract the second magnetic block 62.

Specifically, the first magnetic block 61 is generally the same size as the second magnetic block 62. When the self-control airplane teaching equipment is in a maintenance and overhaul state, the first magnetic block 61 and the second magnetic block 62 are attracted; when the self-control aircraft teaching equipment is not in a maintenance and overhaul state, the first magnetic block 61 is not attracted with the second magnetic block 62.

In some embodiments of the present invention, as shown in fig. 4, the telescopic rod 411 at least includes a first sleeve 4111 and a second sleeve 4112, the first sleeve 4111 and the second sleeve 4112 are sleeved with each other, a limiting member 4113 is disposed between the first sleeve 4111 and the second sleeve 4112, and the limiting member 4113 can limit the first sleeve 4111 and the second sleeve 4112 from separating.

Specifically, the outer diameter of the first sleeve 4111 is generally smaller than the inner diameter of the second sleeve 4112, and when an operator needs to adjust the telescopic rod 411 to make the telescopic rod 411 become long, the first sleeve 411 may be extended from the second sleeve 4112; when the operator needs to adjust the telescopic rod 411 so that the telescopic rod 411 becomes shorter, the first sleeve 411 can be retracted into the second sleeve 4112. And locating part 4113 can make first sleeve 4111 and second sleeve 4112 keep cup jointing, and locating part 4113 has also defined the maximum length of telescopic stem 411, and when first sleeve 4111 has a tendency to separate from second sleeve 4112, locating part 4113 can contact first sleeve 4111 to limit separation of first sleeve 4111 from second sleeve 4112.

In some embodiments of the present invention, as shown in fig. 3, a plurality of universal wheels 4121 are disposed at the bottom of the supporting base 412, and the universal wheels 4121 can drive the supporting base 412 to move.

Specifically, in an embodiment of the present invention, the bottom of the supporting base 412 is provided with a plurality of receiving grooves, the number of the receiving grooves is the same as the number of the universal wheels 4121, and the plurality of receiving grooves and the plurality of universal wheels 4121 are arranged in a one-to-one correspondence manner, when the supporting base 412 does not need to be moved, each universal wheel 4121 can be received in the receiving groove corresponding thereto, and when the supporting base 412 needs to be moved, each universal wheel 4121 can extend out from the receiving groove corresponding thereto. In another embodiment of the present invention, the universal wheel 4121 is provided with a locking member movably disposed on the universal wheel 4121, and when the support base 412 does not need to be moved, the operator can contact the locking member with the universal wheel 4121 to limit the rotation of the universal wheel 4121, and when the support base 412 needs to be moved, the operator can disengage the locking member from the universal wheel 4121, so that the universal wheel 4121 can be automatically rotated.

In some embodiments of the present invention, as shown in fig. 3, the lifting mechanism 3 includes a driving part 31 and a swing arm 32, the main control module 1 is electrically connected to the driving part 31, one end of the swing arm 32 is pivotally connected to the base 2, the other end of the swing arm 32 is connected to the cabin 5, the driving part 31 is connected to the swing arm 32 to enable the swing arm 32 to swing, and the supporting mechanism 4 further includes an auxiliary support 42, and the auxiliary support 42 is connected to the swing arm 32 to enable the auxiliary support 42 to support the swing arm 32.

Specifically, the driving member 31 is generally an air cylinder, and in an embodiment of the present invention, the base 2 is provided with the cavity 21, and the driving member 31 is disposed in the cavity 21, which can protect the driving member 31, reduce the probability of accidental damage to the driving member 31, and save space.

In some embodiments of the present invention, as shown in fig. 1-2, the auxiliary support 42 is flexible, the auxiliary support 42 can be wound around the swing arm 32, and applying a force to the auxiliary support 42 can enable the auxiliary support 42 to extend from the swing arm 32 to form a support structure.

Specifically, the property that an object is deformed by force and the object cannot be restored after the force is lost is called flexibility. The material of the auxiliary support member 42 may be polyether polyol, or may be other flexible materials. When it is desired to support the swing arm 32 using the auxiliary support 42, an operator may apply force to the auxiliary support 42 or use a tool to extend the auxiliary support 42 from the swing arm 32 to form a support structure to support the swing arm 32; when it is not necessary to support the swing arm 32 using the auxiliary support 42, the operator may apply force to the auxiliary support 42 or use a tool to wrap the auxiliary support 42 around the swing arm 32. It should be noted that wrapping the auxiliary support 42 around the swing arm 32 does not interfere with the normal swinging motion of the swing arm 32 during operation.

In some embodiments of the present invention, as shown in fig. 1 to 5, a sensing unit 51 is disposed on the cabin 5, and the main control module 1 is electrically connected to the sensing unit 51 so that the sensing unit 51 can detect the height of the cabin 5 from the ground.

Specifically, when supporting the cabin 5 with the supporting mechanism 4, the height from the ground of the cabin 5 may exceed the adjustment range of the supporting mechanism 4, and after obtaining the detected height from the ground of the cabin 5, the operator can judge whether the height from the ground of the cabin 5 exceeds the adjustment range of the supporting mechanism 4 with the naked eye, and if the operator judges that the height from the ground of the cabin 5 exceeds the adjustment range of the supporting mechanism 4, the operator can control the lifting mechanism 3 to drive the cabin 5 to descend by a certain height through the main control module 1, and then adjust the supporting mechanism 4 to support the cabin 5.

In some embodiments of the present invention, as shown in fig. 1, the present invention further includes a rotating mechanism 7, the rotating mechanism 7 is connected to the base 2, and the main control module 1 is electrically connected to the rotating mechanism 7 to control the rotating mechanism 7 to drive the base 2 to rotate.

While embodiments of the invention have been shown and described, it will be understood by those of ordinary skill in the art that: various changes, modifications, substitutions and alterations can be made to the embodiments without departing from the principles and spirit of the invention, the scope of which is defined by the claims and their equivalents.