Airplane and automobile arm folding mechanism
By designing an arm folding mechanism with fixed seat, storage seat, dual-axis motor and other components, the problem of cumbersome storage of the arm when flying cars are driving on land is solved, the automatic folding and extension of the arm is realized, and the convenience of use is improved sex.
Patent Information
- Application Number
- CN202421441939.7
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-06-24
- Publication Date
- 2025-02-14
- Estimated Expiration
- 2034-06-24
AI Technical Summary
Existing flying cars need to manually separate and store the arm when driving on land, resulting in cumbersome use.
An airplane and automobile arm folding mechanism is designed, and the automatic folding and extension of the arm is achieved through the combination of a fixed seat, a storage seat, a dual-axis motor, a threaded rod, a sleeve plate, a connecting rod and a T-block.
It realizes automatic folding and stretching of the arm throughout the process, saving time and effort, and improving the convenience of use.
Smart Images

Figure CN222474433U_ABST
Abstract
Description
Technical Field
[0001] The utility model belongs to the field of aircraft automobile machine arms, in particular to an aircraft automobile machine arm folding mechanism. Background Art
[0002] A flying car is a means of transportation that combines the features of a car and an airplane, being able to travel on land and fly in the air. This type of transportation is designed to solve problems such as urban traffic congestion and long-distance commuting, providing a faster and more convenient way to travel.
[0003] According to patent application number 202111283097.8, a flying car is disclosed, including a car body and two rotor devices arranged on the car body, the rotor device including an arm and a rotor mechanism, the arm is rotatably connected to the car body, and the rotor mechanism is installed on the arm, wherein the flying car can switch between a flight mode and a land mode, when the flying car is in the land mode, the two arms are at least retracted relative to the car body, when the flying car is in the flight mode, the two arms are unfolded relative to the car body, and the flying car is in a dual-rotor flying car configuration. The flying car provided by the prior art can take off and land vertically by taking advantage of the rotor, breaking through the limitation of the runway range in the actual use scenario, and has a large load;
[0004] When the flying car of this comparison ratio is driving on land and not using the arms, personnel are required to manually separate the arms from the vehicle body and then store the arms in the storage cavity, thereby increasing the complexity of use.
[0005] In summary, the utility model therefore provides an aircraft vehicle arm folding mechanism to solve the above-mentioned problems. Utility Model Content
[0006] In order to solve the above technical problems, the utility model provides the following technical solutions:
[0007] A machine arm folding mechanism for an airplane automobile comprises a fixing seat, the front and back sides of the fixing seat are fixedly connected to a storage seat, and the fixing seat and the storage seat are both arranged on the top of a vehicle body, an machine arm body is arranged in the inner cavity of the storage seat, blades are arranged on the surface of the machine arm body, a double-axis motor is arranged in the inner cavity of the fixing seat, output shafts at both ends of the double-axis motor are drivingly connected to threaded rods, the surfaces of the threaded rods are threadedly connected to sleeve plates, the front and back sides of the sleeve plates are movably connected to connecting rods via rotating shafts, and the other end of the connecting rod is movably connected to a T-block via the rotating shaft.
[0008] Furthermore, in the utility model, a T-shaped slot is provided on one side of the arm body, and the T-shaped block is located in the inner cavity of the T-shaped slot and is slidably connected to the inner cavity of the T-shaped slot.
[0009] Furthermore, in the utility model, the inner cavity of the storage seat is movably connected to a limit rod via a bearing, and one end of the limit rod away from the storage seat is fixedly connected to the arm body.
[0010] Furthermore, in the utility model, through grooves are provided on the front and back sides of the fixing seat, and the connecting rod passes through the inner cavity of the through groove and is slidably connected to the inner cavity of the through groove.
[0011] Furthermore, in the utility model, a limiting groove is provided at the bottom of the inner cavity of the fixing seat, a limiting block is fixedly connected to the bottom of the sleeve plate, the limiting block is located in the inner cavity of the limiting groove and is slidably connected to the inner cavity of the limiting groove.
[0012] Furthermore, in the utility model, a support plate is fixedly connected to the back of the dual-axis motor, and the other end of the support plate is fixedly connected to the inner wall of the fixing seat, and one end of the threaded rod is movably connected to the inner wall of the fixing seat through a bearing.
[0013] Beneficial effects: The utility model has the following beneficial effects:
[0014] The utility model can store and store the machine arm through the storage seat, and the flight operation of the flying car is facilitated by the machine arm body cooperating with the blades. The threaded rod is driven to rotate by the output shaft of the dual-axis motor. Since the threaded rod and the sleeve plate are in a threaded connection state, the threaded rod drives the sleeve plate to move to one side, and the sleeve plate drives the connecting rod to move to one side. The connecting rod drives the T-block to move, so that the T-block pulls the machine arm body gradually to the storage seat until it enters the interior of the storage seat, thereby realizing the folding and storage of the machine arm body. The folding is fully automated, which saves time and effort and improves convenience during use. BRIEF DESCRIPTION OF THE DRAWINGS
[0015] Figure 1 This is a schematic diagram of the structure of the machine arm body of the utility model in the unfolded state;
[0016] Figure 2 This is a schematic diagram of the structure of the machine arm body of the utility model in a folded and stored state;
[0017] Figure 3 This is a schematic diagram of the structure of the fixed seat of the utility model in a sectional state;
[0018] Figure 4 This utility model Figure 1 Schematic diagram of the local enlarged structure at point A in the middle.
[0019] In the figure:
[0020] 1. Fixed seat; 11. Limiting groove; 12. Through groove; 2. Storage seat; 21. Limiting rod; 3. Arm body; 4. Blade; 5. Dual-axis motor; 6. Threaded rod; 7. Sleeve plate; 71. Limiting block; 8. Connecting rod; 9. T-block; 91. T-slot. DETAILED DESCRIPTION
[0021] In order to better understand the technical content of the utility model, specific embodiments are cited and described as follows in conjunction with the accompanying drawings. In this disclosure, various aspects of the utility model are described with reference to the accompanying drawings, and many illustrative embodiments are shown in the accompanying drawings. The embodiments of the present disclosure are not necessarily defined to include all aspects of the utility model. It should be understood that the various concepts and embodiments introduced above, as well as those described in more detail below, can be implemented in any of many ways, because the concepts and embodiments disclosed in the utility model are not limited to any implementation method. In addition, some aspects disclosed in the utility model can be used alone, or used in any appropriate combination with other aspects disclosed in the utility model.
[0022] Example 1
[0023] like Figure 1-4 As shown, it is the first embodiment of the utility model, which provides an aircraft automobile arm folding mechanism, including a fixing seat 1, the front and back sides of the fixing seat 1 are fixedly connected with a storage seat 2, and the fixing seat 1 and the storage seat 2 are both arranged on the top of the vehicle body, the inner cavity of the storage seat 2 is provided with an arm body 3, the surface of the arm body 3 is provided with blades 4, the inner cavity of the fixing seat 1 is provided with a double-axis motor 5, the output shafts at both ends of the double-axis motor 5 are drivingly connected with a threaded rod 6, the surface of the threaded rod 6 is threadedly connected with a sleeve plate 7, the front and back sides of the sleeve plate 7 are movably connected with a connecting rod 8 through a rotating shaft, and the other end of the connecting rod 8 is movably connected with a T-block 9 through a rotating shaft.
[0024] like Figure 1-4 As shown, the arms can be stored and accommodated through the storage seat 2, and the arm body 3 cooperates with the blades 4 to facilitate the flight operation of the flying car. When the arm body 3 needs to be folded, the dual-axis motor 5 is first operated, and the output shaft of the dual-axis motor 5 drives the threaded rod 6 to rotate. Since the threaded rod 6 and the sleeve plate 7 are in a threaded connection state, the threaded rod 6 drives the sleeve plate 7 to move to one side, and the sleeve plate 7 drives the connecting rod 8 to move to one side. One end of the connecting rod 8 drives the T-block 9 to move, so that the T-block 9 pulls the arm body 3 gradually toward the storage seat 2 until it enters the interior of the storage seat 2, thereby realizing the folding and storage of the arm body 3, and the folding is fully automated, which saves time and effort and improves convenience during use.
[0025] Example 2
[0026] Reference Figure 1 ,2 and 4, which are the second embodiment of the present utility model, and this embodiment is based on the previous embodiment.
[0027] In this embodiment, a T-shaped slot 91 is opened on one side of the arm body 3 , and the T-shaped block 9 is located in the inner cavity of the T-shaped slot 91 and is slidably connected with the inner cavity of the T-shaped slot 91 .
[0028] The inner cavity of the storage seat 2 is movably connected to a limit rod 21 through a bearing, and one end of the limit rod 21 away from the storage seat 2 is fixedly connected to the arm body 3.
[0029] like Figure 1 , 2 As shown in FIG. 4 , the T-block 9 is located in the inner cavity of the T-slot 91, so that the T-block 9 can drive the arm body 3 to move when it moves, and the T-block 9 will slide along the inner cavity trajectory of the T-slot 91 during the movement, so as to achieve a limiting effect. The arm body 3 can be limited and supported by the limiting rod 21, and the arm body 3 can move axially with the limiting rod 21 when it moves.
[0030] Example 3
[0031] Reference Figure 3 , which is the third embodiment of the utility model, and this embodiment is based on the previous two embodiments.
[0032] In this embodiment, through slots 12 are provided on the front and back sides of the fixing seat 1 , and the connecting rod 8 passes through the inner cavity of the through slot 12 and is slidably connected to the inner cavity of the through slot 12 .
[0033] A limiting groove 11 is provided at the bottom of the inner cavity of the fixing seat 1 , and a limiting block 71 is fixedly connected to the bottom of the sleeve plate 7 . The limiting block 71 is located in the inner cavity of the limiting groove 11 and is slidably connected to the inner cavity of the limiting groove 11 .
[0034] A support plate is fixedly connected to the back of the dual-axis motor 5, and the other end of the support plate is fixedly connected to the inner wall of the fixing seat 1, and one end of the threaded rod 6 is movably connected to the inner wall of the fixing seat 1 through a bearing.
[0035] like Figure 3 As shown, the dual-axis motor 5 can be well supported by the support plate to ensure its stability during operation. The connecting rod 8 will move along the inner cavity trajectory of the through groove 12 during movement, thereby ensuring the stability of the connecting rod 8 during movement. At the same time, the sleeve plate 7 will drive the limit block 71 to slide along the inner cavity of the limit groove 11 during movement, thereby preventing the sleeve plate 7 from rotating during movement.
[0036] When in use, firstly, the dual-axis motor 5 is operated, and the output shaft of the dual-axis motor 5 will drive the threaded rod 6 to rotate forward. Since the threaded rod 6 and the sleeve plate 7 are in a threaded connection state, the threaded rod 6 will drive the sleeve plate 7 to move to one side, and the sleeve plate 7 will drive the connecting rod 8 to move to one side. One end of the connecting rod 8 will drive the T-block 9 to move, so that the T-block 9 pulls the arm body 3 gradually close to the storage seat 2 until it enters the interior of the storage seat 2, thereby realizing the folding and storage of the arm body 3. When the arm body 3 needs to be extended, When on display and in use, the output shaft of the dual-axis motor 5 drives the threaded rod 6 to rotate in the opposite direction, the threaded rod 6 will drive the sleeve plate 7 to move to one side, the sleeve plate 7 will drive the connecting rod 8 to move, and the connecting rod 8 drives the T-block 9 to move, and then the T-block 9 will push the arm body 3 to rotate, so that one end of the arm body 3 gradually separates from the interior of the storage seat 2 and extends to the outside, thereby realizing the extension operation of the arm body 3, facilitating the use of the arm body 3, and saving time and effort through full-process automated folding or extension, thereby improving convenience during use.
[0037] The standard parts used in this application document can all be purchased from the market and can be customized according to the description in the specification and drawings. The specific connection methods of each part adopt conventional means such as mature bolts, rivets, welding, etc. in the prior art. The machinery, parts and equipment all adopt conventional models in the prior art. The control method is automatic control through a controller. The control circuit of the controller can be implemented through simple programming by technicians in this field, which is common knowledge in the field. This application is mainly used to protect mechanical devices, so this application no longer explains the control method and circuit connection in detail.
[0038] Although the present invention has been disclosed as above with preferred embodiments, it is not intended to limit the present invention. A person with ordinary knowledge in the technical field to which the present invention belongs may make various changes and modifications without departing from the spirit and scope of the present invention. Therefore, the protection scope of the present invention shall be determined by the definition of the claims.
Claims
1. An aircraft vehicle arm folding mechanism, comprising a fixing seat (1), characterized in that: The front and back sides of the fixing seat (1) are fixedly connected to a storage seat (2), and the fixing seat (1) and the storage seat (2) are both arranged on the top of the vehicle body, the inner cavity of the storage seat (2) is provided with an arm body (3), the surface of the arm body (3) is provided with blades (4), the inner cavity of the fixing seat (1) is provided with a dual-axis motor (5), the output shafts at both ends of the dual-axis motor (5) are both transmission-connected to threaded rods (6), the surface of the threaded rods (6) is threadedly connected to a sleeve plate (7), the front and back sides of the sleeve plate (7) are both movably connected to a connecting rod (8) via a rotating shaft, and the other end of the connecting rod (8) is movably connected to a T-block (9) via a rotating shaft.
2. The aircraft automobile arm folding mechanism as claimed in claim 1, characterized in that: A T-shaped slot (91) is provided on one side of the arm body (3); the T-shaped block (9) is located in the inner cavity of the T-shaped slot (91) and is slidably connected to the inner cavity of the T-shaped slot (91).
3. The aircraft automobile arm folding mechanism as claimed in claim 1, characterized in that: The inner cavity of the storage seat (2) is movably connected to a limit rod (21) via a bearing, and one end of the limit rod (21) away from the storage seat (2) is fixedly connected to the arm body (3).
4. The aircraft automobile arm folding mechanism as claimed in claim 1, characterized in that: The front and back sides of the fixing seat (1) are both provided with through grooves (12), and the connecting rod (8) passes through the inner cavity of the through groove (12) and is slidably connected to the inner cavity of the through groove (12).
5. The aircraft automobile arm folding mechanism as claimed in claim 1, characterized in that: A limiting groove (11) is provided at the bottom of the inner cavity of the fixing seat (1), a limiting block (71) is fixedly connected to the bottom of the sleeve plate (7), and the limiting block (71) is located in the inner cavity of the limiting groove (11) and is slidably connected to the inner cavity of the limiting groove (11).
6. The aircraft automobile arm folding mechanism as claimed in claim 1, characterized in that: A support plate is fixedly connected to the back of the dual-axis motor (5), and the other end of the support plate is fixedly connected to the inner wall of the fixing seat (1), and one end of the threaded rod (6) is movably connected to the inner wall of the fixing seat (1) via a bearing.
Citation Information
Patent Citations
Flying car
CN114043831A