Remote control toy plane with air-drop function
By designing the airdrop cargo warehouse and locking mechanism on the remote-controlled toy aircraft, the problem of single function is solved, and the airdrop function is enhanced, which increases the control fun and reduces flight drag.
Patent Information
- Application Number
- CN202420590203.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-03-26
- Publication Date
- 2024-12-27
- Estimated Expiration
- 2034-03-26
AI Technical Summary
The existing remote control toy aircraft has a single function and lacks the airdrop function to increase the joy of handling.
The airdrop warehouse is designed on the abdomen of the remote-controlled toy aircraft, and the hinge and locking mechanism are used to realize the opening and closing of the hatch door. The opening and closing of the hatch door is controlled by the micro unlocking motor, and the automatic opening and closing of the hatch door is achieved by combining the retracting and retracting and releasing torsion spring is achieved to achieve automatic opening and closing. .
It enhances the fun during flight, realizes airdrop operation, has a simple structure, light weight, reliable function, and effectively reduces flight drag.
Smart Images
Figure CN222238766U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the field of design and manufacture of model aircraft, in particular to a remote-controlled toy aircraft with an airdrop function. Background Art
[0002] There are two main types of traditional toy airplanes: one is a toy airplane without human intervention control, and the other is a toy airplane with human control. Currently, most toy airplanes with human control only have basic flight functions, and this single-function toy airplane greatly reduces the control pleasure of the operator.
[0003] Therefore, in order to increase the interest of the existing remote control toy airplane, some functions can be added on the basis of the existing remote control toy airplane. Utility Model Content
[0004] Aiming at the current situation that the existing remote control toy airplanes have a single function, the utility model provides a remote control toy airplane with an airdrop function, which increases the fun of the toy airplane and improves the flight control interest of the operator.
[0005] The utility model discloses a remote-controlled toy airplane with an airdrop function. An airdrop cabin installation cavity is provided on the belly of an existing toy airplane fuselage, and an airdrop cargo hold is fixedly installed inside the cavity.
[0006] The airdrop cargo hold is a rectangular frame structure having a left frame, a right frame and a top frame, all of which have reinforcing beams arranged at equal intervals between the frame body and the opposite side edges of the frame body in the circumferential direction.
[0007] The bottom surface of the airdrop cargo hold is provided with a left door and a right door, which are respectively hinged to the left and right sides of the airdrop cargo hold. Specifically, the front and rear ends of the bottom edges of the left and right frames are designed with columnar frame joints integrally formed with the cargo hold frame, and an axial hole with the axis along the front-to-back direction is coaxially opened on the frame joints, which cooperate with the door joints designed on the left and right doors, respectively, and are connected through a connecting shaft.
[0008] After the left and right doors are closed, the grooves and bosses designed on the opposite sides of the left and right doors are overlapped and positioned, so that the position of the left door can be limited by the right door; at the same time, the lock hook designed on the right door cooperates with the lock tongue of the locking motor installed in the airdrop cabin to achieve locking after the left and right doors are closed, and maintain the closed state of the left and right doors; and when the left and right doors are closed in place, the outer surfaces of the left and right doors are conformal to the outer surface of the fuselage. The above-mentioned locking motor is fixedly installed on the upper surface of the cargo hold bottom support fixedly installed between the left and right side walls of the airdrop cargo hold.
[0009] The advantages of the utility model are:
[0010] 1. The utility model remote control toy airplane is designed with an airdrop mechanism, which increases the airdrop operation during the flight and enhances the fun of the airplane flight process;
[0011] 2. The utility model remote control toy airplane is provided with an airdrop mechanism, which has a simple structure, light weight and reliable functions;
[0012] 3. In the airdrop mechanism added to the remote-controlled toy airplane of the utility model, the design of the cabin door has an outer surface conforming to the fuselage, which effectively reduces the flight resistance of the airplane. BRIEF DESCRIPTION OF THE DRAWINGS
[0013] Figure 1 This is a schematic diagram of the overall structure of the utility model remote-controlled toy airplane when the airdrop cargo compartment is closed;
[0014] Figure 2 This is a schematic diagram of the overall structure of the utility model remote-controlled toy airplane with its airdrop cargo hold opened;
[0015] Figure 3 This is a schematic diagram of the airdrop cargo compartment in the remote-controlled toy airplane of the utility model in an open state;
[0016] Figure 4 This is a schematic diagram of the state in which the airdrop cargo compartment of the remote-controlled toy airplane of the utility model is closed and locked;
[0017] Figure 5 It is a partial schematic diagram of the installation position of the retractable torsion spring of the cabin door and the installation box of the retractable torsion spring of the remote-controlled toy airplane of the utility model;
[0018] Figure 6 It is a schematic diagram of the fixing method between the retractable torsion spring of the cabin door and the fuselage of the remote-controlled toy airplane of the utility model;
[0019] Figure 7 The utility model is a schematic diagram of the airdrop of a remote-controlled toy airplane.
[0020] In the figure:
[0021] 101a-left door 101b-right door 102-cargo hold bottom support
[0022] 103-Cargo hold frame 104-Frame joint 105-Cargo hold joint
[0023] 106-lock head 106a-inclined surface 106b-locking mating surface
[0024] 107- micro unlocking motor 107a- lock tongue 108- torsion spring installation box
[0025] 109-Retractable torsion spring DETAILED DESCRIPTION
[0026] The utility model is further described in detail below in conjunction with the accompanying drawings.
[0027] The utility model discloses a remote-controlled toy airplane with an airdrop function, which improves the structure of an existing remote-controlled toy airplane and adds an airdrop cargo hold to the existing remote-controlled toy airplane structure to realize the airdrop function of the remote-controlled toy airplane.
[0028] The conventional layout of the existing toy airplane includes a fuselage, wings (including ailerons and flaps), a vertical tail (including a rudder), a horizontal tail (including an elevator), a propulsion device, a signal receiving / control device, a flight controller, a steering gear, a landing gear, etc. Based on the existing toy airplane structure, the present invention reserves a rectangular airdrop cabin installation cavity in the fuselage 2 of the toy airplane for accommodating an airdrop cargo hold 1, such as Figure 1 , Figure 2 shown.
[0029] The airdrop cargo hold 1 is a storage structure for airdropped objects, including a left door 101a, a right door 101b, a cargo hold bottom support 102, a cargo hold frame 103 and a locking mechanism. Figure 3 , Figure 4 shown.
[0030] The cargo hold frame 103 is a rectangular parallelepiped structure, and its size is the same as that of the airdrop cabin installation cavity. The cargo hold frame 103 has a left frame, a right frame and a top frame, and all three have a frame body in the circumferential direction and reinforcing beams arranged at equal intervals between the two opposite sides of the frame body.
[0031] Among them, the front and rear ends of the bottom edges of the left and right frames are designed with columnar frame joints 104 integrally formed with the cargo hold frame 103, and the frame joints 104 are coaxially opened with an axial hole along the front-to-back direction for connecting the left door 101a and the right door 101b.
[0032] At the same time, a cargo hold bottom support 102 is fixedly installed between the bottom edges of the left and right frames. The cargo hold bottom support 102 is also a frame structure, and the left and right ends are respectively fixed to the bottom edges of the left and right frames. The right part of the cargo hold bottom support 102 is designed as a platform structure, and the middle part has a rectangular opening to cooperate with the locking mechanism to achieve the locking of the left door 101a and the right door 101b after closing.
[0033] The left hatch 101a and the right hatch 101b have the same structure, with a flat top surface, a side wall perpendicular to the top surface, and a bottom surface that is an arc surface connected to the side wall and the top surface. The side at the angle between the top surface and the bottom surface is a hinged side, and the front and rear parts of the hinged side are respectively designed with an integrally formed columnar hatch joint 105, and the hatch joint 105 is coaxially opened with an axis hole along the front-to-back direction, which is used for connecting the left hatch 101a, the right hatch 101b and the cargo hold frame 103.
[0034] In the above-mentioned right door 101b, an inwardly recessed rectangular groove 101c is designed at the angle between the top surface and the side surface. The rectangular groove 101c is designed along the front-to-back direction and passes through the front and rear side surfaces of the right door 101a. At the same time, in the left door 101b, a rectangular cross-section boss 101d is designed on the side surface. The boss 101d is designed along the front-to-back direction, and the top surface and the front and rear end surfaces are flush with the top surface and the front and rear side surfaces of the left door 101a, respectively, and the cross-sectional dimensions of the boss 101b are the same as the cross-sectional dimensions of the rectangular groove 101c on the above-mentioned right door 101a.
[0035] The front and rear door joints 104 of the hinged side of the left door 101a of the above structure are respectively coaxially arranged with the front and rear frame joints 105 of the bottom side of the left frame, and the ends are in contact with each other, and the rotation shaft passes through the shaft holes on the two joints in contact with each other, so as to realize the hinged connection between the left door 101a and the left frame. Similarly, the front, middle and rear door joints 104 of the hinged side of the right door 101b are respectively coaxially arranged with the front, middle and rear frame joints 105 of the bottom side of the right frame, and the ends are in contact with each other, and the rotation shaft passes through the shaft holes on the two joints in contact with each other, so as to realize the hinged connection between the right door 101b and the right frame.
[0036] When closing the two doors, the left door 101a and the right door 101b are closed in sequence until the top surface of the right door 101b contacts the bottom surface of the cargo hold bottom support 102 and the boss 101d on the left door 101a is inserted into the rectangular groove 101c on the right door 101b, and the doors are closed. At this time, the locking mechanism is used to lock the left door 101a and the right door 101b.
[0037] The locking mechanism includes a locking hook 106 and a micro unlocking motor 107 .
[0038] The lock hook 106 is an L-shaped hook structure as a whole, one side of which is perpendicular to the top surface of the right door 101b, and the end is fixedly installed on the top surface of the right door 101b, and is located in the middle of the right door 101b near the rectangular groove 101c. The other side of the lock hook 106 is a locking matching side, the top is designed as a locking inclined surface 106a for matching with the lock tongue 107a of the micro unlocking motor 107, and the bottom is a locking matching surface 106b for matching with the lock tongue 107a to achieve locking between the left door 101a and the right door 101b.
[0039] The micro unlocking motor 107 is used to lock the hatch 101 after closing and to open the hatch 101 after unlocking. It is fixedly installed on the left platform of the cargo hold bottom support 102, and the direction of the lock tongue 107a is facing the lock hook 106. When the two hatches are closed, the lock tongue 107a of the micro unlocking motor 107 is controlled to extend so that it contacts the locking mating surface 106b at the top of the lock hook 106, thereby limiting the rotation of the left hatch 101a and the right hatch 101b, thereby achieving the locking of the two hatches after closing.
[0040] The lock tongue (suction-type micro-frame electromagnet) of the above-mentioned micro unlocking motor 107 has a spring mechanism inside the lock tongue 107a, and the lock tongue 107a is in an extended state when the power is off. When the power is off and the lock tongue 107a is under pressure, the lock tongue 107a can be retracted. In addition, the lock tongue 107a will also retract after power is turned on.
[0041] The airdrop cargo hold 1 of the above structure is fixed in the airdrop cabin installation cavity by gluing or screwing, and when the two doors are closed, the bottom surfaces of the left door 101a and the right door 101b are conformal to the outer surface of the fuselage to reduce flight resistance. Figure 5 , Figure 6 As shown, a torsion spring installation box 108 is also designed in the middle of the bottom edge of the left frame of the cargo hold frame 103, and a retractable torsion spring 109 is arranged in the torsion spring installation box 108. Both ends of the retractable torsion spring 109 pass through the torsion spring installation box 108, one end is fixedly connected to the left frame, and the other end is clamped and fixed between the inner wall of the airdrop cabin installation cavity and the outer wall of the cargo hold frame 103. Similarly, a retractable torsion spring 109 is installed on the bottom edge of the right frame in the same way. Thus, through the elastic force of the retractable torsion spring 109, the left door 101a and the right door 101b are automatically opened after being unlocked.
[0042] The hatch door opening and closing control in the above-designed airdrop cargo hold 1 is controlled by adding a control channel in the flight controller of the existing toy airplane to control the micro unlocking motor 107. When the airplane is flying, the user can send an airdrop command through the flight controller, and the signal receiving / control device further controls the locking tongue 107a of the micro unlocking motor 107 to retract after receiving the command. The hatch door opens under the action of gravity and the retractable torsion spring 109, and the airdropped objects 4 in the airdrop cargo hold 1 automatically fall out. Figure 7 As shown. After the user loads the airdrop 4, the left door 101a is closed first, and then the right door 101b is closed, so that the boss 101d on the left door 101a is embedded in the groove 101c on the right door 101b, and the left door 101a is pressed by the right door 101b. When the right door 101b is closed at the same time, the top locking inclined surface 106a of the lock hook 106 on the right door 101b contacts the lock tongue 107a, and the lock tongue 107a further moves and compresses along the inclined surface 106a until the top of the lock hook 106 is separated from the lock tongue 107a, and the lock tongue 107a pops out to the bottom of the lock matching side 106b of the lock hook 106, and the lock tongue 107a cooperates with the bottom surface of the lock matching side 106b to limit the rotation of the right door 101b. At this time, the two doors are closed in place, and the loading of the airdrop 4 is completed.
Claims
1. A remote-controlled toy airplane with an airdrop function, characterized in that: An airdrop cabin installation cavity is opened in the belly of the existing toy aircraft fuselage, and an airdrop cargo hold is fixedly installed inside; The bottom surface of the airdrop cargo hold has a left door and a right door, which are hinged to the left and right sides of the airdrop cargo hold respectively; A groove and a boss are designed on the opposite side of the left door and the right door respectively. When the left door and the right door are closed, the boss and the groove overlap and are positioned; at the same time, a lock hook is designed on the right door, which cooperates with the locking motor installed in the airdrop cabin to maintain the closed state of the left door and the right door when the left door and the right door are closed.
2. A remote-controlled toy airplane with an airdrop function as claimed in claim 1, characterized in that: The airdrop cargo hold is a rectangular frame structure having a left frame, a right frame and a top frame, all of which have reinforcing beams arranged at equal intervals between the circumferential frame and the opposite sides of the frame.
3. A remote-controlled toy airplane with an airdrop function as claimed in claim 1, characterized in that: The front and rear ends of the bottom edges of the left and right frames are designed with columnar frame joints that are integrally formed with the cargo hold frame. Axial holes with their axes along the front-to-back direction are coaxially opened on the frame joints, which respectively cooperate with door joints designed on the left and right doors and are connected through connecting shafts.
4. A remote-controlled toy airplane with an airdrop function as claimed in claim 1, characterized in that: The locking motor is fixedly mounted on the upper surface of the cargo hold bottom support fixedly mounted between the left and right side walls of the airdrop cargo hold; The bottom support of the cargo hold is provided with an opening for the locking hook to pass through.
5. A remote-controlled toy airplane with an airdrop function as claimed in claim 1, characterized in that: The left door has the same structure as the right door, with a flat top surface, a side wall perpendicular to the top surface on one side, and a curved bottom surface connected to the side wall and the top surface. In the right door, a groove is designed at the angle between the top surface and the side surface. The groove is designed along the front-to-back direction and runs through the front and rear sides of the right door. At the same time, in the left door, a boss is designed on the side. The boss is designed along the front-to-back direction, and the top surface and front and rear end surfaces are flush with the top surface and front and rear sides of the left door respectively.
6. A remote-controlled toy airplane with an airdrop function as claimed in claim 1, characterized in that: The lock hook is an L-shaped hook structure as a whole, with one side arranged perpendicular to the top surface of the right door and the end fixedly installed on the top surface of the right door; the other side of the lock hook is the locking matching side, and the top is designed as a locking inclined surface, which cooperates with the lock tongue of the locking motor during the closing process of the left and right doors; the bottom surface of the lock hook is the locking matching surface, which cooperates with the lock tongue after the left and right doors are closed.
7. A remote-controlled toy airplane with an airdrop function as claimed in claim 1, characterized in that: When the left door and the right door are fully closed, the outer surfaces of the left door and the right door are conformal to the outer surface of the fuselage.
8. A remote-controlled toy airplane with an airdrop function as claimed in claim 1, characterized in that: A torsion spring installation box is designed at the bottom of the left and right sides of the airdrop cargo hold, and a retractable torsion spring is arranged in the torsion spring installation box; the two ends of the retractable torsion spring are respectively fixed to the airdrop cargo hold and the fuselage.