A new type of electronic product with expandable simulated aircraft toggle switch function
By designing a new electronic product with the function of a scalable simulated aircraft, the existing torque switch has solved the complex structure and limited functions of the existing torque switch, and the effects of simplification of production, cost reduction and function expansion have been achieved.
Patent Information
- Application Number
- CN201911305315.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2019-12-18
- Publication Date
- 2025-04-29
- Estimated Expiration
- 2039-12-18
AI Technical Summary
The existing simulated aircraft's twist jump switch has complex structure, cumbersome production and assembly, and cannot be expanded and multi-purpose, which limits its use on simulated aircraft.
A new type of electronic product with the function of a scalable simulated aircraft torque jump switch is designed, including the jump switch body consisting of a trigger component and a control component. By simplifying the structure and adopting a scalable design, a multi-functional torque jump switch is realized.
It realizes simplification of production and assembly, reduces costs, and expands the functions of the torque switch, including the A and B functions of the simulated torque sub-pole jump switch, as well as the automatic circuit breaker and self-recovery functions.
Smart Images

Figure CN110993415B_ABST
Abstract
Description
Technical Field
[0001] The invention relates to the field of expandable torsion switches, and in particular to a novel electronic product with an expandable simulated airplane torsion switch function. Background Art
[0002] A toggle switch is also called a shaking switch. It gets its name from the fact that it is always twisted when used. A toggle switch is a manually controlled micro switch. In simulated aircraft, various types of toggle switches are usually set up to achieve simulation effects. However, the simulated jump switches currently produced have complex structures, and their production and assembly are relatively cumbersome. They also use more structural components and cannot be expanded for multiple uses, which limits their use in simulated aircraft. Summary of the invention
[0003] The main purpose of the present invention is to provide a novel electronic product with an expandable simulated aircraft torsion switch function, which can effectively solve the problems in the background technology.
[0004] To achieve the above object, the technical solution adopted by the present invention is:
[0005] A novel electronic product with an expandable simulated aircraft torsion jump switch function includes a jump switch body, which includes a trigger component, a control component and a switch housing. The trigger component is mainly composed of a stop block, a rear circuit board, an actuating rod, a contact plate, a front circuit board, a connecting rod, a connecting piece and a torsion handle, and the control component is composed of an electromagnet, a bottom circuit board, a pin and a ZH1.5 connector.
[0006] Preferably, the control assembly is installed at the tail of the trigger assembly, and the switch housing is sleeved on the outside of the trigger assembly and the control assembly, and is connected to a back cover arranged at the bottom of the control assembly.
[0007] Preferably, a rotating ball is provided in the middle of the twist handle, and a mounting pin is installed transversely in the rotating ball. The head of the twist handle passes through the head of the switch housing and is movably mounted on the protruding ring of the head of the switch housing through the mounting pin.
[0008] Preferably, the tail of the twist handle is movably connected to one end of a triangular connecting piece through a connecting pin, the other end of the connecting piece is movably connected to a connecting rod through a connecting pin, and the other end of the connecting rod is movably connected to the head of the actuating rod through a connecting screw.
[0009] Preferably, the outer ring of the actuating rod is further provided with an annular contact disk, the tail of the actuating rod is covered with a connecting spring and is rearwardly connected to a stop block, the outside of the actuating rod and the contact disk is covered with a No. 2 packaging shell, and the outside of the stop block is covered with a No. 1 packaging shell.
[0010] Preferably, a front circuit board and a rear circuit board are respectively provided at the front and rear ends of the No. 2 packaging shell, two micro switches are symmetrically installed on the inner sides of the front circuit board and the rear circuit board, and the No. 2 packaging shell and the No. 1 packaging shell are connected together by three fixing screws.
[0011] Preferably, the ZH1.5 connector is fixedly mounted on the bottom circuit board, and three pins are symmetrically mounted with the center of the circle on the front end of the bottom circuit board. The electromagnet is mounted at the center of the circle of the bottom circuit board through a connecting screw, and a No. 3 packaging shell is sleeved on the outside of the electromagnet, and the No. 3 packaging shell is mounted on the bottom circuit board through three mounting screws, and the pins pass through the reserved holes on the outer wall of the No. 3 packaging shell.
[0012] Compared with the prior art, the present invention has the following beneficial effects:
[0013] In the present invention, a new type of torsion switch with fewer structural components is designed to simplify production and assembly and greatly reduce costs. This product mainly simulates the A-level function, manual B-level function, and automatic circuit breaking B-level function of the torsion switch, and can be expanded to self-recovering A-level and controllable trigger B-level functions, thereby improving the function of the torsion switch. BRIEF DESCRIPTION OF THE DRAWINGS
[0014] Figure 1 This is a schematic diagram of the overall structure of a novel electronic product with an expandable simulated aircraft toggle switch function according to the present invention;
[0015] Figure 2 This is a disassembly diagram of a novel electronic product with an expandable simulated aircraft toggle switch function according to the present invention;
[0016] Figure 3 This is an exploded diagram of a trigger assembly of a novel electronic product with an expandable simulated aircraft toggle switch function according to the present invention;
[0017] Figure 4 This is an exploded view of a control component of a novel electronic product with an expandable simulated aircraft toggle switch function according to the present invention;
[0018] Figure 5 A schematic diagram of a novel electronic product with an expandable simulated airplane torsion switch function in the present invention;
[0019] Figure 6 for Figure 5 Sectional view at AA;
[0020] Figure 7 This is a schematic diagram of the B gear of a novel electronic product with an expandable simulated aircraft toggle switch function according to the present invention;
[0021] Figure 8 for Figure 7 Cross-sectional view at BB in the middle.
[0022] In the figure: 1. jumper body; 2. trigger assembly; 3. control assembly; 4. switch housing; 5. stop block; 6. No. 1 package shell; 7. connecting spring; 8. rear circuit board; 9. micro switch; 10. No. 2 package shell; 11. actuator rod; 12. contact plate; 13. connecting screw; 14. front circuit board; 15. connecting rod; 16. connecting piece; 17. connecting pin; 18. twist handle; 19. mounting pin; 20. fixing screw; 21. electromagnet; 22. No. 3 package shell; 23. bottom circuit board; 24. pin; 25. connecting screw; 26. ZH1.5 connector; 27. mounting screw; 28. rear cover. DETAILED DESCRIPTION
[0023] In order to make the technical means, creative features, objectives and effects achieved by the present invention easy to understand, the present invention is further explained below in conjunction with specific implementation methods.
[0024] In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "two ends", "one end", "the other end" and the like indicate positions or positional relationships based on the positions or positional relationships shown in the drawings, and are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as limiting the present invention. In addition, the terms "first" and "second" are used for descriptive purposes only and cannot be understood as indicating or implying relative importance.
[0025] In the description of the present invention, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "provided with", "connected", etc. should be understood in a broad sense. For example, "connected" can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be indirectly connected through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.
[0026] like Figure 1-8As shown, a new type of electronic product with an expandable simulated aircraft torsion jump switch function includes a jump switch body 1, which includes a trigger component 2, a control component 3 and a switch housing 4. The trigger component 2 is mainly composed of a stop block 5, a rear circuit board 8, an actuating rod 11, a contact plate 12, a front circuit board 14, a connecting rod 15, a connecting piece 16 and a torsion handle 18, and the control component 3 is composed of an electromagnet 21, a bottom circuit board 23, a pin 24 and a ZH1.5 connector 26.
[0027] The control assembly 3 is installed at the tail of the trigger assembly 2, and the switch housing 4 is sleeved on the outside of the trigger assembly 2 and the control assembly 3, and is connected to the back cover 28 arranged at the bottom of the control assembly 3; a rotating ball is provided in the middle position of the twist handle 18, and a mounting pin 19 is installed horizontally in the rotating ball, and the head of the twist handle 18 passes through the head of the switch housing 4 and is movably installed on the protruding ring of the head of the switch housing 4 through the mounting pin 19; the tail of the twist handle 18 is movably connected to one end of the triangular connecting piece 16 through the connecting pin 17, and the other end of the connecting piece 16 is sleeved with a connecting pin 17 and movably connected to the connecting rod 15, and the other end of the connecting rod 15 is movably connected to the head of the actuating rod 11 through the connecting screw 13; the outer ring of the actuating rod 11 is also provided with an annular contact plate 12, and the tail of the actuating rod 11 is sleeved with a connecting spring 7 and connected to the rear On the stop block 5, the outer part of the actuating rod 11 and the contact plate 12 is covered with a No. 2 packaging shell 10, and the outer part of the stop block 5 is covered with a No. 1 packaging shell 6; the front end and the rear end of the No. 2 packaging shell 10 are respectively provided with a front circuit board 14 and a rear circuit board 8, and two micro switches 9 are symmetrically installed on the inner sides of the front circuit board 14 and the rear circuit board 8, and the No. 2 packaging shell 10 and the No. 1 packaging shell 6 are connected together by three fixing screws 20; the ZH1.5 connector 26 is fixedly installed on the bottom circuit board 23, and three pins 24 are symmetrically installed at the front end of the bottom circuit board 23 with the center of the circle, and the electromagnet 21 is installed at the center of the circle of the bottom circuit board 23 by a connecting screw 25, and the outer part of the electromagnet 21 is covered with a No. 3 packaging shell 22, and the No. 3 packaging shell 22 is installed on the bottom circuit board 23 by three mounting screws 27, and the pins 24 pass through the reserved holes on the outer wall of the No. 3 packaging shell 22.
[0028] It should be noted that the present invention is a novel electronic product with an expandable simulated aircraft torsion switch function, wherein the torsion handle 18 in the trigger assembly 2 is fixed to the connecting piece 16 through the connecting pin 17, the connecting piece 16 is connected to the connecting rod 15 through the connecting pin 17, the connecting rod 15 is connected to the actuating rod 11, the actuating rod 11 is installed in the second packaging shell 10, the actuating rod 11 is inserted into the connecting spring 7 and fixed to the stop block 5 through the first packaging shell 6, at this time, the torsion handle 18 is toggled to drive the actuating rod 11 through the connecting rod 15 so that the stop block 5 can be moved in the first packaging shell. The package shell 6 slides freely, one end of the connecting spring 7 presses on the No. 1 package shell 6, and the other end presses on the contact plate 12 of the actuating rod 11. The torsion handle 18 is kept in the A gear by the tension of the spring. When the torsion handle 18 is in the A gear, the contact plate 12 on the actuating rod 11 triggers the micro switch 9 installed on the front circuit board 14, and outputs the A gear contact signal. When the torsion handle 18 is turned to the B gear, the contact plate 12 on the actuating rod 11 triggers the micro switch 9 installed on the rear circuit board 8, and outputs the B gear contact signal. The electromagnet 21 on the control component 3 is energized to eliminate The magnetic magnet is fixed in the No. 3 package shell 22 by the connecting screw 25 and is controlled by the circuit of the ZH1.5 connector 26 on the bottom circuit board 23. When the torsion handle 18 is in the B position, the electromagnet 21 is magnetic, and the stop block 5 remains in the attracted state to keep it in the B position. When the control circuit energizes the electromagnet 21 momentarily, the electromagnet 21 is demagnetized, and the elastic force of the connecting spring 7 pushes the actuating rod 11 to make the torsion handle 18 rebound to the A position. At this time, the contact plate 12 on the actuating rod 11 triggers the micro switch 9 of the A position and outputs the A position contact signal to realize automatic circuit breaking to A. gear; in addition, when the electromagnet 21 is replaced with an energized magnetic magnet, when the torsion handle 18 is moved to the B gear, if the control circuit does not energize the electromagnet 21 at this time, the electromagnet 21 is non-magnetic, and the elastic force of the connecting spring 7 pushes the actuating rod 11 to make the torsion handle 18 rebound to the A gear. At this time, the torsion switch is in the self-resetting A gear state (unable to maintain the B gear). When the torsion handle 18 is moved to the B gear, if the control circuit energizes the electromagnet 21 at this time, the electromagnet 21 is magnetic, and the stop block 5 remains in the attracted state, then it is kept in the B gear, which can be expanded as needed.
[0029] The above shows and describes the basic principles and main features of the present invention and the advantages of the present invention. It should be understood by those skilled in the art that the present invention is not limited to the above embodiments. The above embodiments and descriptions are only for explaining the principles of the present invention. Without departing from the spirit and scope of the present invention, the present invention may have various changes and improvements, which fall within the scope of the present invention to be protected. The scope of protection of the present invention is defined by the attached claims and their equivalents.
Claims
1. A novel electronic product with expandable simulated aircraft toggle switch function, comprising a switch body (1), characterized in that: The circuit breaker body (1) comprises three parts: a trigger assembly (2), a control assembly (3) and a switch housing (4); the trigger assembly (2) comprises a stop block (5), a rear circuit board (8), an actuating rod (11), a contact plate (12), a front circuit board (14), a connecting rod (15), a connecting piece (16) and a twist handle (18); and the control assembly (3) comprises an electromagnet (21), a bottom circuit board (23), a pin (24) and a ZH1.5 connector (26); A rotating ball is provided in the middle of the twist handle (18), and a mounting pin (19) is transversely mounted inside the rotating ball. The head of the twist handle (18) passes through the head of the switch housing (4) and is movably mounted on the protruding ring of the head of the switch housing (4) through the mounting pin (19). The tail of the twist handle (18) is movably connected to one end of a triangular connecting piece (16) through a connecting pin (17); the other end of the connecting piece (16) is sleeved with a connecting rod (15) movably connected to the connecting pin (17); the other end of the connecting rod (15) is movably connected to the head of the actuating rod (11) through a connecting screw (13); The outer ring of the actuating rod (11) is further provided with an annular contact disk (12); the tail of the actuating rod (11) is sleeved with a connecting spring (7) and is rearwardly connected to a stop block (5); the actuating rod (11) and the contact disk (12) are sleeved with a No. 2 packaging shell (10); and the stop block (5) is sleeved with a No. 1 packaging shell (6); A front circuit board (14) and a rear circuit board (8) are respectively arranged at the front and rear ends of the second packaging shell (10); two micro switches (9) are symmetrically mounted on the inner sides of the front circuit board (14) and the rear circuit board (8); and the second packaging shell (10) and the first packaging shell (6) are connected together by three fixing screws (20); The ZH1.5 connector (26) is fixedly mounted on the bottom circuit board (23), and three pins (24) are symmetrically mounted on the front end of the bottom circuit board (23) with the center of the circle. The electromagnet (21) is mounted on the center of the bottom circuit board (23) via a connecting screw (25). A No. 3 packaging shell (22) is sleeved on the outside of the electromagnet (21), and the No. 3 packaging shell (22) is mounted on the bottom circuit board (23) via three mounting screws (27), and the pins (24) pass through the reserved holes on the outer wall of the No. 3 packaging shell (22).
2. According to claim 1, a novel electronic product with expandable simulated aircraft toggle switch function is characterized in that: The control component (3) is installed at the tail of the trigger component (2), and the switch housing (4) is sleeved on the outside of the trigger component (2) and the control component (3), and is connected to a rear cover (28) arranged at the bottom of the control component (3).
Citation Information
Patent Citations
Simulated aircraft twist rod circuit breaker
CN108320977A
Electronic product with extensible simulation airplane toggle jump switch function
CN211062635U