CN110993415A - Novel electronic product with extensible type simulated airplane torsion trip switch function - Google Patents

Novel electronic product with extensible type simulated airplane torsion trip switch function Download PDF

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Publication number
CN110993415A
CN110993415A CN201911305315.6A CN201911305315A CN110993415A CN 110993415 A CN110993415 A CN 110993415A CN 201911305315 A CN201911305315 A CN 201911305315A CN 110993415 A CN110993415 A CN 110993415A
Authority
CN
China
Prior art keywords
circuit board
electronic product
torsion
extensible
switch
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201911305315.6A
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Chinese (zh)
Inventor
付强
周志园
刘忠亮
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Harbin Laite Brothers Technology Development Co ltd
Original Assignee
Harbin Laite Brothers Technology Development Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Harbin Laite Brothers Technology Development Co ltd filed Critical Harbin Laite Brothers Technology Development Co ltd
Priority to CN201911305315.6A priority Critical patent/CN110993415A/en
Publication of CN110993415A publication Critical patent/CN110993415A/en
Pending legal-status Critical Current

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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H23/00Tumbler or rocker switches, i.e. switches characterised by being operated by rocking an operating member in the form of a rocker button
    • H01H23/02Details
    • H01H23/12Movable parts; Contacts mounted thereon
    • H01H23/16Driving mechanisms
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H23/00Tumbler or rocker switches, i.e. switches characterised by being operated by rocking an operating member in the form of a rocker button
    • H01H23/02Details
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H23/00Tumbler or rocker switches, i.e. switches characterised by being operated by rocking an operating member in the form of a rocker button
    • H01H23/02Details
    • H01H23/04Cases; Covers

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  • Mechanical Control Devices (AREA)

Abstract

The invention discloses a novel electronic product with an extensible simulated airplane torsion switch function, which comprises a main body of a jump switch, wherein the main body of the jump switch comprises a trigger component, a control component and a switch shell, the trigger component mainly comprises a stop block, a rear circuit board, an actuating rod, a contact disc, a front circuit board, a connecting rod, a connecting sheet and a torsion handle, and the control component comprises an electromagnet, a bottom circuit board, a contact pin and a ZH1.5 connector. The novel electronic product with the extensible simulated airplane torsion spring switch function is simple to produce and assemble and greatly reduces the cost by designing the novel torsion spring switch with few structural components, mainly simulates the A-gear function, the manual B-gear function and the automatic circuit-breaking-to-B-gear function of a torsion bar spring switch, can be expanded into the self-recovery A-gear function and the controllable triggering-type B-gear function, and improves the function of the torsion switch.

Description

Novel electronic product with extensible type simulated airplane torsion trip switch function
Technical Field
The invention relates to the field of extensible button switches, in particular to a novel electronic product with an extensible simulated airplane button trip switch function.
Background
The toggle switch is also called as a rocker switch, the name of the toggle switch is that the toggle switch is always twisted when the toggle switch is used, the toggle switch is a manually controlled micro switch, and various toggle switches are usually arranged on a simulated airplane to achieve the simulation effect.
Disclosure of Invention
The invention mainly aims to provide a novel electronic product with an extensible simulated airplane torsion trip switch function, which can effectively solve the problems in the background technology.
In order to achieve the purpose, the invention adopts the technical scheme that:
the utility model provides a novel electronic product with extensible emulation aircraft turns round sub-trip switch function, includes the trip switch main part, the trip switch main part is including trigger assembly and control assembly and switch shell triplex, trigger assembly mainly comprises stop block, back circuit board, makes pole, contact dish, front circuit board, connecting rod, connection piece and the knob handle, control assembly then comprises electro-magnet, end circuit board, contact pin and ZH1.5 connector.
Preferably, the control assembly is mounted at the tail part of the trigger assembly, and the switch shell is sleeved outside the trigger assembly and the control assembly and is connected with a rear cover arranged at the bottom of the control assembly.
Preferably, a rotating ball is arranged in the middle of the knob handle, an installation pin is transversely installed in the rotating ball, and the head of the knob handle penetrates through the head of the switch shell and is movably installed on the protruding ring of the head of the switch shell through the installation pin.
Preferably, the tail part of the knob handle is movably connected with one end of a triangular connecting piece through a connecting pin, the other end of the connecting piece is sleeved with a connecting rod which is movably connected to the connecting rod through the connecting pin, and the other end of the connecting rod is movably connected to the head part of the actuating rod through a connecting screw.
Preferably, the outer ring of the actuating rod is further provided with an annular contact disc, the tail of the actuating rod is sleeved with a connecting spring and is connected to the stop block backwards, the actuating rod and the contact disc are sleeved with a second packaging shell, and the stop block is sleeved with a first packaging shell.
Preferably, the front end and the rear end of the second packaging shell are respectively provided with a front circuit board and a rear circuit board, the inner sides of the front circuit board and the rear circuit board are symmetrically provided with two micro switches, and the second packaging shell and the first packaging shell are connected together through three fixing screws.
Preferably, the ZH1.5 connector is fixedly mounted on the bottom circuit board, three contact pins are symmetrically mounted at the front end of the bottom circuit board through the circle center, the electromagnet is mounted at the circle center of the bottom circuit board through a connecting screw, a third packaging shell is sleeved outside the electromagnet, the third packaging shell is mounted on the bottom circuit board through three mounting screws, and the contact pins penetrate out of a reserved hole in the outer wall of the third packaging shell.
Compared with the prior art, the invention has the following beneficial effects:
the novel torque rod switch mainly simulates the A-gear function, the manual B-gear function and the automatic disconnection-to-B-gear function of the torque rod switch, can be expanded into the self-recovery A-gear function and the controllable triggering type B-gear function, and improves the functions of the torque switch.
Drawings
Fig. 1 is a schematic diagram of an overall structure of a novel electronic product with an extensible simulated airplane torsion trip switch function according to the present invention;
FIG. 2 is an exploded view of a novel electronic product with an extensible simulated airplane torsion trip switch function according to the present invention;
FIG. 3 is an exploded view of the trigger assembly of the novel electronic product with the extendable electronic product for simulating the toggle switch function of the airplane;
FIG. 4 is an exploded view of the control module of the novel electronic product with the extendable electronic product for simulating the toggle switch function of the airplane torsion bar according to the present invention;
FIG. 5 is a schematic diagram of the A-shelf of a novel electronic product with an extensible simulated airplane torsion trip switch function according to the present invention;
FIG. 6 is a cross-sectional view taken at A-A of FIG. 5;
FIG. 7 is a schematic diagram of a B-stage of a novel electronic product with an extensible simulated airplane torsion trip switch function according to the present invention;
fig. 8 is a cross-sectional view taken at B-B in fig. 7.
In the figure: 1. a jumper switch main body; 2. a trigger component; 3. a control component; 4. a switch housing; 5. a stopper block; 6. a first package housing; 7. a connecting spring; 8. a rear circuit board; 9. a microswitch; 10. a second package housing; 11. an actuating rod; 12. a contact pad; 13. a connecting screw; 14. a front circuit board; 15. a connecting rod; 16. connecting sheets; 17. a connecting pin; 18. a knob handle; 19. installing a pin; 20. a set screw; 21. an electromagnet; 22. a third packaging shell; 23. a bottom circuit board; 24. inserting a pin; 25. a connecting screw; 26. a ZH1.5 connector; 27. mounting screws; 28. and (7) a rear cover.
Detailed Description
In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the invention easy to understand, the invention is further described with the specific embodiments.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, such as "connected," which may be fixedly connected, detachably connected, or integrally connected; 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.
As shown in fig. 1-8, a novel electronic product with an extensible simulated aircraft torsion bar jumper function comprises a jumper switch main body 1, the jumper switch main body 1 comprises three parts, namely a trigger component 2, a control component 3 and a switch shell 4, the trigger component 2 mainly comprises a stop block 5, a rear circuit board 8, an actuating rod 11, a contact disc 12, a front circuit board 14, a connecting rod 15, a connecting piece 16 and a torsion bar handle 18, and the control component 3 comprises an electromagnet 21, a bottom circuit board 23, a contact pin 24 and a ZH1.5 connector 26.
The control component 3 is arranged at the tail part of the trigger component 2, and the switch shell 4 is sleeved outside the trigger component 2 and the control component 3 and is connected with a rear cover 28 arranged at the bottom of the control component 3; a rotating ball is arranged in the middle of the knob handle 18, an installation pin 19 is transversely installed in the rotating ball, and the head of the knob handle 18 penetrates through the head of the switch shell 4 and is movably installed on a protruding ring of the head of the switch shell 4 through the installation pin 19; the tail part of the knob handle 18 is movably connected with 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 which is movably connected with the connecting pin 17, and the other end of the connecting rod 15 is movably connected with the head part of the actuating rod 11 through a connecting screw 13; an annular contact disc 12 is further arranged on the outer ring of the actuating rod 11, a connecting spring 7 is sleeved at the tail of the actuating rod 11 and is connected to the stop block 5 backwards, a second packaging shell 10 is sleeved outside the actuating rod 11 and the contact disc 12, and a first packaging shell 6 is sleeved outside the stop block 5; the front end and the rear end of the second packaging shell 10 are respectively provided with a front circuit board 14 and a rear circuit board 8, the inner sides of the front circuit board 14 and the rear circuit board 8 are respectively provided with two micro switches 9, and the second packaging shell 10 and the first packaging shell 6 are connected together through three fixing screws 20; the ZH1.5 connector 26 is fixedly installed on the bottom circuit board 23, three contact pins 24 are symmetrically installed at the front end of the bottom circuit board 23 in a circle center manner, the electromagnet 21 is installed at the circle center of the bottom circuit board 23 through a connecting screw 25, a third packaging shell 22 is sleeved outside the electromagnet 21, the third packaging shell 22 is installed on the bottom circuit board 23 through three installation screws 27, and the contact pins 24 penetrate out of a reserved hole in the outer wall of the third packaging shell 22.
It should be noted that the present invention is a novel electronic product with extensible simulated airplane torsion switch function, wherein the torsion handle 18 in the trigger assembly 2 is fixed on 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 enclosure 10, the actuating rod 11 is sleeved in the connecting spring 7 and fixed on the stop block 5 through the first enclosure 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 freely slide in the first enclosure 6, one end of the connecting spring 7 is pressed against the first enclosure 6, and the other end is pressed against the contact disc 12 of the actuating rod 11, the torsion handle 18 is kept on the a gear through the expansion force of the spring, when the torsion handle 18 is on the a gear, the contact disc 12 on the actuating rod 11 triggers the micro switch 9 mounted on the front circuit board 14, outputting an A-gear contact signal, and when the knob handle 18 is shifted to a B-gear, a contact disc 12 on the actuating rod 11 triggers a microswitch 9 arranged on the rear circuit board 8 to output a B-gear contact signal; the electromagnet 21 on the control component 3 is a power-on demagnetizing type magnet, is fixed in a third packaging shell 22 by a connecting screw 25, and is controlled by a circuit of a ZH1.5 connector 26 on a bottom circuit board 23, when the torque handle 18 is in a B gear, the electromagnet 21 has magnetism, the stop block 5 keeps a suction state to keep the B gear, when the control circuit powers on the electromagnet 21 instantly, the electromagnet 21 is demagnetized, the actuating rod 11 is pushed by the elasticity of the connecting spring 7 to enable the torque handle 18 to rebound to an A gear, and at the moment, the contact disc 12 on the actuating rod 11 triggers the microswitch 9 of the A gear to output an A gear contact signal, so that the automatic disconnection is realized as the A gear; in addition, when the electromagnet 21 is changed to be electrified with a magnetic magnet, when the torque handle 18 is shifted to the B gear, if the control circuit does not electrify the electromagnet 21 and the electromagnet 21 is not magnetic, the actuating rod 11 is pushed by the elastic force of the connecting spring 7 to enable the torque handle 18 to rebound to the A gear, at the moment, the torque switch is in a self-reset A gear state (the B gear cannot be kept), and when the torque handle 18 is shifted to the B gear, if the control circuit electrifys the electromagnet 21 and the electromagnet 21 is magnetic, the stop block 5 keeps an attraction state, the stop block is kept to the B gear, and the expansion can be carried out as required.
The foregoing shows and describes the general principles and broad features of the present invention and advantages thereof. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the invention as claimed. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims (7)

1. The utility model provides a novel electronic product that has extensible emulation aircraft button trip switch function, includes trip switch main part (1), its characterized in that: the trip switch main body (1) comprises a trigger assembly (2), a control assembly (3) and a switch shell (4), wherein the trigger assembly (2) mainly comprises a stop block (5), a rear circuit board (8), an actuating rod (11), a contact disc (12), a front circuit board (14), a connecting rod (15), a connecting sheet (16) and a torque handle (18), and the control assembly (3) comprises an electromagnet (21), a bottom circuit board (23), a contact pin (24) and a ZH1.5 connector (26).
2. The novel electronic product with the extensible simulated airplane torsion trip switch function according to claim 1, is characterized in that: the control assembly (3) is arranged at the tail part of the trigger assembly (2), and the switch shell (4) is sleeved outside the trigger assembly (2) and the control assembly (3) and connected with a rear cover (28) arranged at the bottom of the control assembly (3).
3. The novel electronic product with the extensible simulated airplane torsion trip switch function according to claim 1, is characterized in that: the middle position of the knob handle (18) is provided with a rotating ball, a mounting pin (19) is transversely mounted in the rotating ball, and the head of the knob handle (18) penetrates through the head of the switch shell (4) and is movably mounted on a protruding ring of the head of the switch shell (4) through the mounting pin (19).
4. The novel electronic product with the extensible simulated airplane torsion trip switch function according to claim 1, is characterized in that: the tail of the knob handle (18) is movably connected with 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) which is movably connected with the connecting pin (17), and the other end of the connecting rod (15) is movably connected with the head of the actuating rod (11) through a connecting screw (13).
5. The novel electronic product with the extensible simulated airplane torsion trip switch function according to claim 1, is characterized in that: an annular contact disc (12) is further arranged on the outer ring of the actuating rod (11), a connecting spring (7) is sleeved at the tail of the actuating rod (11) and is connected to the stop block (5) backwards, a second packaging shell (10) is sleeved outside the actuating rod (11) and the contact disc (12), and a first packaging shell (6) is sleeved outside the stop block (5).
6. The novel electronic product with the extensible simulated airplane torsion trip switch function according to claim 5, is characterized in that: the front end and the rear end of the second packaging shell (10) are respectively provided with a front circuit board (14) and a rear circuit board (8), the inner sides of the front circuit board (14) and the rear circuit board (8) are symmetrically provided with two micro switches (9), and the second packaging shell (10) and the first packaging shell (6) are connected together through three fixing screws (20).
7. The novel electronic product with the extensible simulated airplane torsion trip switch function according to claim 1, is characterized in that: ZH1.5 connector (26) fixed mounting is on end circuit board (23), three contact pins (24) are installed with centre of a circle symmetry to the front end of end circuit board (23), electro-magnet (21) are installed the centre of a circle department of circuit board (23) to the end through a connecting screw (25), the outside cover of electro-magnet (21) has No. three encapsulation shell (22) to No. three encapsulation shell (22) are installed on circuit board (23) to the end through three mounting screw (27), contact pin (24) then wear out from the preformed hole on No. three encapsulation shell (22) outer wall.
CN201911305315.6A 2019-12-18 2019-12-18 Novel electronic product with extensible type simulated airplane torsion trip switch function Pending CN110993415A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201911305315.6A CN110993415A (en) 2019-12-18 2019-12-18 Novel electronic product with extensible type simulated airplane torsion trip switch function

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201911305315.6A CN110993415A (en) 2019-12-18 2019-12-18 Novel electronic product with extensible type simulated airplane torsion trip switch function

Publications (1)

Publication Number Publication Date
CN110993415A true CN110993415A (en) 2020-04-10

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Application Number Title Priority Date Filing Date
CN201911305315.6A Pending CN110993415A (en) 2019-12-18 2019-12-18 Novel electronic product with extensible type simulated airplane torsion trip switch function

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114995225A (en) * 2022-05-25 2022-09-02 兰州万里航空机电有限责任公司 Controller based on cockpit cover operating device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114995225A (en) * 2022-05-25 2022-09-02 兰州万里航空机电有限责任公司 Controller based on cockpit cover operating device

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