Multi-stage trigger with state feedback function for flight auxiliary integrated switch

Abstract

This invention relates to the field of integrated switch technology, specifically to a multi-stage triggering flight assistance integrated switch with status feedback function. It includes a toggle assembly, a status feedback assembly, and a circuit assembly. The triggering part of the status feedback assembly is connected to the toggle assembly. When the output part of the toggle assembly moves to a preset prediction position, it controls the status feedback assembly to move. During movement, the output part of the status feedback assembly is driven to the output part of the toggle assembly and outputs at least one first status feedback signal. When the output part of the toggle assembly moves to the preset position, the circuit assembly contacts the output part of the toggle assembly and outputs a corresponding signal. This invention dynamically adjusts the required operating force of the toggle assembly at each stage of a single operation stroke by driving the status feedback assembly to the toggle assembly during movement, thereby providing the pilot with clear operational feedback when operating the toggle assembly.

Description

Technical Field

[0001] This invention relates to the field of integrated switch technology, and more specifically to a multi-segment triggering flight assistance integrated switch with status feedback function. Background Technology

[0002] Flying cars are essentially a combination of vertical takeoff and landing aircraft and ground vehicles. Their toggle switches are aviation-grade safety components, with design standards far exceeding those of ordinary car switches. The core design requirements revolve around standards such as preventing accidental activation, ease of blind operation, resistance to extreme conditions, chain slippage prevention, and ensuring safety. Furthermore, due to the high degree of electrification inherent in flying cars compared to traditional aircraft, traditional mechanical switches are no longer suitable for this new type of vehicle. For example, a toggle switch with multiple switching positions disclosed in a Chinese patent (application number: CN201480038294.5) uses a pivoting lever and a pawl mechanism to close and open various circuits, allowing users to quickly switch the device's state and easily check the toggle switch to determine the current switching status. However, in flight... In actual automotive operations, interference factors such as rotor vibration, driving bumps, and takeoff and landing impacts are unavoidable. Furthermore, when piloting a flying car, the time window for the driver to actively check control switches is narrow. Therefore, using the aforementioned switches would present significant limitations and inconvenience in practical operation. Moreover, traditional mechanical switches like toggle switches typically only provide a clear stop signal once during a single operation, indicating whether the switch is in position. Their operating force is generally fixed or linearly variable, failing to provide accurate feedback to the driver in the context of numerous interference factors during flight operations, posing a certain safety risk. Therefore, a toggle switch with moderate tactile feedback and clear feedback is needed to help flying car pilots perform flight operations better and more safely. Summary of the Invention

[0003] The technical problem to be solved by this invention is that existing toggle switches generally only provide a clear sense of stop when the switch is in position during a single operation, which is used to remind the operator whether the switch is in position. At the same time, the operating force is generally fixed or linearly variable, which cannot accurately provide the pilot with operational feedback in flight operations with many interference factors, thus posing a certain safety risk.

[0004] To solve the above-mentioned technical problems, the present invention adopts the following technical solution: a multi-segment triggered flight assistance integrated switch with status feedback function, comprising:

[0005] A toggle assembly is used by the driver to toggle the corresponding switch assembly to output a signal.

[0006] The status feedback component is used to output a first status feedback signal to the driver when the output part of the toggle assembly moves to a preset prediction position;

[0007] Circuit components are used to output corresponding signals under the drive of the toggle assembly;

[0008] The triggering part of the status feedback component is connected to the toggle component. When the output part of the toggle component moves to a preset prediction position, the toggle component controls the status feedback component to move. When the status feedback component moves, it is connected to the output part of the toggle component and outputs at least one first status feedback signal. When the output part of the toggle component moves to a preset position, the circuit component contacts the output part of the toggle component and outputs a corresponding signal.

[0009] In operation, this invention dynamically adjusts the required operating force of the toggle assembly at each stage of a single operation stroke by connecting the state feedback component with the toggle assembly during its operation. This provides the pilot with clear operational feedback when operating the toggle assembly. Furthermore, by setting several sets of state feedback components with different action intensities, each control action can be assigned a unique operating feel, assisting the pilot in precise blind operation. This allows the pilot to promptly determine whether to continue the current control action during the operation stroke. Simultaneously, by outputting multiple first state feedback signals, multi-segment triggering of the feedback signal can be achieved, further improving the operating feel and recognition accuracy. This facilitates the pilot's efficient execution of various control actions, thereby effectively improving the safety factor of flight operations.

[0010] Preferably, the status feedback component is provided with a transmission part for transmission connection with the toggle assembly, and a driving part for driving the transmission part to move. The transmission part of the status feedback component is transmission connected to the output part of the toggle assembly under the drive of the driving part, and the load of the output part of the toggle assembly is adjusted to realize the output of the first status feedback signal. The intensity of the first status feedback signal is set to be adjustable.

[0011] Preferably, the status feedback component is further provided with a reset part for driving the transmission part to reset, and the reset part of the status feedback component drives the transmission part of the status feedback component to reset when the toggle assembly is released.

[0012] Preferably, the state feedback component includes a feedback pressure plate, a drive spring, and an adjusting shaft. The feedback pressure plate includes a connecting part, a rotating part, and a transmission part connected in sequence. The free end of the connecting part is detachably in contact with the toggle assembly. The rotating part is rotatably arranged on one side of the toggle assembly via the adjusting shaft. One end of the drive spring is connected to the rotating part, and the other end of the drive spring is connected to the adjusting part of the adjusting shaft. The preload of the drive spring is adjustable. When the toggle assembly is activated, the drive spring is driven and connected to the toggle assembly via the connecting part, and deforms under the drive of the toggle assembly. The end of the connecting part separates from the toggle assembly when the output part of the toggle assembly moves to a preset prediction position to release the transmission part. The transmission part is driven and connected to the output part of the toggle assembly by the drive spring, and adjusts the load of the output part of the toggle assembly to achieve the output of the first state feedback signal.

[0013] When this invention is in operation, the mechanical operation feedback output and feedback intensity adjustment can be achieved through the cooperation of the feedback pressure plate, drive spring and adjustment shaft without additional electronic components. The feedback is clear, the triggering is stable, the anti-interference ability is strong, and it does not generate electromagnetic interference. It does not affect the flight control, navigation and communication of the flying car. At the same time, the status feedback component and the toggle component are tightly matched and are not affected by the high-frequency vibration of the flying car rotor and the impact of take-off and landing. It has high working stability and long service life.

[0014] Preferably, the device also includes a touch key portion, which is rotatably and limitly mounted on the free end of the transmission unit. When the transmission unit is connected to the toggle assembly, the bottom of the touch key portion abuts against the output portion of the toggle assembly. When the output portion of the toggle assembly moves to a preset control position, the circuit assembly contacts the top of the touch key portion and outputs a corresponding control signal.

[0015] Preferably, the end of the toggle assembly that contacts the connecting part is provided with an abutting rotating block. The abutting rotating block is rotatably mounted on one end of the toggle assembly. The outer end of the abutting rotating block abuts against the connecting part when the toggle assembly is reset and is flipped under the drive of the connecting part. After flipping to a preset position, the abutting rotating block separates from the connecting part and is connected to the connecting part after reset. The inner end of the abutting rotating block abuts against one end of the toggle assembly when the toggle assembly is activated.

[0016] Preferably, the circuit assembly includes at least one set of switch assemblies, each of which includes at least one control switch. When the output portion of the toggle assembly moves to a preset control position, the control switch contacts the output portion of the toggle assembly via a transmission assembly and outputs a corresponding control signal.

[0017] Preferably, the switch assembly is further provided with at least one prediction switch, which contacts the output part of the toggle assembly through a transmission component when the output part of the toggle assembly moves to a preset prediction position, and outputs a corresponding second state feedback signal.

[0018] When the present invention is in operation, by setting a prediction switch, an electrical signal feedback can be output synchronously when the output part of the toggle assembly moves to the preset prediction position. This electrical signal feedback triggers the corresponding sound prediction prompt or light prediction prompt, which makes it easier for the pilot to judge in time whether the current operation needs to continue, avoid misoperation, and thus further improve the safety factor of flight operations.

[0019] Preferably, the toggle assembly includes a toggle seat and a toggle lever for the driver to operate. The toggle lever is detachably mounted on the toggle seat, and the shape and size of the toggle lever are adjustable.

[0020] Preferably, the device also includes a mounting housing, in which the status feedback component and the circuit component are both mounted. One side of the mounting housing has a through hole for the operating part of the toggle assembly to be exposed to the outside. An anti-accidental touch protrusion surrounds the through hole, and the connection end of the operating part of the toggle assembly is arranged inside the anti-accidental touch protrusion.

[0021] The beneficial technical effects of this invention include:

[0022] 1. This invention dynamically adjusts the required operating force of the toggle assembly at each stage of a single operation stroke by connecting the state feedback component with the toggle assembly during its operation. This provides the pilot with clear operational feedback when operating the toggle assembly. Furthermore, by setting several sets of state feedback components with different action intensities, each control action can be given a unique operating feel, which can assist the pilot in precise blind operation control. This allows the pilot to promptly determine whether to continue executing the current control action during the operation stroke. At the same time, by outputting multiple first state feedback signals, multi-segment triggering of feedback signals can be achieved, which can further improve the operating feel and recognition accuracy, making it easier for the pilot to perform various control actions efficiently, thereby effectively improving the safety factor of flight operations.

[0023] 2. This invention achieves mechanical operation feedback output and feedback intensity adjustment through the cooperation of feedback pressure plate, drive spring and adjustment shaft without additional electronic components. The feedback is clear, the triggering is stable, the anti-interference ability is strong, and it does not generate electromagnetic interference. It does not affect the flight control, navigation and communication of the flying car. At the same time, the status feedback component and the toggle component are tightly matched and are not affected by the high-frequency vibration of the flying car rotor and the impact of take-off and landing. It has high working stability and long service life.

[0024] 3. By setting a prediction switch, the present invention can synchronously output an electrical signal feedback when the output part of the toggle assembly moves to a preset prediction position. This electrical signal feedback triggers a corresponding sound prediction prompt or light prediction prompt, which makes it easier for the pilot to judge whether the current operation needs to continue, avoid misoperation, and thus further improve the safety factor of flight operations.

[0025] Other features and advantages of the present invention will be described in detail in the following specific embodiments and accompanying drawings. Attached Figure Description

[0026] The invention will be further described below with reference to the accompanying drawings:

[0027] Figure 1 An exploded view of a multi-segment triggered flight assistance integrated switch with status feedback function;

[0028] Figure 2 Schematic diagram of the toggle assembly and status feedback assembly Figure 1 ;

[0029] Figure 3 Schematic diagram of the toggle assembly and status feedback assembly Figure 2 ;

[0030] Figure 4 This is an exploded view of the circuit components;

[0031] Figure 5 This is a magnified view of the mounting housing.

[0032] Figure 6 A schematic diagram of a multi-segment triggered flight assistance integrated switch with status feedback function;

[0033] Figure 7 This is a circuit structure diagram of a portion of the circuitry in a multi-segment triggered flight assistance integrated switch with status feedback function. Detailed Implementation

[0034] The technical solutions of the embodiments of the present invention will be explained and described below with reference to the accompanying drawings. However, the following embodiments are only preferred embodiments of the present invention and not all of them. Other embodiments obtained by those skilled in the art based on the embodiments in the implementation methods without creative effort are all within the protection scope of the present invention.

[0035] In the following description, terms such as “inner,” “outer,” “upper,” “lower,” “left,” and “right” are used only to indicate orientation or positional relationship for the convenience of describing the embodiments and simplifying the description, and are not intended to indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation, and therefore should not be construed as a limitation of the present invention.

[0036] Example 1:

[0037] Please see Figure 1 This embodiment discloses a multi-segment triggering flight assistance integrated switch with status feedback function, including:

[0038] The toggle assembly 1 is used by the driver to toggle to trigger the corresponding switch assembly 31 to output a signal.

[0039] The status feedback component 2 is used to output a first status feedback signal to the driver when the output part of the toggle component 1 is moved to a preset prediction position;

[0040] Circuit component 3 is used to output corresponding signals under the drive of toggle component 1;

[0041] The triggering part of the status feedback component 2 is connected to the toggle component 1. When the output part of the toggle component 1 moves to the preset prediction position, the status feedback component 2 is activated. When activated, the output part of the status feedback component 2 is connected to the output part of the toggle component 1 and outputs at least one first status feedback signal. In specific implementation, in order to set up a multi-stage triggered status feedback component 2 according to actual needs, so that the driver can clearly identify the accurate operation button among many operation toggle buttons, making it more practical and applicable to a wider range, the circuit component 3 contacts the output part of the toggle component 1 when the output part of the toggle component 1 moves to the preset position and outputs a corresponding signal.

[0042] In this embodiment, the state feedback component 2 dynamically adjusts the required operating force of the toggle component 1 at each stage of a single operation stroke by being connected to the toggle component 1 during its operation. This provides the pilot with clear operational feedback when operating the toggle component 1. Furthermore, by setting several sets of state feedback components 2 with different action intensities, each control action can be given a unique operating feel, which can assist the pilot in performing precise blind operation control. This allows the pilot to promptly determine whether to continue executing the current control action during the operation stroke. At the same time, by outputting multiple first state feedback signals, multi-segment triggering of feedback signals can be achieved, which can further improve the operating feel and recognition accuracy, making it easier for the pilot to perform various control actions efficiently, thereby effectively improving the safety factor of flight operations.

[0043] Preferably, the state feedback component 2 is provided with a transmission part for transmission connection with the toggle assembly 1, and a driving part for driving the transmission part to move. The transmission part of the state feedback component 2 is transmission connected to the output part of the toggle assembly 1 under the drive of the driving part, and the load of the output part of the toggle assembly 1 is adjusted to realize the output of the first state feedback signal. The intensity of the first state feedback signal is set to be adjustable. In actual operation, the damping of the toggle assembly 1 can be dynamically adjusted by mechanical components, and the damping of the toggle assembly 1 can also be adjusted by electronic control equipment. Both can realize the dynamic state feedback requirements required by this embodiment. For example, the state feedback can be more accurate by adjusting the magnetic force of an electromagnet.

[0044] In specific implementation, the status feedback component 2 is also provided with a reset part for driving the transmission part to reset. The reset part of the status feedback component 2 drives the transmission part of the status feedback component 2 to reset when the toggle component 1 is released.

[0045] Example 2:

[0046] Please see Figures 1 to 6 This embodiment provides a multi-segment triggering flight assistance integrated switch with status feedback function. The similarities with other embodiments will not be repeated. The differences will be described in detail below.

[0047] In this embodiment, the state feedback component 2 includes a feedback pressure plate 21, a drive spring 22, and an adjusting shaft 23. The feedback pressure plate 21 includes a connecting part 211, a rotating part 212, and a transmission part 213 connected in sequence. The free end of the connecting part 211 is detachably in contact with the toggle assembly 1. The rotating part 212 is rotatably arranged on one side of the toggle assembly 1 via the adjusting shaft 23. One end of the drive spring 22 is connected to the rotating part 212, and the other end of the drive spring 22 is connected to the adjusting part of the adjusting shaft 23. The preload of the drive spring 22 is adjustable. In specific implementation, the preload of each drive spring 22 can be adjusted by rotating the adjusting shaft 23, thereby giving each toggle assembly 1 a unique operating feel. When the toggle assembly 1 is activated, the drive spring 22... The connecting part 211 is connected to the toggle assembly 1 and deforms under the drive of the toggle assembly 1. When the output part of the toggle assembly 1 moves to the preset prediction position, the end of the connecting part 211 separates from the toggle assembly 1 to release the transmission part 213. The transmission part 213 is connected to the output part of the toggle assembly 1 under the drive of the drive spring 22 and adjusts the load of the output part of the toggle assembly 1 to realize the output of the first state feedback signal. Preferably, a first reset spring can be provided between the transmission part 213 and the output part of the toggle assembly 1 so that the toggle assembly 1 can be reset under the drive of the drive spring 22 and the first reset spring, and can ensure that the toggle assembly 1 will not produce abnormal noise due to external vibration in the daily standby state, and will not rebound, thus ensuring its stable state.

[0048] In this embodiment, through the cooperation of the feedback pressure plate 21, the drive spring 22 and the adjusting shaft 23, the mechanical operation feedback output and the adjustment of the feedback intensity can be realized without additional electronic components. The feedback is clear, the triggering is stable, the anti-interference ability is strong, and it does not generate electromagnetic interference. It does not affect the flight control, navigation and communication of the flying car. At the same time, the status feedback component 2 and the toggle component 1 are tightly matched and are not affected by the high-frequency vibration of the flying car rotor and the impact of take-off and landing. The operation is highly stable and has a long service life.

[0049] Preferably, to further improve the stability of the triggering of the switch assembly 31, a touch part 214 is also included. The touch part 214 is rotatably limited and mounted on the free end of the transmission part 213. When the transmission part 213 is connected to the toggle assembly 1, the bottom of the touch part 214 abuts against the output part of the toggle assembly 1. When the output part of the toggle assembly 1 moves to the preset control position, the circuit assembly 3 contacts the top of the touch part 214 and outputs a corresponding control signal. Preferably, a second reset spring can be provided between the inner side of the touch part 214 and the free end of the transmission part 213, so that the touch part 214 can also be kept stable before the state feedback assembly 2 is activated, and will not produce abnormal noise due to external vibration.

[0050] In this embodiment, a mounting housing 4 is also included. The status feedback component 2 and the circuit component 3 are both installed within the mounting housing 4. The toggle assembly 1 includes a toggle block 11, a toggle seat 12, and a toggle lever 13. The toggle block 11 is rotatably arranged at the bottom of the interior of the mounting housing 4. One end of the toggle seat 12 is mounted on the toggle block 11, and the other end of the toggle seat 12 extends outward and is detachably connected to the toggle lever 13. In specific implementations, toggle levers 13 of different sizes and shapes can be installed according to the different functions controlled, for example... Figure 2 The toggle lever 13 is shaped like a truncated pyramid. It can also be further improved in terms of recognizability by setting indicator lights, markings and other features. It is convenient to use and easy to assemble. The use of a suitable toggle lever 13 also makes it easy for the pilot to move the toggle assembly 1 when wearing flight gloves. It is not easy to slip and has a comfortable feel.

[0051] Preferably, one side of the mounting housing 4 is provided with a through hole for the operating part of the toggle assembly 1 to be exposed to the outside. The through hole is surrounded by an anti-accidental contact protrusion 431. The connecting end of the operating part of the toggle assembly 1 is arranged inside the anti-accidental contact protrusion 431 to prevent the driver from accidentally touching the adjacent toggle assembly 1 when operating the toggle assembly 1. In this embodiment, the anti-accidental contact protrusion 431 is arranged on the bottom surface of the lower housing 43.

[0052] In practical implementation, both the toggle assembly 1 and the status feedback assembly 2 are provided in several groups. These groups of toggle assemblies 1 and status feedback assemblies 2 are arranged sequentially along the length of the mounting housing 4, resulting in high integration of the flight assistance integrated switch and saving installation steps, thus improving installation efficiency. Please refer to [link / reference needed]. Figure 1 In this embodiment, the mounting housing 4 includes an upper cover plate 41, an upper housing 42, and a lower housing 43. The circuit assembly 3 also includes a circuit board 32. The switch assemblies 31 are all mounted on the circuit board 32. The top of the upper housing 42 has a first mounting groove 421 for the circuit assembly 3 to be installed. The circuit board 32 is also covered with a rubber pad 33 made of silicone rubber, which can improve the protection of the circuit assembly 3. After the circuit board 32 is installed into the first mounting groove 421, the upper cover plate 41 covers the opening of the first mounting groove 421 to complete the assembly of the circuit assembly 3. The bottom of the upper housing 42 has several second mounting grooves 422 for installing the toggle switch block 11 and the status feedback assembly 2, and each second mounting groove 422 is connected to the first mounting groove 421, so that the trigger part of the circuit assembly 3 can be exposed in the second mounting groove 422.

[0053] As a further improvement to this embodiment, in order to increase the compression of the drive spring 22 to further increase the force on the output part of the toggle assembly 1 and improve the driver's perception of the first state feedback signal, an abutment block 111 can be provided at the end of the toggle assembly 1 that contacts the connecting part 211. The abutment block 111 is rotatably mounted on one end of the toggle assembly 1. The outer end of the abutment block 111 abuts against the connecting part 211 when the toggle assembly 1 is reset, and flips under the drive of the connecting part 211. The abutment block 111 flips to a preset position. After being positioned, it separates from the connecting part 211 and is connected to the connecting part 211 in a transmission manner after being reset. The inner end of the abutting block 111 abuts against one end of the toggle assembly 1 when the toggle assembly 1 is activated. During operation, it can ensure that the toggle assembly 1 can be stably reset while extending the transmission stroke, resulting in high working stability. Preferably, a third reset spring can be provided between the bottom surface of the inner end of the abutting block 111 and one end of the toggle assembly 1, so that the abutting block 111 can be reset under the drive of the third reset spring after being separated from the connecting part 211.

[0054] Example 3:

[0055] Please see Figure 5 This embodiment provides a multi-segment triggering flight assistance integrated switch with status feedback function. The similarities with other embodiments will not be repeated. The differences will be described in detail below.

[0056] In this embodiment, the circuit assembly 3 is provided with at least one set of switch assemblies 31, and the switch assembly 31 is provided with at least one control switch 311. When the output part of the toggle assembly 1 is moved to a preset control position, the control switch 311 contacts the output part of the toggle assembly 1 through the transmission assembly and outputs a corresponding control signal.

[0057] Preferably, to further improve the perceptibility of the forecast signal, the switch assembly 31 may also be provided with at least one forecast switch 312. When the output part of the toggle assembly 1 is actuated to the preset forecast position, the forecast switch 312 contacts the output part of the toggle assembly 1 through the transmission component and outputs a corresponding second state feedback signal. In specific implementation, the second state feedback signal can be connected to a corresponding sound module, light-emitting module or display module, etc., and the driver is reminded to pay attention to the control action to be performed by receiving the second state feedback signal and outputting corresponding prompt sound, light signal prompt or information display on the screen.

[0058] In specific implementation, the following can be adopted: Figure 7The simplified circuit shown in this embodiment illustrates that several output ports of circuit component 3 are sequentially connected to several corresponding input ports on the flight control system. Circuit component 3 also includes switches K1, K2, K3, K4, K5, K6, K7, K8, resistors R1, R2, R3, R4, R5, and R6. The first terminal of switch K1 is connected to the power supply, and the second terminal of switch K1 is connected to the flight control degradation prediction port of the flight control system and connected to the flight control degradation control port of the flight control system through switch K2. The first terminal of switch K3 is grounded and connected to the first terminal of resistor R1. The second terminal of switch K3 is connected to the automatic flight prediction port of the flight control system through resistor R2 and connected to the automatic flight control port of the flight control system through switch K4. The second terminal of resistor R1 is connected to the automatic flight prediction port of the flight control system. The first terminal of switch K5 is grounded and connected to the first terminal of resistor R3. The system is configured with the following connections: the second terminal of switch K5 is connected to the alarm termination / page-turning signal prediction port of the flight control system via resistor R4, and to the alarm termination / page-turning signal control port of the flight control system via switch K6; the second terminal of resistor R3 is connected to the alarm termination / page-turning signal prediction port of the flight control system; the first and third terminals of switch K7 are both grounded and connected to the first terminal of resistor R5; the second terminal of switch K7 is connected to the power-on / off switch signal prediction port of the flight control system via resistor R6, and to the power-on / off switch signal control port of the flight control system via switch K8; the second terminal of resistor R5 is connected to the power-on / off switch signal prediction port of the flight control system; and the fourth terminal of switch K7 is connected to the battery wake-up signal control port of the flight control system. During operation, the control signal output is triggered by the sequential closing of multiple switches. Even in harsh environments with strong signal interference, erroneous signal output can be effectively avoided, thereby greatly improving the safety factor of flight operations. In this embodiment, by setting the forecast switch 312, an electrical signal feedback can be output synchronously when the output part of the toggle assembly 1 moves to the preset forecast position. This allows the electrical signal feedback to trigger the corresponding sound forecast or light forecast, making it easier for the pilot to judge whether the current operation needs to continue, avoiding misoperation, and thus further improving the safety factor of flight operations.

[0059] The beneficial technical effects of this embodiment include: the present invention dynamically adjusts the magnitude of the operating force required by the toggle assembly at each stage of a single operation stroke by means of a state feedback component that is connected to the toggle assembly during the operation of the toggle assembly, thereby providing the pilot with clear operation feedback when operating the toggle assembly. Furthermore, by setting several sets of state feedback components with different action intensities, each control action can be given a unique operating feel, which can assist the pilot in performing precise blind operation control. This allows the pilot to promptly determine whether to continue executing the current control action during the operation stroke. At the same time, by outputting multiple first state feedback signals to achieve multi-segment triggering of feedback signals, the operating feel and recognition accuracy can be further improved, making it easier for the pilot to perform various control actions efficiently, thereby effectively improving the safety factor of flight operations.

[0060] The above description is merely a specific embodiment of the present invention, but the scope of protection of the present invention is not limited thereto. Those skilled in the art should understand that the present invention includes, but is not limited to, the contents described in the accompanying drawings and the specific embodiments above. Any modifications that do not depart from the functional and structural principles of the present invention will be included within the scope of the claims.

Claims

1. A multi-segment triggered flight assistance integrated switch with status feedback function, characterized in that, include: A toggle assembly (1) is provided for the driver to toggle to trigger the corresponding switch assembly (31) to output a signal; The status feedback component (2) is used to output a first status feedback signal to the driver when the output part of the toggle component (1) moves to a preset prediction position; Circuit component (3) is used to output corresponding signals under the drive of toggle component (1); The triggering part of the state feedback component (2) is connected to the toggle component (1). When the output part of the toggle component (1) moves to the preset prediction position, the state feedback component (2) is activated. When the state feedback component (2) is activated, it is connected to the output part of the toggle component (1) and outputs at least one first state feedback signal. When the output part of the toggle component (1) moves to the preset position, the circuit component (3) contacts the output part of the toggle component (1) and outputs a corresponding signal. The status feedback component (2) includes a feedback pressure plate (21), a drive spring (22), and an adjusting shaft (23). The feedback pressure plate (21) includes a connecting part (211), a rotating part (212), and a transmission part (213) connected in sequence. The free end of the connecting part (211) is detachably in contact with the toggle assembly (1). The rotating part (212) is rotatably arranged on one side of the toggle assembly (1) via the adjusting shaft (23). One end of the drive spring (22) is connected to the rotating part (212), and the other end of the drive spring (22) is connected to the adjusting part of the adjusting shaft (23). The preload of the driving spring (22) is adjustable. When the toggle assembly (1) is activated, the driving spring (22) is connected to the toggle assembly (1) via the connecting part (211) and deforms under the drive of the toggle assembly (1). When the output part of the toggle assembly (1) moves to the preset prediction position, the end of the connecting part (211) separates from the toggle assembly (1) to release the transmission part (213). The transmission part (213) is connected to the output part of the toggle assembly (1) under the drive of the driving spring (22) and adjusts the load of the output part of the toggle assembly (1) to realize the output of the first state feedback signal.

2. The multi-segment triggering flight assistance integrated switch with status feedback function according to claim 1, characterized in that: The state feedback component (2) is provided with a transmission part for transmission connection with the toggle assembly (1) and a driving part for driving the transmission part to move. The transmission part of the state feedback component (2) is driven by the driving part to be transmission connected to the output part of the toggle assembly (1) and the load of the output part of the toggle assembly (1) is adjusted to realize the output of the first state feedback signal. The intensity of the first state feedback signal is set to be adjustable.

3. The multi-segment triggering flight assistance integrated switch with status feedback function according to claim 2, characterized in that: The status feedback component (2) is further provided with a reset part for driving the transmission part to reset. The reset part of the status feedback component (2) drives the transmission part of the status feedback component (2) to reset when the toggle component (1) is released.

4. The multi-segment triggering flight assistance integrated switch with status feedback function according to claim 1, characterized in that: It also includes a touch part (214), which is rotatably limited and mounted on the free end of the transmission part (213). When the transmission part (213) is connected to the output part of the toggle assembly (1), the bottom of the touch part (214) abuts against the output part of the toggle assembly (1). When the output part of the toggle assembly (1) moves to the preset control position, the circuit assembly (3) contacts the top of the touch part (214) and outputs a corresponding control signal.

5. A multi-segment triggered flight assistance integrated switch with status feedback function according to claim 1, characterized in that: The end of the toggle assembly (1) that contacts the connecting part (211) is provided with an abutting rotating block (111). The abutting rotating block (111) is rotatably installed at one end of the toggle assembly (1). The outer end of the abutting rotating block (111) abuts against the connecting part (211) when the toggle assembly (1) is reset, and flips under the drive of the connecting part (211). After flipping to a preset position, the abutting rotating block (111) separates from the connecting part (211) and is connected to the connecting part (211) after being reset. The inner end of the abutting rotating block (111) abuts against one end of the toggle assembly (1) when the toggle assembly (1) is activated.

6. The multi-segment triggered flight assistance integrated switch with status feedback function according to claim 1, characterized in that: The circuit assembly (3) is provided with at least one set of switch assemblies (31), and the switch assembly (31) is provided with at least one control switch (311). When the output part of the toggle assembly (1) moves to the preset control position, the control switch (311) contacts the output part of the toggle assembly (1) through the transmission assembly and outputs a corresponding control signal.

7. A multi-segment triggered flight assistance integrated switch with status feedback function according to claim 6, characterized in that: The switch assembly (31) is further provided with at least one forecast switch (312). When the output part of the toggle assembly (1) moves to the preset forecast position, the forecast switch (312) contacts the output part of the toggle assembly (1) through the transmission assembly and outputs a corresponding second state feedback signal.

8. A multi-segment triggered flight assistance integrated switch with status feedback function according to claim 1, characterized in that: The toggle assembly (1) is provided with a toggle seat (12) and a toggle lever (13) for the driver to toggle. The toggle lever (13) is detachably mounted on the toggle seat (12), and the shape and size of the toggle lever (13) are adjustable.

9. A multi-segment triggered flight assistance integrated switch with status feedback function according to claim 1, characterized in that: It also includes a mounting housing (4), in which the status feedback component (2) and the circuit component (3) are both installed. One side of the mounting housing (4) is provided with a through hole for the operating part of the toggle assembly (1) to be exposed to the outside. The through hole is surrounded by an anti-accidental touch protrusion (431), and the connection end of the operating part of the toggle assembly (1) is arranged inside the anti-accidental touch protrusion (431).

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