Aviation three-mode illuminating lamp control device
By designing the aviation three-mode lighting control device, the signal is used to control the on- and switching of aviation white, night vision green A and red internal modes, the wrong lighting problem caused by misoperation in traditional aircraft lighting systems is solved, and a safe and reliable three-mode lighting switching is achieved.
Patent Information
- Application Number
- CN202420914906.3
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-04-29
- Publication Date
- 2025-03-11
- Estimated Expiration
- 2034-04-29
AI Technical Summary
Traditional aircraft lighting systems are difficult to prevent the pilot from operating incorrectly in the use environment of special aircraft, causing the wrong lighting to be turned on, and cannot meet the lighting needs in different combat situations.
Design an aviation three-mode lighting control device to control the turn-on and switch of three lighting modes (aviation white, night vision green A, infrared mode) through the lighting controller receiving different signals (such as "ground" or "hanging" signals, "28V" signals) to ensure the safety and accuracy of the lighting mode.
The three-mode aerial lighting ceiling lights are realized, which effectively prevents incorrect lighting caused by misoperation and meets the lighting needs in different combat situations.
Smart Images
Figure CN222602632U_ABST
Abstract
Description
Technical Field
[0001] The utility model belongs to the field of aviation electrical technology, relates to an aviation lighting project, and specifically relates to an aviation three-mode lighting lamp control device. Background Art
[0002] Aircraft lighting systems include aircraft cabin lighting, cockpit lighting, and non-external lighting. In traditional aircraft lighting systems, the cabin and cockpit lighting ceiling lights are mostly aviation white lighting. In the use environment of special aircraft, not only general white light lighting is required, but also some lighting requirements in special environments, mainly night vision lighting and infrared lighting. Aviation white is used for daily lighting, NVIS green A lighting is used for night vision and night combat lighting, and infrared lighting is used for combat lighting behind enemy lines, meeting the cabin lighting in different combat situations.
[0003] Traditionally, light switching is operated by using different switches, or by switching a single switch multiple times. However, this is not allowed in the operating environment of special aircraft. It is necessary to strictly prevent the wrong switch from being turned on due to the pilot's misoperation, thereby turning on the wrong light. Utility Model Content
[0004] In order to solve the above problems, the utility model provides an aviation three-mode lighting control device to control lighting with three modes. The lighting controller can turn on / off the ceiling lights in groups. When the lighting controller receives a "ground" or "suspended" signal, it is aviation white. In this state, night vision-compatible NVIS green A lighting and infrared lighting are not available. When the lighting controller receives a "28V" signal, it defaults to NVIS green A lighting. In this state, infrared lighting can be manually selected through the lighting controller.
[0005] The technical solution of the utility model is as follows:
[0006] An aviation three-mode lighting control device includes a lighting control box, two sockets of the lighting control box are connected to an onboard power supply, the lighting control box has connectors for three lighting modes, which are respectively connected to three lighting mode input interfaces of a three-mode ceiling light, and the lighting control box is also provided with a mode switching connector and a concealed mode output connector.
[0007] Furthermore, the connectors of the three lighting modes of the lighting control box are respectively an aviation white output connector, a night vision green A output connector, and an infrared mode output connector, and the three connectors are respectively connected to the three lighting mode input interfaces of the three-mode ceiling light.
[0008] Furthermore, the three lighting mode input interfaces of the three-mode ceiling light have at least two and are divided into two groups. The aviation white output connector, the night vision green A output connector, and the infrared mode output connector of the lighting control box each have two and are divided into two groups. The two groups of three-mode connectors of the lighting control box are respectively connected to a group of three-mode ceiling lights, and the same group of three-mode ceiling lights are connected in parallel.
[0009] Furthermore, when the lighting controller is connected to the "ground" or "floating" signal terminal, the aviation white output connector is connected to the three-mode ceiling light, and the night vision green A output connector and the infrared mode output connector are disconnected from the three-mode ceiling light.
[0010] Further, when the lighting controller is connected to the "28V" signal terminal, the night vision green A output connector or the infrared mode output connector is connected to the three-mode ceiling light.
[0011] Furthermore, the mode switching connector is connected to a switching button, and the switching button controls the switching of the night vision green A output connector or the infrared mode output connector to connect with the three-mode ceiling light.
[0012] Further, when the infrared mode output connector is connected to the three-mode ceiling light, the connector for the concealed mode output is connected to the rear end.
[0013] The beneficial effects of the utility model are as follows:
[0014] The utility model supports the operation and switching of the three-mode aviation lighting ceiling light, and can effectively prevent the turning on of the aviation white light due to misoperation during the flight mission. BRIEF DESCRIPTION OF THE DRAWINGS
[0015] In order to more clearly illustrate the technical solution of the implementation method of the utility model patent, the following is a brief introduction to the drawings required for use in the implementation method. It should be understood that the following drawings only show certain embodiments of the utility model patent and should not be regarded as limiting the scope. For ordinary technicians in this field, other relevant drawings can be obtained based on these drawings without paying creative work.
[0016] Figure 1 It is a schematic diagram of the aviation three-mode lighting control device of the present utility model. DETAILED DESCRIPTION
[0017] This section is an embodiment of the utility model, which is used to explain and illustrate the technical solution of the utility model. In the absence of conflict, the embodiments of the utility model and the features in the embodiments can be combined with each other.
[0018] In the description of the present utility model, it is necessary to understand that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside" and the like indicating directions or positional relationships are based on the orientations or positional relationships of the accompanying drawings, and are only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or case referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on the present utility model. In addition, the terms "first", "second", etc. are only used for descriptive purposes, and cannot be understood as indicating or implying relative importance or implying the number of technical features indicated. Thus, features defined as "first", "second", etc. may explicitly or implicitly include more of the features. In the description of the present utility model, unless otherwise specified, "multiple" means two or more.
[0019] In the description of the present utility model, it should be noted that, unless otherwise clearly specified and limited, the terms "installation", "connection" and "connection" should be interpreted in a broad sense, for example, it can be a fixed connection, a detachable connection or an integrated connection; it can be a mechanical connection or a point connection; it can be a direct connection or an indirect connection 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 utility model can be understood by specific circumstances.
[0020] Embodiment 1:
[0021] An aviation three-mode lighting control device includes a lighting control box, two sockets of the lighting control box are connected to an onboard power supply, the lighting control box has connectors for three lighting modes, which are respectively connected to three lighting mode input interfaces of a three-mode ceiling light, and the lighting control box is also provided with a mode switching connector and a concealed mode output connector.
[0022] The connectors of the three lighting modes of the lighting control box are respectively aviation white output connector, night vision green A output connector, and infrared mode output connector. The three connectors are respectively connected to the three lighting mode input interfaces of the three-mode ceiling light.
[0023] The three lighting mode input interfaces of the three-mode ceiling light have at least two and are divided into two groups. The aviation white output connector, night vision green A output connector and infrared mode output connector of the lighting control box each have two and are divided into two groups. The two groups of three-mode connectors of the lighting control box are respectively connected to a group of three-mode ceiling lights, and the same group of three-mode ceiling lights are connected in parallel.
[0024] When the lighting controller is connected to the "ground" or "floating" signal terminal, the aviation white output connector is connected to the three-mode ceiling light, and the night vision green A output connector and the infrared mode output connector are disconnected from the three-mode ceiling light.
[0025] When the lighting controller is connected to the "28V" signal terminal, the night vision green A output connector or the infrared mode output connector is connected to the three-mode ceiling light.
[0026] The mode switching connector is connected to the switching button, and the switching button controls the switching of the night vision green A output connector or the infrared mode output connector to connect with the three-mode ceiling light.
[0027] When the infrared mode output connector is connected to the three-mode ceiling light, the connector of the concealed mode output is connected to the rear end.
[0028] Embodiment 2:
[0029] The utility model is further described in detail below in conjunction with the accompanying drawings and specific implementation methods: Figure 1 This is a circuit cross-link diagram.
[0030] When the lighting controller receives a "ground" or "floating" signal, the three-mode lighting ceiling light is aviation white. In this state, night vision-compatible NVIS green A lighting and infrared lighting are not available; when the lighting controller receives a "28V" signal, the three-mode lighting ceiling light defaults to NVIS green A lighting. In this state, the lighting controller can be manually switched to infrared lighting (stealth mode).
[0031] Finally, it should be noted that the above embodiments are only used to illustrate the technical solution of the utility model, but the protection scope of the utility model is not limited thereto. Any technician familiar with the field can easily think of various equivalent modifications or substitutions within the technical scope disclosed in the utility model, and these modifications or substitutions should be included in the protection scope of the utility model.
Claims
1. An aviation three-mode lighting control device, characterized in that: It includes a lighting control box, two sockets of which are connected to an onboard power supply. The lighting control box has connectors for three lighting modes, which are respectively connected to three lighting mode input interfaces of the three-mode ceiling light. The lighting control box is also provided with a mode switching connector and a concealed mode output connector.
2. The aviation three-mode lighting control device according to claim 1, characterized in that: The connectors of the three lighting modes of the lighting control box are respectively aviation white output connector, night vision green A output connector, and infrared mode output connector. The three connectors are respectively connected to the three lighting mode input interfaces of the three-mode ceiling light.
3. The aviation three-mode lighting control device according to claim 2, characterized in that: The three lighting mode input interfaces of the three-mode ceiling light have at least two and are divided into two groups. The aviation white output connector, night vision green A output connector and infrared mode output connector of the lighting control box each have two and are divided into two groups. The two groups of three-mode connectors of the lighting control box are respectively connected to a group of three-mode ceiling lights, and the same group of three-mode ceiling lights are connected in parallel.
4. The aviation three-mode lighting control device according to claim 2, characterized in that: When the lighting controller is connected to the "ground" or "floating" signal terminal, the aviation white output connector is connected to the three-mode ceiling light, and the night vision green A output connector and the infrared mode output connector are disconnected from the three-mode ceiling light.
5. The aviation three-mode lighting control device according to claim 2, characterized in that: When the lighting controller is connected to the "28V" signal terminal, the night vision green A output connector or the infrared mode output connector is connected to the three-mode ceiling light.
6. The aviation three-mode lighting control device according to claim 5, characterized in that: The mode switching connector is connected to the switching button, and the switching button controls the switching of the night vision green A output connector or the infrared mode output connector to connect with the three-mode ceiling light.
7. The aviation three-mode lighting control device according to claim 1, characterized in that: When the infrared mode output connector is connected to the three-mode ceiling light, the connector of the concealed mode output is connected to the rear end.