CN203601582U - Plane loading simulator - Google Patents
Plane loading simulator Download PDFInfo
- Publication number
- CN203601582U CN203601582U CN201320737196.3U CN201320737196U CN203601582U CN 203601582 U CN203601582 U CN 203601582U CN 201320737196 U CN201320737196 U CN 201320737196U CN 203601582 U CN203601582 U CN 203601582U
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- joint
- interface
- switch
- contactless switch
- contact
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Abstract
The utility model provides a plane loading simulator which can conveniently output wheel load aerial or ground simulation control signals according to needs. According to the technical scheme, a first contactor J1 control end, a second contactor J2 control end and a third contactor J3 control end are connected between a power source and the ground in parallel, a change-over switch E1 is connected with among the power source and the first contactor J1 control end, the second contactor J2 control end and the third contactor J3 control end in series, a power good-state switch E2 and a power good-state indicator light K1 are sequentially connected between the power source and the ground in series, and contacts of a change-over light K2 and a third contactor J3 are sequentially connected between the power source and the ground in series.
Description
Technical field
The utility model belongs to change-over swith, relates to a kind of aircraft carrying simulator.
Background technology
Aircraft has very high security and reliability, thus the ground simulation of being everlasting when the state of the related systems such as flight control system, avionics system, Weapon Fire-Control-System after aircraft lift-off, thereby whether consistent with design while checking each system to fly aloft.
Utility model content
The purpose of this utility model is: a kind of aircraft carrying simulator is provided, can exports easily as required wheel load in the air or ground simulation control signal.
The technical solution of the utility model is: a kind of aircraft carrying simulator, comprising:
First interface, the second interface;
Described first interface is provided with A, B, C, D, E, F, G, eight joints of H; Described the second interface is provided with a, b, c, d, e, f, g, eight joints of h;
Described first interface A joint one end is connected with analog machine, and the A joint other end is connected with second interface a joint one end, and the second interface a joint other end is connected with the first jack of the first micro-switch plug of aircraft;
Described first interface B joint one end is connected with analog machine, and the B joint other end is connected with second interface b joint one end, and the second interface b joint other end is connected with the second jack of the first micro-switch plug of aircraft;
Described first interface C joint one end is connected with analog machine, and the C joint other end is connected with second interface c joint one end, and the second interface c joint other end is connected with the 3rd jack of the first micro-switch plug of aircraft;
Described first interface D joint one end is connected with analog machine, and the D joint other end is connected with second interface d joint one end, and the second interface d joint other end is connected with the 4th jack of the first micro-switch plug of aircraft;
Described first interface E joint one end is connected with analog machine, and the E joint other end is connected with second interface e joint one end, and the second interface e joint other end is connected with the first jack of the second micro-switch plug of aircraft;
Described first interface F joint one end is connected with analog machine, and the F joint other end is connected with second interface f joint one end, and the second interface f joint other end is connected with the second jack of the second micro-switch plug of aircraft;
Described first interface G joint one end is connected with analog machine, and the G joint other end is connected with second interface g joint one end, and the second interface g joint other end is connected with the 3rd jack of the second micro-switch plug of aircraft;
Described first interface H joint one end is connected with analog machine, and the H joint other end is connected with second interface h joint one end, and the second interface h joint other end is connected with the 4th jack of the second micro-switch plug of aircraft;
Between first interface A joint and the second interface a joint, be serially connected with the first contact of the first contactless switch;
Between first interface B joint and the second interface b joint, be serially connected with the second contact of the first contactless switch;
Between first interface C joint and the second interface c joint, be serially connected with the 3rd contact of the first contactless switch;
Between first interface D joint and the second interface d joint, be serially connected with the 4th contact of the first contactless switch;
Between first interface E joint and the second interface e joint, be serially connected with the first contact of the second contactless switch;
Between first interface F joint and the second interface f joint, be serially connected with the second contact of the second contactless switch;
Between first interface G joint and the second interface g joint, be serially connected with the 3rd contact of the second contactless switch;
Between first interface H joint and the second interface h joint, be serially connected with the 4th contact of the second contactless switch;
The first contactless switch J1 control end, the second contactless switch J2 control end, the 3rd contactless switch J3 control end are connected in parallel between power supply and ground; Change-over swith E1 is connected between power supply and the first contactless switch J1 control end, the second contactless switch J2 control end, the 3rd contactless switch J3 control end; The good switch E2 of power supply and the good indicator lamp K1 of power supply are connected between power supply and ground successively; The contact of conversion lamp K2 and the 3rd contactless switch J3 is connected between power supply and ground successively.
The advantage that the utility model is created is: can facilitate as required, export accurately aerial or ground wheel load analog control signal.XX type aircraft has increased a front-wheel carrying switch with the XX series aircraft of safeguarding not long ago, and the redundance management, particularly flight control system that have increased control signal require two remaining four-way control signals to have the conformability of height, otherwise just report fault.The simulator of the XX series aircraft of safeguarding not long ago can not meet XX type aircraft utilization requirement; Through using, electric correlation technique can facilitate as required this utility model aircraft carrying simulator from new design, output is accurately aerial or ground wheel load analog control signal.
Accompanying drawing explanation
Fig. 1 is the utility model electrical equipment connection diagram.
The specific embodiment
Below the utility model is described in further details.
A kind of aircraft carrying simulator, as shown in Figure 1, comprising:
First interface, the second interface;
Described first interface is provided with A, B, C, D, E, F, G, eight joints of H; Described the second interface is provided with a, b, c, d, e, f, g, eight joints of h;
Described first interface A joint one end is connected with analog machine, and the A joint other end is connected with second interface a joint one end, and the second interface a joint other end is connected with the first jack of the first micro-switch plug of aircraft;
Described first interface B joint one end is connected with analog machine, and the B joint other end is connected with second interface b joint one end, and the second interface b joint other end is connected with the second jack of the first micro-switch plug of aircraft;
Described first interface C joint one end is connected with analog machine, and the C joint other end is connected with second interface c joint one end, and the second interface c joint other end is connected with the 3rd jack of the first micro-switch plug of aircraft;
Described first interface D joint one end is connected with analog machine, and the D joint other end is connected with second interface d joint one end, and the second interface d joint other end is connected with the 4th jack of the first micro-switch plug of aircraft;
Described first interface E joint one end is connected with analog machine, and the E joint other end is connected with second interface e joint one end, and the second interface e joint other end is connected with the first jack of the second micro-switch plug of aircraft;
Described first interface F joint one end is connected with analog machine, and the F joint other end is connected with second interface f joint one end, and the second interface f joint other end is connected with the second jack of the second micro-switch plug of aircraft;
Described first interface G joint one end is connected with analog machine, and the G joint other end is connected with second interface g joint one end, and the second interface g joint other end is connected with the 3rd jack of the second micro-switch plug of aircraft;
Described first interface H joint one end is connected with analog machine, and the H joint other end is connected with second interface h joint one end, and the second interface h joint other end is connected with the 4th jack of the second micro-switch plug of aircraft;
Between first interface A joint and the second interface a joint, be serially connected with the first contact of the first contactless switch;
Between first interface B joint and the second interface b joint, be serially connected with the second contact of the first contactless switch;
Between first interface C joint and the second interface c joint, be serially connected with the 3rd contact of the first contactless switch;
Between first interface D joint and the second interface d joint, be serially connected with the 4th contact of the first contactless switch;
Between first interface E joint and the second interface e joint, be serially connected with the first contact of the second contactless switch;
Between first interface F joint and the second interface f joint, be serially connected with the second contact of the second contactless switch;
Between first interface G joint and the second interface g joint, be serially connected with the 3rd contact of the second contactless switch;
Between first interface H joint and the second interface h joint, be serially connected with the 4th contact of the second contactless switch;
The first contactless switch J1 control end, the second contactless switch J2 control end, the 3rd contactless switch J3 control end are connected in parallel between power supply and ground; Change-over swith E1 is connected between power supply and the first contactless switch J1 control end, the second contactless switch J2 control end, the 3rd contactless switch J3 control end; The good switch E2 of power supply and the good indicator lamp K1 of power supply are connected between power supply and ground successively; The contact of conversion lamp K2 and the 3rd contactless switch J3 is connected between power supply and ground successively.
Aircraft is aloft under state, change-over swith E1 disconnects, the first contactless switch J1, the second contactless switch J2, the 3rd contactless switch J3 are in off-position, the second contact of the first contactless switch J1, the 4th contact, the second contact of the second contactless switch J2, the 4th closing of contact, the first contact of the first contactless switch J1, the 3rd contact, the first contact of the second contactless switch J2, the 3rd contact open circuit.Conversion lamp K2 extinguishes.
Aircraft is under ground state, change-over swith E1 closure, the first contactless switch J1, the second contactless switch J2, the 3rd contactless switch J3 are in "on" position, the second contact of the first contactless switch J1, the 4th contact, the second contact of the second contactless switch J2, the 4th contact open circuit, the first contact of the first contactless switch J1, the 3rd contact, the first contact of the second contactless switch J2, the 3rd closing of contact.Conversion lamp K2 lights.
The closed K1 lamp of change-over swith E1 is bright, represents that external power source is normal; If the closed K1 of change-over swith E1 does not work, represent external power source mal.
Claims (1)
1. an aircraft carrying simulator, is characterized in that, comprising:
First interface, the second interface;
Described first interface is provided with A, B, C, D, E, F, G, eight joints of H; Described the second interface is provided with a, b, c, d, e, f, g, eight joints of h;
Described first interface A joint one end is connected with analog machine, and the A joint other end is connected with second interface a joint one end, and the second interface a joint other end is connected with the first jack of the first micro-switch plug of aircraft;
Described first interface B joint one end is connected with analog machine, and the B joint other end is connected with second interface b joint one end, and the second interface b joint other end is connected with the second jack of the first micro-switch plug of aircraft;
Described first interface C joint one end is connected with analog machine, and the C joint other end is connected with second interface c joint one end, and the second interface c joint other end is connected with the 3rd jack of the first micro-switch plug of aircraft;
Described first interface D joint one end is connected with analog machine, and the D joint other end is connected with second interface d joint one end, and the second interface d joint other end is connected with the 4th jack of the first micro-switch plug of aircraft;
Described first interface E joint one end is connected with analog machine, and the E joint other end is connected with second interface e joint one end, and the second interface e joint other end is connected with the first jack of the second micro-switch plug of aircraft;
Described first interface F joint one end is connected with analog machine, and the F joint other end is connected with second interface f joint one end, and the second interface f joint other end is connected with the second jack of the second micro-switch plug of aircraft;
Described first interface G joint one end is connected with analog machine, and the G joint other end is connected with second interface g joint one end, and the second interface g joint other end is connected with the 3rd jack of the second micro-switch plug of aircraft;
Described first interface H joint one end is connected with analog machine, and the H joint other end is connected with second interface h joint one end, and the second interface h joint other end is connected with the 4th jack of the second micro-switch plug of aircraft;
Between first interface A joint and the second interface a joint, be serially connected with the first contact of the first contactless switch;
Between first interface B joint and the second interface b joint, be serially connected with the second contact of the first contactless switch;
Between first interface C joint and the second interface c joint, be serially connected with the 3rd contact of the first contactless switch;
Between first interface D joint and the second interface d joint, be serially connected with the 4th contact of the first contactless switch;
Between first interface E joint and the second interface e joint, be serially connected with the first contact of the second contactless switch;
Between first interface F joint and the second interface f joint, be serially connected with the second contact of the second contactless switch;
Between first interface G joint and the second interface g joint, be serially connected with the 3rd contact of the second contactless switch;
Between first interface H joint and the second interface h joint, be serially connected with the 4th contact of the second contactless switch;
The first contactless switch J1 control end, the second contactless switch J2 control end, the 3rd contactless switch J3 control end are connected in parallel between power supply and ground; Change-over swith E1 is connected between power supply and the first contactless switch J1 control end, the second contactless switch J2 control end, the 3rd contactless switch J3 control end; The good switch E2 of power supply and the good indicator lamp K1 of power supply are connected between power supply and ground successively; The contact of conversion lamp K2 and the 3rd contactless switch J3 is connected between power supply and ground successively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320737196.3U CN203601582U (en) | 2013-11-19 | 2013-11-19 | Plane loading simulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320737196.3U CN203601582U (en) | 2013-11-19 | 2013-11-19 | Plane loading simulator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203601582U true CN203601582U (en) | 2014-05-21 |
Family
ID=50714270
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320737196.3U Expired - Fee Related CN203601582U (en) | 2013-11-19 | 2013-11-19 | Plane loading simulator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203601582U (en) |
-
2013
- 2013-11-19 CN CN201320737196.3U patent/CN203601582U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140521 Termination date: 20161119 |