CN203013017U - Distributed-type non-avionic simulation excitation system - Google Patents
Distributed-type non-avionic simulation excitation system Download PDFInfo
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- CN203013017U CN203013017U CN 201220651906 CN201220651906U CN203013017U CN 203013017 U CN203013017 U CN 203013017U CN 201220651906 CN201220651906 CN 201220651906 CN 201220651906 U CN201220651906 U CN 201220651906U CN 203013017 U CN203013017 U CN 203013017U
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- simulation excitation
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- emulation excitation
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Abstract
The utility model provides a distributed-type non-avionic simulation excitation system. According to the distributed-type non-avionic simulation excitation system, various non-avionics simulation excitation devices are connected with a front-end machine (1) through an optical fiber network so as to form the whole distributed-type non-avionic simulation excitation system. The non-avionic simulation excitation devices comprise the following components of: an electromechanical system simulator (2), a flight control system simulator (3), a weapon simulator (4), a sensor A actuator (5), and a sensor B actuator (6); and the non-avionic simulation excitation devices are also connected with an avionics system (7). According to the distributed-type non-avionic simulation excitation system of the utility model, the front end machine (1) is adopted to set each non-avionic simulation excitation device in a unified manner; each set parameter is of high concurrency, so that each non-avionic simulation excitation devices can provide highly synchronous simulation excitation signals for the avionics system according to unified and real time setting; various kinds of non-avionic simulation excitation device signals are synchronously set on one interface, such that testing work can be facilitated.
Description
Technical field
The utility model relates to distributed non-avionics emulation excitation system global design and applied technical field, and a kind of distributed non-avionics emulation excitation system is provided especially.
Background technology
In prior art, in the test of Aircraft electric system, emulator, the driver of these non-avionics systems of driver of Mechano-Electronic System Simulation device, flight control system emulator, weapon simulation device, each sensor are discrete, and parameters, can not provide concurrent simulate signal respectively.Just comprehensively the non-avionics environment of simulated aircraft (such as: when checking the following function of avionics system: the parameter of fuel system and flight control system changes simultaneously, see that avionics system is to the reaction of this variation-demonstration, record etc.), make the avionics test not comprehensive, need to wait until that non-avionics real equipment participates in into just can carrying out afterwards, increase the weight of the burden that the later stage checks.
People expect to obtain better distributed non-avionics emulation excitation system of a kind of technique effect.
The utility model content
The purpose of this utility model is to provide better distributed non-avionics emulation excitation system of a kind of technique effect.In order to solve the described problem of background technology part, the utility model has designed a kind of emulation excitation system of non-avionics, and the non-avionics emulation pumping signal of high concurrency can be provided.
A kind of distributed non-avionics emulation excitation system of the utility model, it is characterized in that: described distributed non-avionics emulation excitation system is connected to each non-avionics emulation excitation set on a FEP 1 by fiber optic network, consists of whole distributed non-avionics emulation excitation system; By the unified setting of FEP 1 and the real-time Transmission of fiber optic network, make each emulation excitation set that the emulation pumping signal of high level of synchronization can be provided for avionics system;
Non-avionics emulation excitation set is the combination of following several equipment: Mechano-Electronic System Simulation device 2, flight control system emulator 3, weapon simulation device 4, sensors A driver 5, sensor B driver 6; Above-mentioned non-avionics emulation excitation set also all is connected with avionics system 7.
Described distributed non-avionics emulation excitation system is characterized in that: being used for each non-avionics emulation excitation set is connected to a fiber optic network on test FEP 1 jointly is the Real-time Network network.
Mechano-Electronic System Simulation device 2, flight control system emulator 3, weapon simulation device 4 and each sensor that the utility model utilization is present, be connected by fiber optic network with the FEP 1 of responsible unified management, under unified control of FEP 1, complete the real-time setting of various non-avionics emulation excitation sets.
Concrete connected mode is: FEP 1 adopts common computer, and configuration optical fiber network interface card, and FEP 1 and each emulator, driver are connected on the fiber optic network switch.
Compared with prior art, the advantage and the effect that have of the utility model:
1) owing to adopting fiber optic network, and adopt the unified setting of 1 pair of each emulation excitation set of FEP, and the real-time Transmission of fiber optic network, make each parameters have very high concurrency, make each emulation excitation set according to unified real-time setting, provide the emulation pumping signal of high level of synchronization for avionics system.
2) various non-avionics emulation excitation set signals are set simultaneously on an interface, bring convenience to test job.
Description of drawings
Below in conjunction with drawings and the embodiments, the utility model is described in further detail:
Fig. 1 is that figure is seen in distributed non-avionics emulation excitation system principle of compositionality signal.
Embodiment
Embodiment 1
A kind of distributed non-avionics emulation excitation system, it is connected to each non-avionics emulation excitation set on a FEP 1 by fiber optic network, consists of whole distributed non-avionics emulation excitation system; By the unified setting of FEP 1 and the real-time Transmission of fiber optic network, make each emulation excitation set that the emulation pumping signal of high level of synchronization can be provided for avionics system;
Non-avionics emulation excitation set is the combination of following several equipment: Mechano-Electronic System Simulation device 2, flight control system emulator 3, weapon simulation device 4, sensors A driver 5, sensor B driver 6; Above-mentioned non-avionics emulation excitation set also all is connected with avionics system 7.
Described distributed non-avionics emulation excitation system, being used for each non-avionics emulation excitation set is connected to a fiber optic network on test FEP 1 jointly is the Real-time Network network.
Mechano-Electronic System Simulation device 2, flight control system emulator 3, weapon simulation device 4 and each sensor that the present embodiment utilization is present, be connected by fiber optic network with the FEP 1 of responsible unified management, under unified control of FEP 1, complete the real-time setting of various non-avionics emulation excitation sets.
Concrete connected mode is: FEP 1 adopts common computer, and configuration optical fiber network interface card, and FEP 1 and each emulator, driver are connected on the fiber optic network switch.
Compared with prior art, the advantage and the effect that have of the present embodiment:
1) owing to adopting fiber optic network, and adopt the unified setting of 1 pair of each emulation excitation set of FEP, and the real-time Transmission of fiber optic network, make each parameters have very high concurrency, make each emulation excitation set according to unified real-time setting, provide the emulation pumping signal of high level of synchronization for avionics system.
2) various non-avionics emulation excitation set signals are set simultaneously on an interface, bring convenience to test job.
Claims (2)
1. distributed non-avionics emulation excitation system, it is characterized in that: described distributed non-avionics emulation excitation system is connected to each non-avionics emulation excitation set on a FEP (1) by fiber optic network, consists of whole distributed non-avionics emulation excitation system;
Non-avionics emulation excitation set is the combination of following several equipment: Mechano-Electronic System Simulation device (2), flight control system emulator (3), weapon simulation device (4), sensors A driver (5), sensor B driver (6);
Above-mentioned non-avionics emulation excitation set also all is connected with avionics system (7).
2. according to the described distributed non-avionics emulation excitation system of claim 1, it is characterized in that: the fiber optic network that is used for each non-avionics emulation excitation set is connected on a test FEP (1) jointly is the Real-time Network network.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220651906 CN203013017U (en) | 2012-11-30 | 2012-11-30 | Distributed-type non-avionic simulation excitation system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220651906 CN203013017U (en) | 2012-11-30 | 2012-11-30 | Distributed-type non-avionic simulation excitation system |
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| CN203013017U true CN203013017U (en) | 2013-06-19 |
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| CN 201220651906 Expired - Lifetime CN203013017U (en) | 2012-11-30 | 2012-11-30 | Distributed-type non-avionic simulation excitation system |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103760439A (en) * | 2013-09-24 | 2014-04-30 | 中国航空工业集团公司沈阳飞机设计研究所 | Automatic test system of avionic system |
| CN105590495A (en) * | 2016-03-18 | 2016-05-18 | 中国直升机设计研究所 | Reconfigurable avionics system training simulator |
| CN111208744A (en) * | 2019-12-27 | 2020-05-29 | 中国航空工业集团公司西安飞机设计研究所 | Central alarm verification method under comprehensive modular avionics architecture |
-
2012
- 2012-11-30 CN CN 201220651906 patent/CN203013017U/en not_active Expired - Lifetime
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103760439A (en) * | 2013-09-24 | 2014-04-30 | 中国航空工业集团公司沈阳飞机设计研究所 | Automatic test system of avionic system |
| CN103760439B (en) * | 2013-09-24 | 2016-04-06 | 中国航空工业集团公司沈阳飞机设计研究所 | A kind of Auto-Test System of avionics system |
| CN105590495A (en) * | 2016-03-18 | 2016-05-18 | 中国直升机设计研究所 | Reconfigurable avionics system training simulator |
| CN105590495B (en) * | 2016-03-18 | 2019-05-07 | 中国直升机设计研究所 | A kind of restructural avionics system training simulators |
| CN111208744A (en) * | 2019-12-27 | 2020-05-29 | 中国航空工业集团公司西安飞机设计研究所 | Central alarm verification method under comprehensive modular avionics architecture |
| CN111208744B (en) * | 2019-12-27 | 2022-09-20 | 中国航空工业集团公司西安飞机设计研究所 | Central alarm verification method under comprehensive modular avionics architecture |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
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| CX01 | Expiry of patent term |
Granted publication date: 20130619 |