CN205679930U - A kind of aircraft power plant complex control system testing stand - Google Patents
A kind of aircraft power plant complex control system testing stand Download PDFInfo
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- CN205679930U CN205679930U CN201620518405.9U CN201620518405U CN205679930U CN 205679930 U CN205679930 U CN 205679930U CN 201620518405 U CN201620518405 U CN 201620518405U CN 205679930 U CN205679930 U CN 205679930U
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Abstract
The utility model discloses a kind of aircraft power plant complex control system testing stand.Described aircraft power plant complex control system testing stand includes: main frame assembly, is provided with interface plug；Avionics and outside simulator, it is arranged on main frame assembly；Display, it is arranged on described main frame assembly；Plug-in display, plug-in display is connected with described main frame assembly by suspension strut structure；Accelerator control device, it is arranged on described main frame assembly；Shutdown handle, it is arranged on described main frame assembly；Passenger cabin top panel emulator, it is arranged on described main frame assembly.This utility model provides a kind of aircraft power plant complex control system testing stand, this testing stand by himself can by aircraft avionics, fly the systems such as control, undercarriage and cross-linked by interface, hand over defeated by the signal between each system, thus provide condition for complete machine power set complex control system and crosslinking assays thereof.
Description
Technical field
This utility model relates to aircraft power plant experimental technique field, particularly relates to a kind of aircraft power plant comprehensive
Control system testing stand.
Background technology
Modern aeroengine complex control system is developed into the complete of advanced person by original hydromechanical control system
Authority digital motive complex control system (FADEC).At present, complete machine power set complex control system and crosslinking thereof are related to
The testing equipment of test still belongs to blank.
In prior art, do not have a kind of testing stand can comprehensive each airborne equipment, and by these equipment and aircraft avionics,
Fly the systems such as control, undercarriage to be cross-linked by interface, hand over defeated by the signal between each system.
Thus, it is desirable to have a kind of technical scheme overcomes or at least alleviates at least one drawbacks described above of prior art.
Utility model content
The purpose of this utility model is to provide a kind of aircraft power plant complex control system testing stand to overcome or extremely
Alleviate at least one drawbacks described above of prior art less.
For achieving the above object, this utility model provides a kind of aircraft power plant complex control system testing stand, institute
State aircraft power plant complex control system testing stand to include: main frame assembly, described main frame assembly is provided with interface and inserts
Head；Avionics and outside simulator, described avionics and outside simulator are arranged on main frame assembly；Display, described aobvious
Show that device is arranged on described main frame assembly；Plug-in display, described plug-in display is by suspension strut structure and described master
Body frame assembly connects；Accelerator control device, described accelerator control device is arranged on described main frame assembly；Shutdown handle, institute
State shutdown handle to be arranged on described main frame assembly；Passenger cabin top panel emulator, described passenger cabin top panel emulator sets
Put on described main frame assembly.
Preferably, described main frame assembly includes: support cabinet, described support cabinet be arranged on ground or on the basis of, described
Supporting and be cashier's office in a shop provided with holding tank, described avionics and outside simulator are arranged in described holding tank.
Preferably, described support cabinet extends to the direction away from ground, forms display and accommodates platform, and described display accommodates
Platform includes multiple display holding tank, and the display surface of each display is towards identical.
Preferably, the sidewall of the side of described support cabinet being provided with described suspension strut structure, described suspension strut is tied
Structure is firm shape part, and one end being connected with plug-in display of described suspension strut structure is universal joint such that it is able to make described
Plug-in display rotates around described universal joint.
Preferably, the opposite side bending of described support cabinet extends, and forms shutdown handle and accommodates platform, and described shutdown handle is arranged
Accommodate on platform at described shutdown handle.
Preferably, described support cabinet from the display surface of display towards direction extend, formed throttle platform, described throttle control
Device processed is arranged on described throttle platform.
Preferably, the space that described throttle platform and described shutdown handle accommodate between platform is the first station, described throttle platform
The space of opposite side be the second station.
Preferably, described display accommodate platform to away from support cabinet direction extend, and to the display surface of display towards
Direction bends, and forms passenger cabin top and controls pallet, and described passenger cabin top panel emulator is arranged on described passenger cabin top and controls on pallet.
This utility model provides a kind of aircraft power plant complex control system testing stand, and this testing stand passes through himself
Can by aircraft avionics, fly the systems such as control, undercarriage and cross-linked by interface, hand over defeated by the signal between each system,
Thus provide condition for complete machine power set complex control system and crosslinking assays thereof.
Accompanying drawing explanation
Fig. 1 is the structural representation of the aircraft power plant complex control system testing stand according to this utility model one embodiment
Figure.
Fig. 2 is another structural representation of the aircraft power plant complex control system testing stand shown in Fig. 1.
Reference:
Detailed description of the invention
Clearer, below in conjunction with this utility model for the purpose making this utility model implement, technical scheme and advantage
Accompanying drawing in embodiment, is further described in more detail the technical scheme in this utility model embodiment.In the accompanying drawings, ad initio
Represent same or similar element to same or similar label eventually or there is the element of same or like function.Described reality
Executing example is a part of embodiment of this utility model rather than whole embodiments.The embodiment described below with reference to accompanying drawing
It is exemplary, it is intended to be used for explaining this utility model, and it is not intended that to restriction of the present utility model.New based on this practicality
Embodiment in type, the every other enforcement that those of ordinary skill in the art are obtained under not making creative work premise
Example, broadly falls into the scope of this utility model protection.Below in conjunction with the accompanying drawings embodiment of the present utility model is described in detail.
In description of the present utility model, it is to be understood that term " " center ", " longitudinally ", " laterally ", "front", "rear",
The orientation of the instruction such as "left", "right", " vertically ", " level ", " top ", " end " " interior ", " outward " or position relationship are for based on accompanying drawing institute
The orientation shown or position relationship, be for only for ease of description this utility model and simplify description rather than instruction or hint indication
Device or element must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that to this practicality
The restriction of novel protected scope.
Fig. 1 is the structural representation of the aircraft power plant complex control system testing stand according to this utility model one embodiment
Figure.Fig. 2 is another structural representation of the aircraft power plant complex control system testing stand shown in Fig. 1.
Aircraft power plant complex control system testing stand as shown in Figures 1 and 2 includes main frame assembly, avionics and outer
Portion's simulator, display 1, plug-in display 2, accelerator control device 4, shutdown handle 5 and passenger cabin top panel emulator
6, main frame assembly is provided with interface plug.
Seeing Fig. 1, in the present embodiment, avionics and outside simulator are arranged on main frame assembly；Display 1 is arranged
On main frame assembly；Plug-in display 2 is connected with main frame assembly by suspension strut structure 3；Accelerator control device 4 is arranged
On main frame assembly；Shutdown handle 5 is arranged on main frame assembly；Passenger cabin top panel emulator 6 is arranged on main frame group
On part.
Specifically, in the present embodiment, main frame assembly includes supporting cabinet 7, display accommodates platform 8, shutdown handle accommodates
Platform 9, throttle platform 10 and passenger cabin top control pallet 13.
See Fig. 2, in the present embodiment, support cabinet 7 be arranged on ground or on the basis of, support on cabinet 7 and be provided with receiving
Groove, avionics and outside simulator are arranged in holding tank.Advantageously, in one embodiment, it is provided with outside holding tank
Cabinet door, cabinet door can be closed holding tank, thus enter dust in preventing holding tank.
See Fig. 2, in the present embodiment, support cabinet 7 and extend to the direction away from ground, form display and accommodate platform 8, aobvious
Showing that device accommodates platform 8 and includes multiple display holding tank, the display surface of each display is towards identical.
See Fig. 2, in the present embodiment, the sidewall of the side supporting cabinet 7 is provided with suspension strut structure 3, hangs and prop up
Support structure 3 is firm shape part, and one end being connected with plug-in display 2 of suspension strut structure 3 is universal joint such that it is able to outside making
Hang display 2 to rotate around universal joint.
Seeing Fig. 1 and Fig. 2, in the present embodiment, the opposite side bending supporting cabinet 7 extends, and forms shutdown handle and accommodates platform
9, shutdown handle 5 is arranged on shutdown handle and accommodates on platform 9.It is understood that the cable part of shutdown handle is from shutdown handle
Accommodate under the platform of platform or accommodate platform internal drilling at shutdown handle and pass through.
See Fig. 2, in the present embodiment, support cabinet 7 from the display surface of display towards direction extend (paper in Fig. 2
Vertical outwardly direction), form throttle platform 10, accelerator control device 4 is arranged on throttle platform 10.
Seeing Fig. 1, in the present embodiment, the space that throttle platform 10 and shutdown handle accommodate between platform 9 is the first station 11,
The space of the opposite side of throttle platform is the second station 12.
Increase and have the station that can accommodate worker such that it is able to meet the purpose of man-machine efficacy test.
See Fig. 1, extend to away from the direction supporting cabinet 7 in this example it is shown that device accommodates platform 8, and to display
Display surface direction bending, formed passenger cabin top control pallet 13, passenger cabin top panel emulator 6 be arranged on passenger cabin top control
On pallet 13.
The aircraft power plant complex control system test platform structure of the application rationally, advanced technology, synthesization high, general
Property is strong.System can in the case of non-genuine electromotor, supported whole flight envelope internally-powered apparatus system dynamically and
Steady operation process and with the crosslinking assays of the external system such as avionics and man-machine efficacy test.
Last it is noted that above example is only in order to illustrate the technical solution of the utility model, rather than it is limited
System.Although being described in detail this utility model with reference to previous embodiment, those of ordinary skill in the art should manage
Solve: the technical scheme described in foregoing embodiments still can be modified by it, or enters wherein portion of techniques feature
Row equivalent；And these amendments or replacement, do not make the essence of appropriate technical solution depart from each embodiment of this utility model
The spirit and scope of technical scheme.
Claims (8)
1. an aircraft power plant complex control system testing stand, it is characterised in that described aircraft power plant Comprehensive Control
Systems test bed includes:
Main frame assembly, described main frame assembly is provided with interface plug；
Avionics and outside simulator, described avionics and outside simulator are arranged on main frame assembly；
Display (1), described display (1) is arranged on described main frame assembly；
Plug-in display (2), described plug-in display (2) is connected with described main frame assembly by suspension strut structure (3)；
Accelerator control device (4), described accelerator control device (4) is arranged on described main frame assembly；
Shutdown handle (5), described shutdown handle (5) is arranged on described main frame assembly；
Passenger cabin top panel emulator (6), described passenger cabin top panel emulator (6) is arranged on described main frame assembly.
2. aircraft power plant complex control system testing stand as claimed in claim 1, it is characterised in that described main frame group
Part includes:
Support cabinet (7), described support cabinet (7) be arranged on ground or on the basis of, described support cabinet (7) is provided with holding tank,
Described avionics and outside simulator are arranged in described holding tank.
3. aircraft power plant complex control system testing stand as claimed in claim 2, it is characterised in that described support cabinet
(7) extending to the direction away from ground, form display and accommodate platform (8), described display accommodates platform (8) and includes multiple display
Holding tank, the display surface of each display is towards identical.
4. aircraft power plant complex control system testing stand as claimed in claim 3, it is characterised in that described support cabinet
(7) being provided with described suspension strut structure (3) on the sidewall of side, described suspension strut structure (3) is firm shape part, described outstanding
The one end being connected with plug-in display (2) hanging supporting construction (3) is universal joint such that it is able to make described plug-in display
(2) rotate around described universal joint.
5. aircraft power plant complex control system testing stand as claimed in claim 4, it is characterised in that described support cabinet
(7) opposite side bending extends, and forms shutdown handle and accommodates platform (9), and described shutdown handle (5) is arranged on described shutdown handle to be held
On Na Tai (9).
6. aircraft power plant complex control system testing stand as claimed in claim 5, it is characterised in that described support cabinet
(7) from the display surface of display towards direction extend, formed throttle platform (10), described accelerator control device (4) is arranged on institute
State on throttle platform (10).
7. aircraft power plant complex control system testing stand as claimed in claim 6, it is characterised in that described throttle platform
(10) space and between described shutdown handle receiving platform (9) is the first station (11), the space of the opposite side of described throttle platform
It is the second station (12).
8. aircraft power plant complex control system testing stand as claimed in claim 7, it is characterised in that described display holds
Na Tai (8) extends to away from the direction supporting cabinet (7), and bends to the display surface direction of display, forms the control of passenger cabin top
Making sheet platform (13), described passenger cabin top panel emulator (6) is arranged on described passenger cabin top and controls on pallet (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620518405.9U CN205679930U (en) | 2016-05-31 | 2016-05-31 | A kind of aircraft power plant complex control system testing stand |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620518405.9U CN205679930U (en) | 2016-05-31 | 2016-05-31 | A kind of aircraft power plant complex control system testing stand |
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| Publication Number | Publication Date |
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| CN205679930U true CN205679930U (en) | 2016-11-09 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201620518405.9U Active CN205679930U (en) | 2016-05-31 | 2016-05-31 | A kind of aircraft power plant complex control system testing stand |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106769068A (en) * | 2016-12-15 | 2017-05-31 | 中国航空工业集团公司西安飞机设计研究所 | A kind of aircraft engine loads Servo simulation test method |
| CN108983756A (en) * | 2018-08-17 | 2018-12-11 | 国营芜湖机械厂 | A kind of avionics flight control system floor synthetic debugging verification platform |
| CN109637254A (en) * | 2019-01-22 | 2019-04-16 | 大连海事大学 | A kind of overboard escape training device of helicopter |
-
2016
- 2016-05-31 CN CN201620518405.9U patent/CN205679930U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106769068A (en) * | 2016-12-15 | 2017-05-31 | 中国航空工业集团公司西安飞机设计研究所 | A kind of aircraft engine loads Servo simulation test method |
| CN108983756A (en) * | 2018-08-17 | 2018-12-11 | 国营芜湖机械厂 | A kind of avionics flight control system floor synthetic debugging verification platform |
| CN108983756B (en) * | 2018-08-17 | 2021-07-13 | 国营芜湖机械厂 | Avionics flight control system ground comprehensive debugging and verification platform |
| CN109637254A (en) * | 2019-01-22 | 2019-04-16 | 大连海事大学 | A kind of overboard escape training device of helicopter |
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