CN108447334A - A kind of flight control system transmission parts dismounting calibration training system - Google Patents
A kind of flight control system transmission parts dismounting calibration training system Download PDFInfo
- Publication number
- CN108447334A CN108447334A CN201810306205.0A CN201810306205A CN108447334A CN 108447334 A CN108447334 A CN 108447334A CN 201810306205 A CN201810306205 A CN 201810306205A CN 108447334 A CN108447334 A CN 108447334A
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- China
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- transmission parts
- fixed
- flight control
- control system
- rudder face
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
Abstract
A kind of flight control system transmission parts dismounting calibration training system.It includes graphic control panel, electrical control cabinet, sectional wheel, motor fixed rack, link mechanism, rudder face drift angle instruction disk, simulation rudder face, simulation aircraft skin, simulation aircraft stringer, π type grooves, main body rack, good fortune horse wheel, fixed pulley, connection fixture, transmission parts mounting bracket, angle connector, alternating current torque motor and cable wire.Flight control system transmission parts dismounting calibration training system provided by the invention can be used for the training and teaching of the various different transmission mechanisms such as rigid, soft and cable wire of flight control system, it is greatly improved the level and efficiency of the work of flight control system transmission parts associated maintenance, while avoiding the faulty operation caused by artificial origin in actual operation；This system the degree of automation is higher, is convenient for the training overall process of teacher remote monitoring student, greatly promotes the teaching level that civil aviation locomotive safeguards training.
Description
Technical field
The invention belongs to the teaching, training technical fields of flight control system transmission parts, are grasped more particularly to a kind of aircraft
Vertical drive system component dismounting calibration training system.
Background technology
Flight control system is to transmit control command, driving rudder face and other mechanisms to control the electromechanics of aircraft flight attitude
Integrated system.The reliability direct relation flight safety of flight control system, transmission parts are the important sets of flight control system
At part, the even more most important thing of civil aircraft track check and maintenance work.
With the development automatically controlled with microelectric technique, fax flight control system is increasingly becoming the mainstream of airline carriers of passengers
Configuration, but traditional Mechanical type airplane steerable system is still the crucial backup steerable system of modern airline carriers of passengers.In recent years,
The aging trend of domestic civil aviaton's fleet is more apparent, and the transmission parts of flight control system go out in daily maintenance checking process
Existing failure, the probability of fatigue aging are higher and higher, to which the safe flight to airline carriers of passengers brings very big hidden danger.
In the line maintenance of airline carriers of passengers, the detection of flight control system transmission parts is essential items for inspection.Traditional
It is in seasonal law or periodically right due to there is the influences such as gap, friction, flexible deformation in flight control system
Transmission parts such as are calibrated, checked and are lubricated at the maintenance works.Therefore, airline trains department and domestic air mail class universities and colleges all
Using the examination and maintenance of flight control system as compulsory course.But still lack the inspection for flight control system at present
With the Special teaching equipment of maintenance.
Invention content
To solve the above-mentioned problems, the purpose of the present invention is to provide a kind of dismounting of flight control system transmission parts to calibrate
Training system.
In order to achieve the above object, flight control system transmission parts dismounting calibration training system packet provided by the invention
It includes：Graphic control panel, electrical control cabinet, sectional wheel, motor fixed rack, link mechanism, rudder face drift angle instruction disk, simulation rudder
Face, simulation aircraft skin, simulation aircraft stringer, π type grooves, main body rack, good fortune horse wheel, fixed pulley, connection fixture, transmission parts
Mounting bracket, angle connector, alternating current torque motor and cable wire；Wherein, main body rack is tower structure；Four good fortune horse wheels are pacified respectively
Mounted in the lower part four corners of main body rack；Simulation aircraft skin is arc panel, is vertically arranged, outer surface is fixed on main body rack
Front end；π type grooves are horizontally disposed, and more π type groove spacing distances are fixed on the inner surface of simulation aircraft skin；More simulations fly
Machine stringer is spaced the front for being fixed on π type grooves in vertical manner by multiple angle connectors respectively；Transmission parts mounting bracket is
Plane frame structure is fixed on the front end of simulation aircraft stringer by multiple connection fixtures；Motor fixed rack and rudder face are inclined
Angle instruction disk is separately fixed at the front end middle and upper part and side of transmission parts mounting bracket, and the edge part of rudder face drift angle instruction disk
Position carries scale；Sectional wheel is mounted on motor fixed rack in a rotating manner；Simulation rudder face is L-shaped bar, and middle part is to rotate
Mode be mounted on rudder face drift angle instruction disk front end face in the middle part of；The both ends of link mechanism be connected to the edge of sectional wheel with
And one end of simulation rudder face；Alternating current torque motor is mounted on the back side of motor fixed rack, and output shaft is fixed in sectional wheel
In heart hole；The lower part both sides position of transmission parts mounting bracket is separately installed with two fixed pulleys arranged up and down and this four fixed sliding
The outside of wheel is cased with a cable wire, and two fixed pulleys arranged up and down, the sector at upper right position are installed in upper left-hand position
A fixed pulley is installed in wheel lower section, and the outside of this three fixed pulleys and sectional wheel is cased with another cable wire；Electrical control
Cabinet is mounted on main body rack side, and graphic control panel is mounted on the top of electrical control cabinet, and electrical control cabinet is touched with industry
Touch screen and alternating current torque motor electrical connection.
The flight control system transmission parts dismounting calibration training system further includes a monitoring camera and monitoring
Mounting bracket；The rear end of wherein monitoring mounting bracket is fixed on main body rack upper end, and front end extends forward；Monitoring camera is mounted on prison
The front bottom end of mounting bracket is controlled, and monitoring camera is electrically connected with electrical control cabinet.
The monitoring camera selects fluorite CS-C4S-52WEFR high-definition night-viewing cameras.
The alternating current torque motor selects the 220V 40W alternating current torque motors with retarder.
The graphic control panel selects Proface GC-4401W high definition graphic control panels.
It is hard that flight control system transmission parts dismounting calibration training system provided by the invention can be used for flight control system
The training and teaching of the various different transmission mechanisms such as formula, soft and cable wire, it is related to be greatly improved flight control system transmission parts
The level and efficiency of maintenance work, while avoiding the faulty operation caused by artificial origin in actual operation；This system is automatic
Change degree is higher, is convenient for the training overall process of teacher remote monitoring student, can greatly promote the teaching that civil aviation locomotive safeguards training
It is horizontal.
Description of the drawings
Fig. 1 is flight control system transmission parts provided by the invention dismounting calibration training system structural schematic diagram.
Fig. 2 is flight control system transmission parts provided by the invention dismounting calibration training system part-structure axis side signal
Figure.
Fig. 3 is that alternating current torque motor is solid in flight control system transmission parts provided by the invention dismounting calibration training system
Determine mode partial schematic diagram.
Fig. 4 is that jointed gear unit is pacified in flight control system transmission parts provided by the invention dismounting calibration training system
Fill schematic diagram.
Fig. 5 is that transmission rope connection is shown in flight control system transmission parts provided by the invention dismounting calibration training system
It is intended to.
Specific implementation mode
Calibration training is dismounted to flight control system transmission parts provided by the invention in the following with reference to the drawings and specific embodiments
Exercising system is described in detail.
As Figure 1-Figure 5, flight control system transmission parts dismounting calibration training system provided by the invention includes：Work
Industry touch screen 1, electrical control cabinet 2, sectional wheel 5, motor fixed rack 6, link mechanism 7, rudder face drift angle instruction disk 8, simulation rudder
Face 9, simulation aircraft skin 10, simulation aircraft stringer 11, π type grooves 12, main body rack 13, good fortune horse wheel 14, fixed pulley 15, connection are solid
Determine part 16, transmission parts mounting bracket 17, angle connector 18, alternating current torque motor 19 and cable wire 20；Wherein, main body rack 13 is frame
Rack and panel construction；Four good fortune horse wheels 14 are separately mounted to the lower part four corners of main body rack 13；Simulation aircraft skin 10 is arc panel,
It is vertically arranged, outer surface is fixed on the front end of main body rack 13；π type grooves 12 are horizontally disposed, and more 12 spacing distances of π type grooves are solid
It is scheduled on the inner surface of simulation aircraft skin 10；More simulation aircraft stringers 11 are respectively by multiple angle connectors 18 with vertical
Mode interval is fixed on the front of π type grooves 12；Transmission parts mounting bracket 17 is plane frame structure, passes through multiple connection fixtures
16 are fixed on the front end of simulation aircraft stringer 11；Motor fixed rack 6 and rudder face drift angle instruction disk 8 are separately fixed at transmission parts
The front end middle and upper part of mounting bracket 17 and side, and the edge of rudder face drift angle instruction disk 8 carries scale；Sectional wheel 5 is to turn
Dynamic mode is mounted on motor fixed rack 6；Simulation rudder face 9 is L-shaped bar, and middle part is mounted on rudder face drift angle in a rotating manner
In the middle part of the front end face for indicating disk 8；The both ends of link mechanism 7 be connected to sectional wheel 5 edge and simulate rudder face 9 one
End；Alternating current torque motor 19 is mounted on the back side of motor fixed rack 6, and output shaft is fixed in the centre bore of sectional wheel 5；Transmission
The lower part both sides position of part mounting rack 17 is separately installed with two fixed pulleys 15 arranged up and down and this four fixed pulleys 15
Outside is cased with a cable wire 20, and two fixed pulleys 15 arranged up and down, the sector at upper right position are installed in upper left-hand position
A fixed pulley 15 is installed in 5 lower section of wheel, and the outside of this three fixed pulleys 15 and sectional wheel 5 is cased with another cable wire 20；
Electrical control cabinet 2 is mounted on 13 side of main body rack, and graphic control panel 1 is mounted on the top of electrical control cabinet 2, and electric-controlled
Cabinet 2 processed is electrically connected with graphic control panel 1 and alternating current torque motor 19.
The flight control system transmission parts dismounting calibration training system further includes a monitoring camera 3 and monitoring
Mounting bracket 4；The rear end of wherein monitoring mounting bracket 4 is fixed on 13 upper end of main body rack, and front end extends forward；Monitoring camera 3 is pacified
Mounted in the front bottom end of monitoring mounting bracket 4, and monitoring camera 3 is electrically connected with electrical control cabinet 2.
The monitoring camera 3 selects fluorite CS-C4S-52WEFR high-definition night-viewing cameras.
The alternating current torque motor selects the 220V 40W alternating current torque motors with retarder.
The graphic control panel selects Proface GC-4401W high definition graphic control panels.
The application method that flight control system transmission parts provided by the invention are now dismounted to calibration training system illustrates such as
Under：
First, start the electrical control cabinet 2 of flight control system transmission parts dismounting calibration training system by testing staff
And complete System self-test；
Second, two cable wires 20 are installed on fixed pulley 15 and sectional wheel 5 according to Fig. 5 by teacher；
Third carries out the rigid transmission of flight control system and safeguards training：Teacher is using graphic control panel 1 and passes through electric-controlled
Cabinet 2 processed controls alternating current torque motor 19 and rotates, and thus sectional wheel 5 is driven to rotate together, and is then driven and is simulated by link mechanism 7
Rudder face 9 rotates, and student can observe the number of degrees of rudder face drift angle on rudder face drift angle instruction disk 8 using scale；
4th, it carries out flight control system flexible transmission and safeguards training：The fixed pulley 15 of lower part four can be used to train for student
The duties such as the inspection of cable wire 20 and lubrication work.
In addition, in teaching process, teacher can observe the training of student in real time by monitoring camera 3.In addition, such as
This system gives a warning in use or abnormal conditions, should power off and stop using at once.
It is emphasized that embodiment of the present invention is illustrative, without being restrictive, therefore the present invention is simultaneously
It is not limited to the embodiment described in specific implementation mode.Without departing from the scope of the invention, it can be carried out respectively
Kind is improved or is replaced.Especially, as long as there is no the conflict in structure, the feature in each embodiment can be combined with each other,
Or according to the technique and scheme of the present invention and the other embodiment that obtains of other this similar principles by those skilled in the art, together
Sample belongs to the scope of protection of the invention.
Claims (5)
1. a kind of flight control system transmission parts dismounting calibration training system, it is characterised in that：The flight control system
Training system is calibrated in transmission parts dismounting：Graphic control panel (1), electrical control cabinet (2), sectional wheel (5), motor fix branch
Frame (6), link mechanism (7), rudder face drift angle instruction disk (8), simulation rudder face (9), simulation aircraft skin (10), simulation aircraft stringer
(11), π type grooves (12), main body rack (13), good fortune horse wheel (14), fixed pulley (15), connection fixture (16), transmission parts installation
Frame (17), angle connector (18), alternating current torque motor (19) and cable wire (20)；Wherein, main body rack (13) is tower structure；
Four good fortune horse wheels (14) are separately mounted to the lower part four corners of main body rack (13)；It is arc panel to simulate aircraft skin (10), is hung down
Straight setting, outer surface is fixed on the front end of main body rack (13)；π type grooves (12) are horizontally disposed, more π type grooves (12) interval distances
From be fixed on simulation aircraft skin (10) inner surface on；More simulation aircraft stringers (11) pass through multiple angle connectors respectively
(18) it is spaced the front for being fixed on π type grooves (12) in vertical manner；Transmission parts mounting bracket (17) is plane frame structure, is led to
Cross the front end that multiple connection fixtures (16) are fixed on simulation aircraft stringer (11)；Motor fixed rack (6) and rudder face drift angle refer to
Show that disk (8) is separately fixed at the front end middle and upper part and side of transmission parts mounting bracket (17), and rudder face drift angle indicates disk (8)
Edge carries scale；Sectional wheel (5) is mounted on motor fixed rack (6) in a rotating manner；It is L to simulate rudder face (9)
Shape bar, middle part are mounted in the middle part of the front end face of rudder face drift angle instruction disk (8) in a rotating manner；The both ends of link mechanism (7) point
It is not connected to the edge of sectional wheel (5) and one end of simulation rudder face (9)；Alternating current torque motor (19) is mounted on motor and fixes branch
The back side of frame (6), output shaft are fixed in the centre bore of sectional wheel (5)；The lower part both sides position of transmission parts mounting bracket (17)
The outside for being separately installed with two fixed pulleys (15) arranged up and down and this four fixed pulleys (15) is cased with a cable wire (20), on
Portion's left-hand portion installs two fixed pulleys (15) arranged up and down, and installation one is fixed below the sectional wheel (5) at upper right position
Pulley (15), and the outside of this three fixed pulleys (15) and sectional wheel (5) is cased with another cable wire (20)；Electrical control cabinet
(2) it is mounted on main body rack (13) side, graphic control panel (1) is mounted on the top of electrical control cabinet (2), and electrical control
Cabinet (2) is electrically connected with graphic control panel (1) and alternating current torque motor (19).
2. flight control system transmission parts dismounting calibration training system according to claim 1, it is characterised in that：It is described
Flight control system transmission parts dismounting calibration training system further include a monitoring camera (3) and monitor mounting bracket (4)；
The rear end of wherein monitoring mounting bracket (4) is fixed on main body rack (13) upper end, and front end extends forward；Monitoring camera (3) is installed
In the front bottom end of monitoring mounting bracket (4), and monitoring camera (3) is electrically connected with electrical control cabinet (2).
3. flight control system transmission parts dismounting calibration training system according to claim 2, it is characterised in that：It is described
Monitoring camera (3) select fluorite CS-C4S-52WEFR high-definition night-viewing cameras.
4. flight control system transmission parts dismounting calibration training system according to claim 1, it is characterised in that：It is described
Alternating current torque motor (19) select the 220V 40W alternating current torque motors with retarder.
5. flight control system transmission parts dismounting calibration training system according to claim 1, it is characterised in that：It is described
Graphic control panel (1) select Proface GC-4401W high definition graphic control panels.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810306205.0A CN108447334A (en) | 2018-04-08 | 2018-04-08 | A kind of flight control system transmission parts dismounting calibration training system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810306205.0A CN108447334A (en) | 2018-04-08 | 2018-04-08 | A kind of flight control system transmission parts dismounting calibration training system |
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| Publication Number | Publication Date |
|---|---|
| CN108447334A true CN108447334A (en) | 2018-08-24 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810306205.0A Pending CN108447334A (en) | 2018-04-08 | 2018-04-08 | A kind of flight control system transmission parts dismounting calibration training system |
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| Country | Link |
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| CN (1) | CN108447334A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109036086A (en) * | 2018-09-10 | 2018-12-18 | 苏州大成有方数据科技有限公司 | A kind of front handling mobile crane simulator that three face rings is wound |
| CN109118867A (en) * | 2018-09-10 | 2019-01-01 | 苏州大成有方数据科技有限公司 | A kind of front handling mobile crane simulator of stereo-circulation formula |
| CN109147544A (en) * | 2018-09-10 | 2019-01-04 | 苏州大成有方数据科技有限公司 | A kind of front handling mobile crane simulator with movable platform |
| CN109166394A (en) * | 2018-09-10 | 2019-01-08 | 苏州大成有方数据科技有限公司 | A kind of front handling mobile crane simulator that movable three face ring is wound |
| CN111564086A (en) * | 2020-05-26 | 2020-08-21 | 江西电力职业技术学院 | Teaching dismouting device of pump |
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| CN102157089A (en) * | 2011-04-01 | 2011-08-17 | 天津中天翔翼航空科技有限公司 | Simulation device for steering wheel of airplane flight simulator |
| CN103308295A (en) * | 2013-01-05 | 2013-09-18 | 中国航空工业集团公司西安飞机设计研究所 | Control and check test method for flight control mechanical control system |
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2018
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| CN102157089A (en) * | 2011-04-01 | 2011-08-17 | 天津中天翔翼航空科技有限公司 | Simulation device for steering wheel of airplane flight simulator |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109036086A (en) * | 2018-09-10 | 2018-12-18 | 苏州大成有方数据科技有限公司 | A kind of front handling mobile crane simulator that three face rings is wound |
| CN109118867A (en) * | 2018-09-10 | 2019-01-01 | 苏州大成有方数据科技有限公司 | A kind of front handling mobile crane simulator of stereo-circulation formula |
| CN109147544A (en) * | 2018-09-10 | 2019-01-04 | 苏州大成有方数据科技有限公司 | A kind of front handling mobile crane simulator with movable platform |
| CN109166394A (en) * | 2018-09-10 | 2019-01-08 | 苏州大成有方数据科技有限公司 | A kind of front handling mobile crane simulator that movable three face ring is wound |
| CN111564086A (en) * | 2020-05-26 | 2020-08-21 | 江西电力职业技术学院 | Teaching dismouting device of pump |
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Application publication date: 20180824 |