CN108281060A - A kind of emulation cockpit panel module for flight simulation - Google Patents
A kind of emulation cockpit panel module for flight simulation Download PDFInfo
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- CN108281060A CN108281060A CN201810299385.4A CN201810299385A CN108281060A CN 108281060 A CN108281060 A CN 108281060A CN 201810299385 A CN201810299385 A CN 201810299385A CN 108281060 A CN108281060 A CN 108281060A
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- 238000004088 simulation Methods 0.000 title claims abstract description 56
- 230000003044 adaptive effect Effects 0.000 claims abstract description 77
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- 239000010410 layer Substances 0.000 claims description 15
- 239000002344 surface layer Substances 0.000 claims description 15
- 239000002775 capsule Substances 0.000 claims description 7
- 230000009471 action Effects 0.000 claims description 3
- 230000008901 benefit Effects 0.000 abstract description 9
- 238000012423 maintenance Methods 0.000 abstract description 2
- 238000012549 training Methods 0.000 description 22
- 230000006872 improvement Effects 0.000 description 10
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- 238000005516 engineering process Methods 0.000 description 6
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- 238000004891 communication Methods 0.000 description 4
- 238000011161 development Methods 0.000 description 4
- 238000009434 installation Methods 0.000 description 4
- 230000006855 networking Effects 0.000 description 3
- 238000011160 research Methods 0.000 description 3
- 238000012360 testing method Methods 0.000 description 3
- 238000002474 experimental method Methods 0.000 description 2
- 230000002452 interceptive effect Effects 0.000 description 2
- 230000007774 longterm Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- 238000001179 sorption measurement Methods 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- 238000013473 artificial intelligence Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004422 calculation algorithm Methods 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
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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
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
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Abstract
The invention discloses a kind of emulation cockpit panel modules for flight simulation, including：Front panel and two side panels；Front panel include front panel module group and with front panel pedestal, common interface module A and at least one adaptive magnetic force firm joint device A are installed, the corresponding common interface module A of front panel pedestal is equipped with common interface module B, corresponding adaptive magnetic force firm joint device A is equipped with adaptive magnetic force firm joint device B in front panel module group；Side panel includes side plate module group and side panel pedestal, at least one common interface module C and at least one adaptive magnetic force firm joint device C are installed, the corresponding common interface module C of side panel pedestal is equipped with common interface module D, corresponding adaptive magnetic force firm joint device C is equipped with adaptive magnetic force firm joint device D in the plate module group of side.The configuration of the present invention is simple is convenient for maintenance, and reliability and efficiency-cost ratio are with the obvious advantage；Universal joint, with needing combo, adaptability and generalization with the obvious advantage.
Description
Technical field
The present invention relates to flight simulation applied technical field more particularly to a kind of emulation cockpit panels for flight simulation
Module.
Background technology
Simulated training with system emulation for main technical support, with the development of computer technology and system simulation technology,
The equipment that simulation trainer is widely used in flight, driving etc. uses operation training.Simulated training due to safety, economy,
Efficiently, controllably, can be repeated several times, devoid of risk, not climate condition and place space limitation etc., especially in flight simulation emulation side
Face has unrivaled unique advantage.
And increasing with aircraft type, each money aircraft cockpit are all not quite similar so that mating to carry out simulation instruction
The type of experienced flight simulator also greatly increases therewith, this, which has been inevitably resulted in, repeats to research and develop, and increases maintenance
Difficulty.And simulated flight is to realize flight simulation by the powerful operational capability of computer, even if being different flight simulator,
Computer simulation model, algorithm, hardware interface and the digital-to-analogue conversion of its bottom are all similar, are ground to save simulation trainer
Expense processed shortens the R＆D cycle, and the standardization and generalization of simulation trainer become the only selection researched and developed for simulating assembly, this
The utilization rate for also improving equipment simultaneously, enhances the reliability of equipment.
Similarly, with the development of the technologies such as microelectronics, artificial intelligence and virtual reality, in equipment simulatings such as driving, manipulations
Training aspect, standardization, the generalization of simulation trainer are also the developing direction in future.
With the fast development of modern military technology, flight training is also gradually towards architecture, integrated, complication side
To development, this also proposed similar requirement to fly simulation training, and the simulated training of architecture is also gradually brought into schedule.And
Architecture simulated training, it is necessary to which, with mission requirements to draw, the training unit with " full dimension is with group " is support, when arbitrary
Between, anywhere distributes according to specific tasks plan and role and requires, determines the combo and quantity of flight simulation functional unit,
The Dock With Precision Position of operational training demand and training support supply, maximum limit are realized in the organizational framework simulated training of flexible ground
Improve training efficiency-cost ratio, to the maximum extent performance group instruction degree of freedom in degree ground.Currently, traditional simulated training can only rely on it is existing
The simulator of fixed type is trained, and existing simulation trainer type is various, and function is relatively simple：For same
Kind type, has the simulator of several kinds of different types, each simulator can only carry out corresponding part technique and tactics simulated training.
And the standard between various simulators due to network interface is not consistent, data cannot be shared, and cannot be distributed on a large scale
The simulated training of formula interactive mode.Therefore architecture simulated training at this stage, can only according to the quantity of existing simulator, model with
And its function that can be realized customizes certain tasks, can not accomplish according to the flexible combo of mission requirements, this and architecture simulation instruction
Experienced mission requirements run in the opposite direction.New requirement is thus proposed to flight simulator：In order to adapt to architecture simulation
Trained variation, flight simulator must provide standardization, unitized combined equipment, could flexibly match at any time by required type
Group, and can be trained according to operational training plan networking at any time, meet architecture simulated training mission requirements, performance group to greatest extent
Instruct degree of freedom.
Invention content
Shortcoming present in regarding to the issue above, the present invention provide a kind of emulation cockpit panel for flight simulation
Module.
To achieve the above object, the present invention provides a kind of emulation cockpit panel module for flight simulation, including：Front
Plate and two side panels；
The front panel include front panel module group for analog capsule cabin front face instrument and equipment and with the front
The matched front panel pedestal of plate module group, be equipped in the front panel module group common interface module A and it is at least one from
It adapts to magnetic force firm joint device A, the front panel pedestal corresponding common interface module A and common interface module B, institute is installed
It states the corresponding adaptive magnetic force firm joint device A of front panel pedestal and adaptive magnetic force firm joint device B is installed；
Each side panel include side plate module group for analog capsule cabin both sides instrument and equipment and with the side
The matched side panel pedestal of panel module group, be equipped in the side plate module group at least one common interface module C and
At least one adaptive magnetic force firm joint device C, the corresponding common interface module C of side panel pedestal are equipped with general connect
Mouth mold block D, the corresponding adaptive magnetic force firm joint device C of side panel pedestal are equipped with adaptive magnetic force firm joint device D.
As a further improvement on the present invention, the front panel module group is top panel unit module, the top panel list
The surface layer of element module is aircraft cockpit front top half Simulation Interface, and middle layer is for the control circuit of operation and for showing
The core engine of control, bottom are the common interface module A and adaptive magnetic force firm joint device A.
As a further improvement on the present invention, the front panel module group is top panel unit module and following plate unit mould
The T-type structure that block is constituted；
The surface layer of the top panel unit module is aircraft cockpit front top half Simulation Interface, and middle layer is for transporting
The control circuit of calculation and core engine for aobvious control, bottom is common interface module E, lock A and the adaptive magnetic force are affixed
Device A；The surface layer of the lower panel unit module is aircraft cockpit front lower half portion Simulation Interface, and middle layer is for operation
Control circuit and core engine for aobvious control, bottom be with the matched common interface module F of the common interface module E,
With the lock A matched lock B and common interface module A；
The slot being inserted into for the upper end of the lower panel unit module is provided in the middle part of the top panel unit module, it is described
The bottom of slot is equipped with the common interface module E and lock A, and the upper end of the lower panel unit module is equipped with described general connect
Mouth mold block F and lock B, after the lock A is with lock B lockings, the common interface module E is opposite with common interface module F
It connects.
As a further improvement on the present invention, the side wall of the slot is equipped with sliding rail, the lower panel unit module
The corresponding sliding rail of side wall is equipped with sliding slot.
As a further improvement on the present invention, the pin hole passed through for safety pin A is offered on the top panel unit module
A offers the pin hole B passed through for safety pin A on the lower panel unit module.
As a further improvement on the present invention, the front panel pedestal is the ∏ type knots that two support columns are constituted with crossbeam
Structure；
The crossbeam is fixedly arranged in the middle of backboard, and the backboard is equipped with upright guide rail and common interface module B, it is described on
The corresponding upright guide rail in the back side of panel unit module is equipped with guide block；Two adaptive magnetic force firm joint device B installations
On the crossbeam and it is located at the backboard both sides, the support for carrying the top panel unit module is installed on the crossbeam
Plate；It is described general to connect when the guide block, which slides into the upright guide rail and the top panel unit module, to be against on the supporting plate
Mouth modules A is connected to each other with common interface module B, and the adaptive magnetic force firm joint device A is opposite with adaptive magnetic force firm joint device B
It connects.
As a further improvement on the present invention, it is equipped on the support column for overturning the folding dress for folding the crossbeam
It sets；
The folding device includes the first fixing piece being mounted on upper support column, second on lower support column solid
Determine part, lock shaft and knob, first fixing piece is hinged on by articulated shaft on second fixing piece；
First fixing piece is equipped with guide hole, and second fixing piece is equipped with card slot, and the lock shaft level wears institute
Guide hole is stated, the middle part of the lock shaft is connected to by spring on second fixing piece, and the both ends of the lock shaft are hinged with described
Knob；Under original state, the lock shaft is caught under the action of the spring in the card slot, locks the upper branch of the support column
Dagger and lower support column；The knob is pulled up, the lock shaft leaves the card slot, the upper support column and crossbeam overturning folding
It is folded.
As a further improvement on the present invention, the back side of the top panel unit module is equipped with for hanging over the backboard top
The hanging block in portion offers the pin hole C passed through for safety pin B on the hanging block, offers on the backboard and is passed through for safety pin B
Pin hole D.
As a further improvement on the present invention, the side plate module group is the rectangular of multiple side panel unit modules composition
Shape structure；
The surface layer of each side panel unit module is aircraft cockpit side Simulation Interface, and middle layer is for operation
Control circuit and core engine for aobvious control, bottom is the common interface module C and adaptive magnetic force firm joint device C.
As a further improvement on the present invention, the side panel pedestal is rectangle structure；
The common interface module C of corresponding all side panel unit modules is equipped with described general on the side panel pedestal
Interface module D, the adaptive magnetic force firm joint device C installations of the corresponding all side panel unit modules of side panel pedestal are
State adaptive magnetic force firm joint device D.
Compared with prior art, beneficial effects of the present invention are：
Emulation cockpit panel module of the invention is simple in structure, is convenient for safeguarding, reliability and efficiency-cost ratio are with the obvious advantage；Interface
It is general, with needing combo, adaptability and generalization with the obvious advantage；Can combine closely various state application scenarios needs, flexible configuration face
Plate unit combines, and fast implements the full cockpit interface emulation demand of different type of machines, effectively avoids the wasting of resources and repeat to research and develop, for boat
Standardization, architecture and the networking of sky education, training and innovation experiment create condition.
Description of the drawings
Fig. 1 is the composition signal of the disclosed emulation cockpit panel module for flight simulation of an embodiment of the present invention
Figure；
Fig. 2 is the connection relationship diagram of front panel disclosed in an embodiment of the present invention；
Fig. 3 is the connection relationship diagram of side panel disclosed in an embodiment of the present invention；
Fig. 4 is top panel unit module, lower panel unit module or side plate unit disclosed in an embodiment of the present invention
The structural schematic diagram of module；
Fig. 5 is the Facad structure figure of front panel module group disclosed in an embodiment of the present invention；
Fig. 6 is the backside structure figure of front panel module group disclosed in an embodiment of the present invention；
Fig. 7 is the structure chart of front panel pedestal disclosed in an embodiment of the present invention；
Fig. 8 is the schematic diagram after front panel pedestal disclosed in an embodiment of the present invention folds；
Fig. 9 is the structure chart of folding device disclosed in an embodiment of the present invention；
Figure 10 is the Facad structure figure of side plate module group disclosed in an embodiment of the present invention；
Figure 11 is the backside structure figure of side plate module group disclosed in an embodiment of the present invention；
Figure 12 is the structure chart of side panel pedestal disclosed in an embodiment of the present invention.
In figure：
1, front panel；
10, front panel module group；101, common interface module A；102, adaptive magnetic force firm joint device A；
11, top panel unit module；111, common interface module E；112, A is latched；113, slot；114, sliding rail；115、
Pin hole A；116, guide block；117, hanging block；118, pin hole C；
12, lower panel unit module；121, common interface module F；122, B is latched；123, sliding slot；124, pin hole B；
13, front panel pedestal；131, common interface module B；132, adaptive magnetic force firm joint device B；133, support column；
134, crossbeam；135, backboard；136, upright guide rail；137, supporting plate；138, pin hole D；
14, folding device；141, the first fixing piece；142, the second fixing piece；143, lock shaft；144, it shakes hands；145, guide hole；
146, card slot；147, spring；148, articulated shaft；
2, side panel；
20, side plate module group；201, common interface module C；202, adaptive magnetic force firm joint device C；
21, side panel unit module；
22, side panel pedestal；221, common interface module D；222, adaptive magnetic force firm joint device D.
Specific implementation mode
In order to make the object, technical scheme and advantages of the embodiment of the invention clearer, below in conjunction with the embodiment of the present invention
In attached drawing, technical scheme in the embodiment of the invention is clearly and completely described, it is clear that described embodiment is
A part of the embodiment of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, ordinary skill people
The every other embodiment that member is obtained without making creative work, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that term "center", "upper", "lower", "left", "right", "vertical",
The orientation or positional relationship of the instructions such as "horizontal", "inner", "outside" be based on the orientation or positional relationship shown in the drawings, merely to
Convenient for the description present invention and simplify description, do not indicate or imply the indicated device or element must have a particular orientation,
With specific azimuth configuration and operation, therefore it is not considered as limiting the invention.In addition, term " first ", " second ",
" third " is used for description purposes only, and is not understood to indicate or imply relative importance.
In the description of the present invention, it is also necessary to which explanation is unless specifically defined or limited otherwise, term " installation ",
" connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or integrally connect
It connects；It can be mechanical connection, can also be electrical connection；It can be directly connected, can also indirectly connected through an intermediary, it can
To be the connection inside two elements.For the ordinary skill in the art, it can understand above-mentioned term with concrete condition
Concrete meaning in the present invention.
The present invention is described in further detail below in conjunction with the accompanying drawings：
The present invention relates to flight simulation application fields, including but not limited to Flight Simulator Trainers, specifically, being a kind of
It is imitative for building full cockpit with the emulation cockpit panel module for flight simulation that the unit structure of standardised generic is built
True environment realizes cockpit operating function, provides the man-machine interface interactive environment consistent with real cabin.The core of the panel module
It is a series of combination of panel unit modules and pedestal, panel unit block combiner can be flexibly replaced on demand, to realize
To the analog simulation at different type of machines interface；The panel module is detachable and folding storage, when use can Fast Installation in place, and energy
It prevents work mistiming mobile and accidentally dismantles, especially adapted to the needs of simulation trainer low cost zero dimension shield.The present invention can be with
According to different application scenarios needs, flexible configuration assembled panel unit, to realize the mould to the full cockpit interface of different type of machines
Quasi- emulation is replacing damage component with the mode for replacing panel unit module, is realizing user's zero dimension shield.
As shown in Figs 1-4, the present invention provides a kind of emulation cockpit panel module for flight simulation, including：Front panel 1
With two side panels 2；Wherein：
The front panel 1 of the present invention includes front panel module group 10 and front panel pedestal 13, and front panel module group 10 is used for mould
The instrument and equipment of quasi- cockpit front face, front panel pedestal 13 are mounted on the pedestal of analog capsule cabin；In front panel module group 10
Common interface module A101 and at least one adaptive magnetic force firm joint device A102 are installed, front panel pedestal 13 is corresponding general
Interface module A101 is equipped with common interface module B131, the corresponding adaptive magnetic force firm joint device A102 peaces of front panel pedestal 13
Equipped with adaptive magnetic force firm joint device B132；Front panel pedestal 13 can be connected with host and power supply respectively, front panel module group 10
Realize that with host, power supply is supplied by front panel pedestal 13 to front panel module group 10 into row data communication by front panel pedestal 13
Electricity.Specifically：
The front panel module group 10 of the present invention can be individual top panel unit module 11 or top panel unit module
11 with the combination of lower panel unit module 12；It is general to connect when front wall module group 10 is individual top panel unit module 11
Mouth mold block A102 and adaptive magnetic force firm joint device A102 are correspondingly arranged on top panel unit module 11.As shown in figure 4, above
The surface layer of plate unit module 11 be aircraft cockpit front top half Simulation Interface, middle layer be for operation control circuit and
For the core engine of aobvious control, bottom is common interface module A101 and adaptive magnetic force firm joint device A102.As shown in Figure 2,4,
When front wall module group 10 is the combination of top panel unit module 11 and lower panel unit module 12, top panel unit module 11
Surface layer be aircraft cockpit front top half Simulation Interface, middle layer is the control circuit for operation and the core for aobvious control
Scheming, bottom are common interface module E111, latch A112 and adaptive magnetic force firm joint device A102；Lower panel unit module
Surface layer is aircraft cockpit front lower half portion Simulation Interface, and middle layer is the control circuit for operation and the core for aobvious control
Machine, bottom are and the matched common interface module F121 of common interface module E111 and the lock matched locks of A112
B122 and common interface module A101；It latches A112 and latches the buckle structure that B122 is constituted as vehicle safety belt lock catch, pass through
It latches A112 and realizes that top panel unit module 11 and the machinery of lower panel unit module 12 are affixed with B122 is latched；Adaptive magnetic force
Firm joint device A102 and adaptive magnetic force firm joint device B132 is two parts of adaptive magnetic force firm joint device, when adaptive magnetic force
When firm joint device is powered, pass through the affixed reality of absorption of adaptive magnetic force firm joint device A102 and adaptive magnetic force firm joint device B132
The fixation of existing top panel unit module 11 and front panel pedestal 13, when adaptive magnetic force firm joint device powers off, adaptive magnetic force
The adsorption capacity of firm joint device A102 and adaptive magnetic force firm joint device B132 disappears, detachable top panel unit module 11 and front
Plate pedestal 13.After top panel unit module 11 and lower panel unit module 12 assemble, lock A112 is fastened with lock B122 to be locked
Tightly, common interface module A101 and common interface module B131 be connected to each other, common interface module E111 and common interface module
F121 is connected to each other, and adaptive magnetic force firm joint device A102 and adaptive magnetic force firm joint device B132 absorption is fixed；Wherein, general to connect
Mouth mold block A101 and common interface module B131 and common interface module E111 and common interface module F121 is general-purpose interface
Existing 36 general needle general-purpose interfaces can be selected in the male connector and female of module, common interface module.
Specifically, the upper surface of the as seen in figs. 5-6 mechanical structure of plate unit module 11 and lower panel unit module 12；Its
In, top panel unit module 11 constitutes T-type structure with lower panel unit module 12, and the middle part of top panel unit module 11 is provided with
It is equipped with common interface module E111 and lock for the bottom of the slot 113 that the upper end of lower panel unit module 12 is inserted into, slot 113
The upper end of A112, lower panel unit module 12 are equipped with common interface module F121 and lock B122, as lock A112 and lock
After B122 lockings, common interface module E111 is connected to each other with common interface module F121.Further, for the ease of following plate unit
Module 12 is smoothly inserted into connection along slot 113, and the present invention is equipped with sliding rail 114, lower panel unit module on the side wall of slot 113
The 12 corresponding sliding rail 114 of side wall is equipped with sliding slot 123；Further, it offers on top panel unit module 11 and is passed through for safety pin A
Pin hole A115, offer the pin hole B124 passed through for safety pin A on lower panel unit module 12；When top panel unit module 11
With lower panel unit module 12 by the way that further pin hole can be sequentially inserted by safety pin A after latching A112 and lock B122 lockings
In A115 and pin hole B124, the further locking of top panel unit module 11 and lower panel unit module 12 is realized.
Specifically, the mechanical structure of front panel pedestal 13 as Figure 7-8, front panel pedestal 13 is two support columns
The 133 ∏ type structures constituted with crossbeam 134, crossbeam 134 are fixedly arranged in the middle of backboard 135, and backboard 135 is equipped with upright guide rail
The corresponding upright guide rail 136 in the back side of 136 and common interface module B131, top panel unit module 11 are equipped with guide block 116, such as scheme
Shown in 6；Two adaptive magnetic force firm joint device B132 are mounted on crossbeam 134 and are located at 135 both sides of backboard, pacify on crossbeam 134
Equipped with the supporting plate 137 for carrying top panel unit module 11；When guide block 116 slide into upright guide rail 136 and above plate unit mould
When block 11 is against on supporting plate 137, common interface module A101 is connected to each other with common interface module B131, the adaptive affixed dress of magnetic force
A102 and adaptive magnetic force firm joint device B132 is set to be connected to each other.Further, as shown in fig. 6, the back side of top panel unit module 11
Equipped with the hanging block 117 for hanging over 135 top of backboard, the pin hole C118 passed through for safety pin B, backboard are offered on hanging block 117
The pin hole D138 passed through for safety pin B is offered on 135；As adaptive magnetic force firm joint device A102 and the affixed dress of adaptive magnetic force
It can be further sequentially inserted into pin hole C118 and pin hole D138 by safety pin B after setting B132 absorption lockings, realize top panel list
The further locking of element module 11 and front panel pedestal 13.
Specifically, as shown in Figure 7,8, being equipped on support column 133 of the invention for overturning the folding for folding crossbeam 134
Device 14, the front panel pedestal 13 before overturning is as shown in fig. 7, the front panel pedestal 13 after overturning is as shown in Figure 8.Specifically, such as
Shown in Fig. 9, folding device 14 includes the first fixing piece 141 being mounted on upper support column, second on lower support column
Fixing piece 142, lock shaft 143 and knob 144, the first fixing piece 141 is hinged on by articulated shaft 148 on the second fixing piece 142；The
One fixing piece 141 is equipped with guide hole 145, and the second fixing piece 142 is equipped with card slot 146, and 143 level of lock shaft wears guide hole 145, locks
The middle part of axis 143 is connected to by spring 147 on the second fixing piece 142, and the both ends of lock shaft 143 are hinged with knob 144；Initial shape
Under state (spring in the raw or tensional state), lock shaft 143 is caught under the action of spring 147 in card slot 146, locking branch
The upper support column of dagger 133 and lower support column, the schematic diagram after locking are as shown in Figure 7；Knob 144 is pulled up, lock shaft is driven
143 move in guide hole 145 and leave card slot 146, it can be achieved that upper support column and crossbeam overturning fold.
As shown in Fig. 1,3,4, each side panel of the present invention 2 includes the side panel for analog capsule cabin both sides instrument and equipment
Module group 20 and with 20 matched side panel pedestal 22 of side plate module group, side panel pedestal 22 be mounted on analog capsule cabin bottom
On seat；At least one common interface module C201 and at least one adaptive magnetic force affixed dress are installed in side plate module group 20
C202 is set, 22 corresponding common interface module C201 of side panel pedestal is equipped with common interface module D221, side panel pedestal 22
Corresponding adaptive magnetic force firm joint device C202 is equipped with adaptive magnetic force firm joint device D222；Wherein, common interface module
C201 and common interface module D221 is the male connector and female of common interface module, and common interface module can be selected existing general
36 needle general-purpose interfaces；Adaptive magnetic force firm joint device C202 and adaptive magnetic force firm joint device D222 is the affixed dress of adaptive magnetic force
The two parts set pass through adaptive magnetic force firm joint device C202 and adaptive magnetic force when adaptive magnetic force firm joint device is powered
The affixed fixation for realizing side plate module group 20 and side panel pedestal 22 of absorption of firm joint device D222, when adaptive magnetic force is affixed
When device powers off, the adsorption capacity of adaptive magnetic force firm joint device C202 and adaptive magnetic force firm joint device D222 disappears, detachably
Side plate module group 20 and side panel pedestal 22.Side panel pedestal 22 can be connected with host and power supply respectively, side plate module group
20 realize that with host, power supply gives side plate module group 20 by side panel pedestal 22 into row data communication by side panel pedestal 22
Power supply.
Specifically, as shown in figs. 10-12, side plate module group 20 is the rectangle that multiple side panel unit modules 21 are constituted
The surface layer of structure, each side panel unit module 21 is aircraft cockpit side Simulation Interface, and middle layer is the control for operation
Circuit and core engine for aobvious control, bottom is common interface module C201 and adaptive magnetic force firm joint device C202, such as Fig. 4 institutes
Show；Side panel pedestal 22 is rectangle structure, and the general of corresponding all side panel unit modules 21 connects on side panel pedestal 22
Mouth mold block C201 is equipped with common interface module D221, the corresponding all side panel unit modules of side panel pedestal 22 21 it is adaptive
Answer magnetic force firm joint device C202 that adaptive magnetic force firm joint device D202 is installed；Further, side panel pedestal 22, which is equipped with, accommodates
The storage tank of different side panel unit modules 21, storage tank can the frame of offside panel unit module 21 limited；If side
Panel will be used for a long time, then tightened by jackscrew bolt, realize long-term affixed.
Further, quick despatch when self-adaptive electromagnetic power firm joint device can guarantee off working state, and work shape can be prevented
Mistake in state is mobile and accidentally dismantles；The panel module uses vehicle safety belt lock catch (lock A and lock B) structure as separable
The mechanical attachment member of formula panel facilitates collection to transport it is advantageous that realizing the fast assembling-disassembling of panel module；The panel module
In the ad hoc general purpose interface bus (36 needle general-purpose interface) that flight-simulation equipment field is needed using analogue simulation is adapted to for the first time, and
It is not the communication linkage realized by special digiverter using actual airplane bus with simulation computer；Further,
The dismounting that upper and lower panel unit module is realize combination using the combination of sliding rail chute-type, panel unit module is detachably stored, preceding
Panel pedestal passes through in the foldable collection of folding device to rectangle side's cabinet.
Further, as shown in figure 4, upper and lower, the side panel unit module of the panel module can be divided into three layers：Surface layer is winged
Engine base cabin Simulation Interface, including various instrument show and Operation switch and button, interface and real cabin interface function it is complete
Unanimously, each panel unit module is all the analog simulation to a certain function module of cockpit, and the group of all panel unit modules
It closes then structure and the human-computer interaction function consistent with real cabin is realized to the full analogue simulation of cockpit；Middle layer uses miniature interior
It sets the aobvious control core engine of formula and control circuit realizes that the instrument at emulation cockpit interface shows and handles, serviced using without external large size
Device；And core engine can convenient changing；Core engine is different IPs scheming used in existing different type of machines, the structure and original of core engine
Reason is existing known technology, and the present invention, which does not make the structure of core engine and working method, to be changed, just for different type of machines
Boiler-plate configures the core engine and control circuit needed for it；Control circuit includes microcontroller, control circuit and upper and lower, side panel
Each electronic component on unit module surface layer is connected, and acquires each element operation variable input microcontroller, microcontroller is according to plug-in
By the way that operation signal is reached host by USB and network interface after processing, microcontroller also receives main finger by USB and network
It enables, function corresponding with each element execution that circuit connects is controlled after being handled by plug-in, such as light light on and off, built-in motor
It does；Bottom is then common interface module and all kinds of firm joint devices, and common interface module is docked with the realization of the interface of pedestal, used
In data communication and power supply power supply, firm joint device includes adaptive magnetic force firm joint device or safety belt for vehicle buckle structure etc., is used
In with pedestal reinforcement by connection and when work, prevents from accidentally dismantling or maloperation causes common interface module to unclamp.Wherein, each face
Plate unit module can be all individually replaced；It is connected between top panel unit module, lower panel unit module or side panel unit module
All circuits on surface layer, middle layer and bottom component are fixed using heat conductive silica gel, to increase reliability.
Further, before of the invention, side panel pedestal be universal, include mainly common interface module and all kinds of affixed
Device.The common interface module of all pedestals and the position of firm joint device are fixed, for the cockpit of different type of machines, base
Seat is generally applicable.Common interface module use standardized designs, the common interface module phase of interface and panel unit module
Instead, it is easy to implement docking, the data being used between panel unit module communicate and power supply power supply.Firm joint device mainly have from
Adapt to magnetic force firm joint device, safety belt for vehicle buckle structure, sliding-rail sliding and safety plug etc..The firm joint device of each pedestal
Including one of which or several, between panel unit module reinforcement by connection and when work, prevents from accidentally dismantling or maloperation
Common interface module is caused to unclamp.
Further, it only needs simply to dock when panel module of the invention combination, does not need cable and additional firm joint device,
Realize fast assembling-disassembling；Meanwhile panel module pin safe to use realizes backup connection, and backed up as the intensity of fixed connection mode,
It is also prevented from the dismounting of work mistiming.
It is as follows provided by the present invention for the dismounting mode of the emulation cockpit panel module of flight simulation：
1, simulation trainer panel module can be included in collection in rectangle side's cabinet completely after folding；It is first when installing and using
It first pulls out bottom base, after fix in position, opens the folding device on front panel base seat support, holder is installed in place.
Lower panel unit module is inserted into top panel unit module by the unit module up and down for 2, taking out front panel along sliding rail,
It is fixed with vehicle safety belt lock catch, it is merged into front panel, then front panel is installed to the backboard of front panel pedestal, is made
Docked in place with the common interface module of pedestal.Front panel module group installs.
3, the corresponding unit module of side panel is installed to side panel pedestal successively, is allowed to the general-purpose interface mould with pedestal
Block docks in place.
4, safety pin is inserted into corresponding pin hole, non-power-off must not pull up when dismantling.So far, entire panel module installs
Finish, can be powered.
5, it if necessary to be used for a long time, then installs jackscrew bolt additional in the corresponding position of pedestal and tightens.It realizes long-term affixed.
6, after being powered, panel is adsorbed on pedestal, prevents maloperation from dismantling by adaptive magnetic force firm joint device work.
7, after being powered, each panel unit module carries out self-test, and self-test is by that can work normally.Self-test is not by needing then to power off
Replace corresponding panel unit module.
When 8, being dismantled after use, deenergization, adaptive magnetic force firm joint device no longer work first, and safety plug is pulled out one by one
Under, by front panel and front panel base-separation, the vehicle safety belt lock catch of unit module on front panel is pinned, under sliding rail extraction
Upper and lower unit module is detached and is collected by panel unit module.
9, the folding device on front panel base seat support is closed, holder is made to be rotated by 90 ° folding, it is parallel with cross bar, convenient for receiving
It hides.
10, each unit module on side panel pedestal is removed successively, if there is jackscrew bolt, first removes jackscrew bolt.
11, bottom base is pushed into rectangle cabinet, folding storage finishes.
When needing replacing panel, deenergization, adaptive magnetic force firm joint device no longer work first, core engine no longer work
Make, then replaces corresponding panel unit module.
When needing replacing core engine, deenergization, adaptive magnetic force firm joint device no longer work first, core engine no longer work
Make.The data circuit interface of panel is unpluged with core engine data-interface by corresponding service hatch, then replaces core engine.
The invention has the advantages that：
1, simple in structure, convenient for safeguard, reliability and efficiency-cost ratio are with the obvious advantage.
2, Universal joint, with needing combo, adaptability and generalization with the obvious advantage.
3, can combine closely various state application scenarios needs, and the combination of flexible configuration panel unit fast implements different type of machines
Full cockpit interface emulates demand, effectively avoids the wasting of resources and repeats to research and develop, and is the standard of air training, training and innovation experiment
Change, architecture and networking create condition.
It these are only the preferred embodiment of the present invention, be not intended to restrict the invention, for those skilled in the art
For member, the invention may be variously modified and varied.Any modification made by all within the spirits and principles of the present invention,
Equivalent replacement, improvement etc., should all be included in the protection scope of the present invention.
Claims (10)
1. a kind of emulation cockpit panel module for flight simulation, which is characterized in that including：Front panel and two side panels；
The front panel include front panel module group for analog capsule cabin front face instrument and equipment and with the front template die
Block group matched front panel pedestal is equipped with common interface module A and at least one adaptive in the front panel module group
Magnetic force firm joint device A, the corresponding common interface module A of front panel pedestal is equipped with common interface module B, before described
The corresponding adaptive magnetic force firm joint device A of panel pedestal is equipped with adaptive magnetic force firm joint device B；
Each side panel include side plate module group for analog capsule cabin both sides instrument and equipment and with the side panel
Module group matched side panel pedestal is equipped at least one common interface module C and at least in the side plate module group
One adaptive magnetic force firm joint device C, the corresponding common interface module C of side panel pedestal are equipped with general-purpose interface mould
Block D, the corresponding adaptive magnetic force firm joint device C of side panel pedestal are equipped with adaptive magnetic force firm joint device D.
2. being used for the emulation cockpit panel module of flight simulation as described in claim 1, which is characterized in that the front template die
Block group is top panel unit module, and the surface layer of the top panel unit module is aircraft cockpit front top half Simulation Interface,
Middle layer is the control circuit for operation and the core engine for showing control, and bottom is for the common interface module A and adaptively
Magnetic force firm joint device A.
3. being used for the emulation cockpit panel module of flight simulation as described in claim 1, which is characterized in that the front template die
Block group is the T-type structure that top panel unit module is constituted with lower panel unit module；
The surface layer of the top panel unit module is aircraft cockpit front top half Simulation Interface, and middle layer is for operation
Control circuit and core engine for aobvious control, bottom is common interface module E, lock A and the adaptive magnetic force firm joint device
A；The surface layer of the lower panel unit module is aircraft cockpit front lower half portion Simulation Interface, and middle layer is the control for operation
Circuit processed and core engine for aobvious control, bottom for the matched common interface module F of the common interface module E and institute
State the matched lock B and common interface module A of lock A；
The slot being inserted into for the upper end of the lower panel unit module, the slot are provided in the middle part of the top panel unit module
Bottom be equipped with the common interface module E and lock A, the upper end of the lower panel unit module is equipped with the general-purpose interface mould
Block F and lock B, after the lock A is with lock B lockings, the common interface module E and common interface module F is connected to each other.
4. being used for the emulation cockpit panel module of flight simulation as claimed in claim 3, which is characterized in that the side of the slot
Wall is equipped with sliding rail, and the corresponding sliding rail of side wall of the lower panel unit module is equipped with sliding slot.
5. being used for the emulation cockpit panel module of flight simulation as claimed in claim 3, which is characterized in that the top panel list
It offers the pin hole A passed through for safety pin A on element module, offers on the lower panel unit module and passed through for safety pin A
Pin hole B.
6. being used for the emulation cockpit panel module of flight simulation as claimed in claim 2 or claim 3, which is characterized in that the front
Plate pedestal is the ∏ type structures that two support columns are constituted with crossbeam；
The crossbeam is fixedly arranged in the middle of backboard, and the backboard is equipped with upright guide rail and common interface module B, the top panel
The corresponding upright guide rail in the back side of unit module is equipped with guide block；Two adaptive magnetic force firm joint device B are mounted on institute
The backboard both sides are stated on crossbeam and be located at, the supporting plate for carrying the top panel unit module is installed on the crossbeam；
When the guide block slides into the upright guide rail and the top panel unit module is against on the supporting plate, the general-purpose interface mould
Block A is connected to each other with common interface module B, and the adaptive magnetic force firm joint device A is connected to each other with adaptive magnetic force firm joint device B.
7. being used for the emulation cockpit panel module of flight simulation as claimed in claim 6, which is characterized in that on the support column
It is equipped with for overturning the folding device for folding the crossbeam；
The folding device includes the first fixing piece being mounted on upper support column, the second fixation on lower support column
Part, lock shaft and knob, first fixing piece are hinged on by articulated shaft on second fixing piece；
First fixing piece is equipped with guide hole, and second fixing piece is equipped with card slot, and the lock shaft level wears described lead
The middle part in hole, the lock shaft is connected to by spring on second fixing piece, and the both ends of the lock shaft are hinged with the knob；
Under original state, the lock shaft is caught under the action of the spring in the card slot, locks the upper support column of the support column
With lower support column；The knob is pulled up, the lock shaft leaves the card slot, and the upper support column and crossbeam overturning fold.
8. being used for the emulation cockpit panel module of flight simulation as claimed in claim 6, which is characterized in that the top panel list
The back side of element module is equipped with for hanging over the hanging block at the top of the backboard, and the pin passed through for safety pin B is offered on the hanging block
Hole C offers the pin hole D passed through for safety pin B on the backboard.
9. being used for the emulation cockpit panel module of flight simulation as described in claim 1, which is characterized in that the side template die
Block group is the rectangle structure that multiple side panel unit modules are constituted；
The surface layer of each side panel unit module is aircraft cockpit side Simulation Interface, and middle layer is the control for operation
Circuit and core engine for aobvious control, bottom is the common interface module C and adaptive magnetic force firm joint device C.
10. being used for the emulation cockpit panel module of flight simulation as claimed in claim 9, which is characterized in that the side panel
Pedestal is rectangle structure；
The common interface module C of corresponding all side panel unit modules is equipped with the general-purpose interface on the side panel pedestal
Module D, the adaptive magnetic force firm joint device C of the corresponding all side panel unit modules of side panel pedestal be equipped with it is described from
Adapt to magnetic force firm joint device D.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201810299385.4A CN108281060B (en) | 2018-04-04 | 2018-04-04 | A emulation cabin panel module for flight simulation |
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|---|---|---|---|
| CN201810299385.4A CN108281060B (en) | 2018-04-04 | 2018-04-04 | A emulation cabin panel module for flight simulation |
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Cited By (1)
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| CN111564082A (en) * | 2019-02-14 | 2020-08-21 | 波音公司 | Medium fidelity simulation approach and method for flight crew training and evaluation |
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| CN108281060B (en) | 2024-02-09 |
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