CN108281060B - A emulation cabin panel module for flight simulation - Google Patents
A emulation cabin panel module for flight simulation Download PDFInfo
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- CN108281060B CN108281060B CN201810299385.4A CN201810299385A CN108281060B CN 108281060 B CN108281060 B CN 108281060B CN 201810299385 A CN201810299385 A CN 201810299385A CN 108281060 B CN108281060 B CN 108281060B
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- 230000003044 adaptive effect Effects 0.000 claims description 10
- 230000007774 longterm Effects 0.000 claims description 5
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- 238000012360 testing method Methods 0.000 claims description 2
- 238000012423 maintenance Methods 0.000 abstract description 7
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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 simulation cabin panel module for flight simulation, which comprises: a front panel and two side panels; the front panel comprises a front panel module group and a front panel base, wherein the front panel module group is provided with a universal interface module A and at least one self-adaptive magnetic force fixedly-connecting device A, the front panel base is provided with a universal interface module B corresponding to the universal interface module A, and the self-adaptive magnetic force fixedly-connecting device B corresponding to the self-adaptive magnetic force fixedly-connecting device A; the side panel comprises a side panel module group and a side panel base, wherein the side panel module group is provided with at least one universal interface module C and at least one self-adaptive magnetic force fixedly-connecting device C, the side panel base is provided with a universal interface module D corresponding to the universal interface module C, and the self-adaptive magnetic force fixedly-connecting device D corresponding to the self-adaptive magnetic force fixedly-connecting device C. The invention has the advantages of simple structure, convenient maintenance and obvious reliability and cost effectiveness ratio; the interface is universal, the group is matched according to the need, and the advantages of adaptability and popularization are obvious.
Description
Technical Field
The invention relates to the technical field of flight simulation application, in particular to a simulation cabin panel module for flight simulation.
Background
The simulation training uses system simulation as a main technical support, and along with the development of computer technology and system simulation technology, the simulation training device is widely used for equipment use operation training in the aspects of flight, driving and the like. The simulation training has incomparable unique advantages in the aspect of flight simulation because of safety, economy, high efficiency, controllability, repeated times, no risk, no limitation of climate conditions and site space and the like.
With the increase of the types of aircrafts, the cockpit of each type of aircrafts is different, so that the types of flight simulators matched with the aircraft for simulation training are greatly increased, repeated research and development are inevitably caused, and the maintenance difficulty is increased. The simulation flight is realized by means of strong computing power of a computer, and even for different flight simulators, the computer simulation model, algorithm, hardware interface and digital-to-analog conversion at the bottom layer are similar, so that the development cost of the simulation trainer is saved, the development period is shortened, the standardization and generalization of the simulation trainer become different choices for the development of simulation equipment, and the utilization rate of equipment is improved, and the reliability of the equipment is enhanced.
Similarly, with the development of technologies such as microelectronics, artificial intelligence and virtual reality, the standardization and generalization of the simulation trainer are also future development directions in terms of simulation training of driving, control and other equipment.
With the rapid development of modern military technologies, flight training is gradually developed towards systemization, integration and complexity, and similar requirements are also provided for flight simulation training, and the systemized simulation training is also gradually scheduled. The systematic simulation training is carried out by taking the task requirement as traction and taking the training units of 'full-dimension group following' as support, determining the group allocation and the number of the flight simulation functional units at any time and any place according to specific task plans and role allocation requirements, flexibly organizing the systematic simulation training, realizing the accurate butt joint of the combat training requirement and the training guarantee supply, furthest improving the training efficiency and cost ratio and furthest exerting the freedom of group training. At present, the traditional simulation training can only rely on the existing simulator of a fixed model for training, but the existing simulation training device has various types and single function: for the same model, there are several different types of simulators, each of which can only perform a corresponding part of technical simulation training. The standards of the network interfaces are inconsistent, so that data cannot be shared, and large-scale distributed interactive simulation training cannot be performed. Therefore, the systematic simulation training at the present stage can only customize certain tasks according to the number and the model of the existing simulators and the functions which can be realized by the simulators, and can not be flexibly assembled according to the task requirements, which is contrary to the task requirements of the systematic simulation training. This places new demands on the flight simulator: in order to adapt to the change of the systematic simulation training, the flight simulator must provide standardized and generalized combined equipment to flexibly group at any time according to the required model, and can realize networking training at any time according to a combat training plan, so that the requirements of the systematic simulation training task are met to the maximum extent, and the freedom of the group training is exerted.
Disclosure of Invention
In order to overcome the defects in the prior art, the invention provides a simulation cabin panel module for flight simulation.
In order to achieve the above object, the present invention provides a simulation cabin panel module for flight simulation, comprising: a front panel and two side panels;
the front panel comprises a front panel module group for simulating instruments and equipment on the front face of the cabin and a front panel base matched with the front panel module group, wherein a universal interface module A and at least one self-adaptive magnetic force fixedly-connecting device A are installed on the front panel module group, a universal interface module B is installed on the front panel base corresponding to the universal interface module A, and a self-adaptive magnetic force fixedly-connecting device B is installed on the front panel base corresponding to the self-adaptive magnetic force fixedly-connecting device A;
each side panel comprises a side panel module group for simulating instruments and equipment on two sides of a cabin and a side panel base matched with the side panel module group, wherein at least one universal interface module C and at least one self-adaptive magnetic force fixedly-connecting device C are installed on the side panel module group, a universal interface module D is installed on the side panel base corresponding to the universal interface module C, and a self-adaptive magnetic force fixedly-connecting device D is installed on the side panel base corresponding to the self-adaptive magnetic force fixedly-connecting device C.
As a further improvement of the invention, the front panel module group is an upper panel unit module, the surface layer of the upper panel unit module is a simulation interface of the upper half part of the front part of the aircraft cabin, the middle layer is a control circuit for operation and a core machine for display control, and the bottom layer is the universal interface module A and the self-adaptive magnetic force fixedly-connecting device A.
As a further improvement of the present invention, the front panel module group is a T-shaped structure composed of an upper panel unit module and a lower panel unit module;
the surface layer of the upper panel unit module is a simulation interface of the upper half part of the front part of the aircraft cabin, the middle layer is a control circuit for operation and a core machine for display control, and the bottom layer is a universal interface module E, a lock catch A and the self-adaptive magnetic force fixedly-connecting device A; the surface layer of the lower panel unit module is a simulation interface of the lower half part of the front part of the aircraft cabin, the middle layer is a control circuit for operation and a core machine for display control, and the bottom layer is a universal interface module F matched with the universal interface module E, a lock catch B matched with the lock catch A and the universal interface module A;
the middle part of the upper panel unit module is provided with a slot for the upper end of the lower panel unit module to be inserted, the bottom of the slot is provided with a universal interface module E and a lock catch A, the upper end of the lower panel unit module is provided with a universal interface module F and a lock catch B, and after the lock catch A and the lock catch B are locked, the universal interface module E is in butt joint with the universal interface module F.
As a further improvement of the invention, the side wall of the slot is provided with a sliding rail, and the side wall of the lower panel unit module is provided with a sliding groove corresponding to the sliding rail.
As a further improvement of the invention, the upper panel unit module is provided with a pin hole A for the safety pin A to pass through, and the lower panel unit module is provided with a pin hole B for the safety pin A to pass through.
As a further improvement of the invention, the front panel base is of an n-shaped structure formed by two support columns and a cross beam;
a backboard is fixed in the middle of the cross beam, a vertical guide rail and a universal interface module B are arranged on the backboard, and a guide block is arranged on the back surface of the upper panel unit module corresponding to the vertical guide rail; the two self-adaptive magnetic force fixedly connected devices B are arranged on the cross beam and positioned on two sides of the back plate, and a supporting plate for bearing the upper panel unit module is arranged on the cross beam; when the guide blocks slide into the vertical guide rails and the upper panel unit modules are propped against the supporting plates, the universal interface module A is butted with the universal interface module B, and the self-adaptive magnetic force fixedly-connecting device A is butted with the self-adaptive magnetic force fixedly-connecting device B.
As a further improvement of the invention, the support column is provided with a folding device for turning and folding the cross beam;
the folding device comprises a first fixing piece arranged on the upper support column, a second fixing piece arranged on the lower support column, a lock shaft and a handle, wherein the first fixing piece is hinged on the second fixing piece through a hinge shaft;
the first fixing piece is provided with a guide hole, the second fixing piece is provided with a clamping groove, the lock shaft horizontally penetrates through the guide hole, the middle part of the lock shaft is connected to the second fixing piece through a spring, and the two ends of the lock shaft are hinged with the handles; in an initial state, the lock shaft is clamped into the clamping groove under the action of the spring, and the upper support column and the lower support column of the support column are locked; the handle is pulled upwards, the lock shaft leaves the clamping groove, and the upper support column and the cross beam are turned and folded.
As a further improvement of the invention, a hanging block used for hanging on the top of the back plate is arranged on the back surface of the upper panel unit module, a pin hole C for the safety pin B to pass through is formed on the hanging block, and a pin hole D for the safety pin B to pass through is formed on the back plate.
As a further improvement of the present invention, the side panel module group is a rectangular structure formed by a plurality of side panel unit modules;
the surface layer of each side panel unit module is an aircraft cabin side simulation interface, the middle layer is a control circuit for operation and a core machine for display control, and the bottom layer is the universal interface module C and the self-adaptive magnetic force fixedly-connecting device C.
As a further improvement of the invention, the side panel base is of rectangular structure;
the universal interface module D is arranged on the universal interface module C corresponding to all the side panel unit modules on the side panel base, and the adaptive magnetic force fixedly connecting device D is arranged on the adaptive magnetic force fixedly connecting device C corresponding to all the side panel unit modules on the side panel base.
Compared with the prior art, the invention has the beneficial effects that:
the simulation cabin panel module has the advantages of simple structure, convenient maintenance and obvious reliability and cost effectiveness ratio; the interfaces are universal, matched according to requirements, and the advantages of adaptability and popularization are obvious; the method can be used for tightly combining the requirements of multiple-mode application scenes, flexibly configuring the panel unit combination, rapidly realizing the simulation requirements of all cabin interfaces of different types, effectively avoiding the waste of resources and repeated research and development, and creating conditions for standardization, systemization and networking of aviation education, training and innovation experiments.
Drawings
FIG. 1 is a schematic diagram of a simulation cockpit panel module for flight simulation according to one embodiment of the present invention;
FIG. 2 is a schematic diagram of a connection relationship of a front panel according to an embodiment of the present invention;
FIG. 3 is a schematic diagram illustrating a connection relationship between side panels according to an embodiment of the present invention;
fig. 4 is a schematic view showing the structure of an upper panel unit module, a lower panel unit module or a side panel unit module according to an embodiment of the present invention;
FIG. 5 is a front block diagram of a front panel module group according to an embodiment of the present invention;
FIG. 6 is a rear block diagram of a front panel module group according to an embodiment of the present invention;
FIG. 7 is a block diagram of a front panel base according to an embodiment of the present invention;
FIG. 8 is a schematic view of a front panel base according to an embodiment of the present invention after being folded;
FIG. 9 is a block diagram of a folding device according to an embodiment of the present invention;
FIG. 10 is a front block diagram of a side panel module set according to one embodiment of the present invention;
FIG. 11 is a rear block diagram of a side panel module set according to one embodiment of the present invention;
fig. 12 is a block diagram of a side panel base according to an embodiment of the present invention.
In the figure:
1. a front panel;
10. a front panel module group; 101. a universal interface module A; 102. the self-adaptive magnetic force fixedly connecting device A;
11. an upper panel unit module; 111. a universal interface module E; 112. a lock catch A; 113. a slot; 114. a slide rail; 115. pin holes A; 116. a guide block; 117. hanging blocks; 118. a pin hole C;
12. a lower panel unit module; 121. a universal interface module F; 122. a lock catch B; 123. a chute; 124. pin holes B;
13. a front panel base; 131. a universal interface module B; 132. the self-adaptive magnetic force fixedly connecting device B; 133. a support column; 134. a cross beam; 135. a back plate; 136. a vertical guide rail; 137. a supporting plate; 138. a pin hole D;
14. a folding device; 141. a first fixing member; 142. a second fixing member; 143. a lock shaft; 144. a handle; 145. a guide hole; 146. a clamping groove; 147. a spring; 148. a hinge shaft;
2. a side panel;
20. a side panel module group; 201. a universal interface module C; 202. the self-adaptive magnetic force fixedly connecting device C;
21. a side panel unit module;
22. a side panel base; 221. a universal interface module D; 222. and a self-adaptive magnetic force fixedly connecting device D.
Detailed Description
For the purpose of making the objects, technical solutions and advantages of the embodiments of the present invention more apparent, the technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is apparent that the described embodiments are some embodiments of the present invention, but not all embodiments of the present invention. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
In the description of the present invention, it should be noted that the directions or positional relationships indicated by the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. are based on the directions or positional relationships shown in the drawings, are merely for convenience of describing the present invention and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it should also be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be either fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present invention will be understood in specific cases by those of ordinary skill in the art.
The invention is described in further detail below with reference to the attached drawing figures:
the invention relates to the field of flight simulation application, including but not limited to a flight simulation trainer, in particular to a simulation cabin panel module for flight simulation constructed by a standardized and generalized unit architecture, which is used for constructing a full cabin simulation environment, realizing cabin manipulation function and providing a man-machine interface interaction environment consistent with a real cabin. The core of the panel module is a series of combinations of panel unit modules and bases, and the panel unit module combination can be flexibly replaced according to requirements, so that the simulation of interfaces of different models is realized; the panel module can be disassembled, folded and stored, can be quickly assembled in place when in use, can prevent misoperation during working and can be mistakenly disassembled, and particularly meets the low-cost zero maintenance requirement of the simulation trainer. The invention can flexibly configure the combined panel unit according to different application scene requirements, thereby realizing the analog simulation of the full cabin interfaces of different machine types, and realizing the zero maintenance of users by replacing damaged parts in a mode of replacing the panel unit module.
As shown in fig. 1-4, the present invention provides a simulation cockpit panel module for flight simulation, comprising: a front panel 1 and two side panels 2; wherein:
the front panel 1 of the present invention comprises a front panel module group 10 and a front panel base 13, wherein the front panel module group 10 is used for simulating the instrument and equipment of the front part of the cabin, and the front panel base 13 is installed on the base of the simulated cabin; the front panel module group 10 is provided with a universal interface module A101 and at least one self-adaptive magnetic force fixedly-connecting device A102, the front panel base 13 is provided with a universal interface module B131 corresponding to the universal interface module A101, and the front panel base 13 is provided with a self-adaptive magnetic force fixedly-connecting device B132 corresponding to the self-adaptive magnetic force fixedly-connecting device A102; the front panel base 13 may be connected to a host and a power supply, respectively, and the front panel module group 10 performs data communication with the host through the front panel base 13, and the power supply supplies power to the front panel module group 10 through the front panel base 13. Specific:
the front panel module group 10 of the present invention may be a single upper panel unit module 11, or may be a combination of an upper panel unit module 11 and a lower panel unit module 12; when the front panel module group 10 is an independent upper panel unit module 11, the universal interface module a102 and the adaptive magnetic force fixing device a102 are correspondingly arranged on the upper panel unit module 11. As shown in fig. 4, the surface layer of the upper panel unit module 11 is a simulation interface of the upper half of the front part of the aircraft cabin, the middle layer is a control circuit for operation and a core machine for display control, and the bottom layer is a universal interface module a101 and a self-adaptive magnetic force fixedly-connecting device a102. As shown in fig. 2 and 4, when the front panel module group 10 is a combination of an upper panel unit module 11 and a lower panel unit module 12, the surface layer of the upper panel unit module 11 is a simulation interface of the upper half part of the front part of the aircraft cabin, the middle layer is a control circuit for operation and a core machine for display control, and the bottom layer is a universal interface module E111, a lock catch a112 and a self-adaptive magnetic force fixedly-connecting device a102; the surface layer of the lower panel unit module is a simulation interface of the lower half part of the front part of the aircraft cabin, the middle layer is a control circuit for operation and a core machine for display control, and the bottom layer is a universal interface module F121 matched with a universal interface module E111, a lock catch B122 matched with a lock catch A112 and a universal interface module A101; the lock catch structure formed by the lock catch A112 and the lock catch B122 is a vehicle safety belt lock catch, and the mechanical fixedly connection of the upper panel unit module 11 and the lower panel unit module 12 is realized through the lock catch A112 and the lock catch B122; the self-adaptive magnetic force fixing device A102 and the self-adaptive magnetic force fixing device B132 are two parts of the self-adaptive magnetic force fixing device, when the self-adaptive magnetic force fixing device is electrified, the fixing of the upper panel unit module 11 and the front panel base 13 is realized through the adsorption fixing of the self-adaptive magnetic force fixing device A102 and the self-adaptive magnetic force fixing device B132, and when the self-adaptive magnetic force fixing device is powered off, the adsorption force of the self-adaptive magnetic force fixing device A102 and the self-adaptive magnetic force fixing device B132 disappears, and the upper panel unit module 11 and the front panel base 13 can be detached. After the upper panel unit module 11 and the lower panel unit module 12 are assembled, the lock catch A112 and the lock catch B122 are buckled and locked, the universal interface module A101 is in butt joint with the universal interface module B131, the universal interface module E111 is in butt joint with the universal interface module F121, and the self-adaptive magnetic force fixedly connecting device A102 and the self-adaptive magnetic force fixedly connecting device B132 are adsorbed and fixed; the universal interface module a101 and the universal interface module B131, and the universal interface module E111 and the universal interface module F121 are male and female connectors of the universal interface module, and the universal interface module may be a 36-pin universal interface.
Specifically, the mechanical structures of the upper panel unit module 11 and the lower panel unit module 12 as shown in fig. 5 to 6; the upper panel unit module 11 and the lower panel unit module 12 form a T-shaped structure, a slot 113 for inserting the upper end of the lower panel unit module 12 is formed in the middle of the upper panel unit module 11, a universal interface module E111 and a lock catch a112 are arranged at the bottom of the slot 113, a universal interface module F121 and a lock catch B122 are arranged at the upper end of the lower panel unit module 12, and after the lock catch a112 and the lock catch B122 are locked, the universal interface module E111 is in butt joint with the universal interface module F121. Further, in order to facilitate the smooth insertion and connection of the lower panel unit module 12 along the slot 113, the side wall of the slot 113 is provided with a sliding rail 114, and the side wall of the lower panel unit module 12 is provided with a sliding groove 123 corresponding to the sliding rail 114; further, the upper panel unit module 11 is provided with a pin hole a115 through which the safety pin a passes, and the lower panel unit module 12 is provided with a pin hole B124 through which the safety pin a passes; after the upper panel unit module 11 and the lower panel unit module 12 are locked by the lock catches a112 and B122, the upper panel unit module 11 and the lower panel unit module 12 can be further inserted into the pin holes a115 and B124 in sequence by the safety pin a, so that further locking of the upper panel unit module 11 and the lower panel unit module 12 is realized.
Specifically, as shown in fig. 7-8, the front panel base 13 has a pi-shaped structure formed by two support columns 133 and a cross beam 134, a back plate 135 is fixed in the middle of the cross beam 134, a vertical guide rail 136 and a universal interface module B131 are arranged on the back plate 135, and a guide block 116 is arranged on the back surface of the upper panel unit module 11 corresponding to the vertical guide rail 136, as shown in fig. 6; two self-adaptive magnetic force fixing devices B132 are arranged on the cross beam 134 and are positioned on two sides of the back plate 135, and a supporting plate 137 for bearing the upper panel unit module 11 is arranged on the cross beam 134; when the guide blocks 116 slide into the vertical guide rails 136 and the upper panel unit module 11 abuts against the supporting plate 137, the universal interface module a101 abuts against the universal interface module B131, and the adaptive magnetic force fixing device a102 abuts against the adaptive magnetic force fixing device B132. Further, as shown in fig. 6, a hanging block 117 for hanging on the top of the back plate 135 is provided on the back surface of the upper panel unit module 11, a pin hole C118 through which the safety pin B passes is provided on the hanging block 117, and a pin hole D138 through which the safety pin B passes is provided on the back plate 135; after the self-adaptive magnetic force fixing device A102 and the self-adaptive magnetic force fixing device B132 are adsorbed and locked, the self-adaptive magnetic force fixing device A and the self-adaptive magnetic force fixing device B can be further inserted into the pin hole C118 and the pin hole D138 in sequence through the safety pin B, so that the upper panel unit module 11 and the front panel base 13 can be further locked.
Specifically, as shown in fig. 7 and 8, the support post 133 of the present invention is provided with a folding device 14 for turning over the folding cross beam 134, the front panel base 13 before turning over is shown in fig. 7, and the front panel base 13 after turning over is shown in fig. 8. Specifically, as shown in fig. 9, the folding device 14 includes a first fixing member 141 mounted on the upper support column, a second fixing member 142 mounted on the lower support column, a lock shaft 143, and a handle 144, the first fixing member 141 being hinged to the second fixing member 142 by a hinge shaft 148; the first fixing piece 141 is provided with a guide hole 145, the second fixing piece 142 is provided with a clamping groove 146, the lock shaft 143 horizontally penetrates through the guide hole 145, the middle part of the lock shaft 143 is connected to the second fixing piece 142 through a spring 147, and two ends of the lock shaft 143 are hinged with handles 144; in the initial state (the spring is in a natural state or a tensile state), the lock shaft 143 is clamped into the clamping groove 146 under the action of the spring 147, and the upper support column and the lower support column of the support column 133 are locked, and the schematic diagram after locking is shown in fig. 7; pulling the pull handle 144 upward, the lock shaft 143 is moved in the guide hole 145 and out of the catch groove 146, and the upper support column and the cross beam can be turned and folded.
As shown in fig. 1, 3 and 4, each side panel 2 of the present invention comprises a side panel module group 20 for simulating instruments and equipment on both sides of a cabin and a side panel base 22 matched with the side panel module group 20, wherein the side panel base 22 is installed on a base of the simulated cabin; the side panel module group 20 is provided with at least one universal interface module C201 and at least one self-adaptive magnetic force fixedly-connecting device C202, the side panel base 22 is provided with a universal interface module D221 corresponding to the universal interface module C201, and the side panel base 22 is provided with a self-adaptive magnetic force fixedly-connecting device D222 corresponding to the self-adaptive magnetic force fixedly-connecting device C202; wherein, the universal interface module C201 and the universal interface module D221 are the male and female heads of the universal interface module, and the universal interface module can be selected from the existing universal 36-pin universal interface; the self-adaptive magnetic force fixing device C202 and the self-adaptive magnetic force fixing device D222 are two parts of the self-adaptive magnetic force fixing device, when the self-adaptive magnetic force fixing device is powered on, the side panel module group 20 and the side panel base 22 are fixed through the adsorption fixing of the self-adaptive magnetic force fixing device C202 and the self-adaptive magnetic force fixing device D222, and when the self-adaptive magnetic force fixing device is powered off, the adsorption force of the self-adaptive magnetic force fixing device C202 and the self-adaptive magnetic force fixing device D222 disappears, and the side panel module group 20 and the side panel base 22 can be detached. The side panel base 22 may be connected to a host and a power source, respectively, and the side panel module group 20 performs data communication with the host through the side panel base 22, and the power source supplies power to the side panel module group 20 through the side panel base 22.
Specifically, as shown in fig. 10-12, the side panel module group 20 is a rectangular structure formed by a plurality of side panel unit modules 21, the surface layer of each side panel unit module 21 is an aircraft cabin side simulation interface, the middle layer is a control circuit for operation and a core machine for display control, and the bottom layer is a universal interface module C201 and an adaptive magnetic force fixing device C202, as shown in fig. 4; the side panel base 22 has a rectangular structure, the universal interface module D221 is installed on the side panel base 22 corresponding to the universal interface module C201 of all the side panel unit modules 21, and the adaptive magnetic force fixing device D202 is installed on the side panel base 22 corresponding to the adaptive magnetic force fixing device C202 of all the side panel unit modules 21; further, the side panel base 22 is provided with a receiving groove for receiving different side panel unit modules 21, and the receiving groove can limit the frame of the side panel unit module 21; if the side panel is to be used for a long time, the long-term fixedly connection is realized by screwing the jackscrew bolt.
Furthermore, the self-adaptive electromagnetic force fixedly-connecting device can ensure quick assembly and disassembly in a non-working state and can prevent error movement and error disassembly in the working state; the panel module uses the structure of the safety belt lock catch (lock catch A and lock catch B) for the vehicle as a mechanical fixedly connected element of the separable panel, and has the advantages of realizing the quick assembly and disassembly of the panel module and being convenient for collection and transportation; the panel module uses a special universal interface bus (36-pin universal interface) which is suitable for simulation needs for the first time in the field of flight simulation equipment, and realizes communication link with a simulation computer through a special digital-to-analog conversion device instead of using a real aircraft bus; further, the upper panel unit module and the lower panel unit module are combined by using sliding rail and sliding chute type combinations, the panel unit modules can be disassembled and stored, and the front panel base can be folded and stored into a rectangular square cabinet through the folding device.
Further, as shown in fig. 4, the upper, lower, and side panel unit modules of the panel module may be divided into three layers: the surface layer is an aircraft cabin simulation interface, comprises various instrument display and operation switches and buttons, the interface is completely consistent with the functions of a real cabin interface, each panel unit module is used for simulating a certain function module of the cabin, and the combination of all panel unit modules is used for constructing the full simulation of the cabin so as to realize the human-computer interaction function consistent with the real cabin; the middle layer uses a miniature built-in display control core machine and a control circuit to realize instrument display and processing of the simulation cabin interface, and a large-scale server is not required to be externally connected in use; the core machine can be replaced conveniently; the invention does not change the structure and the working mode of the core machine, but configures the core machine and the control circuit needed by the simulation cabin of different models; the control circuit comprises a singlechip, the control circuit is connected with each electronic element on the surface layers of the upper side panel unit module, the lower side panel unit module and the upper side panel unit module, operation variables of each element are collected and input into the singlechip, the singlechip transmits operation signals to the host through a USB and a network interface after processing according to a built-in program, the singlechip also receives main instructions through the USB and the network, and the singlechip controls each element connected with the circuit to execute corresponding functions such as lamp lighting and extinguishing, built-in motor actuation and the like after processing through the built-in program; the bottom layer is a universal interface module and various fixing devices, the universal interface module is in butt joint with the interfaces of the base for data communication and power supply, the fixing devices comprise self-adaptive magnetic fixing devices or safety belt locking structures for vehicles and the like, and the universal interface module is prevented from being loosened due to error disassembly or error operation during connection reinforcement with the base and working. Wherein each panel unit module is individually replaceable; all lines connecting the surface, middle and bottom layer elements between the upper, lower or side panel unit modules are fixed using thermally conductive silicone to increase reliability.
Furthermore, the front panel base and the side panel base of the invention are all universal and mainly comprise a universal interface module and various fixing devices. The positions of the universal interface modules and the fixing devices of all the bases are fixed, and the bases can be used for cabins of different types. The universal interface module adopts standardized design, and the interface is opposite to the universal interface module of the panel unit module, so that the universal interface module is convenient to realize butt joint and is used for data communication and power supply between the universal interface module and the panel unit module. The fixing device mainly comprises a self-adaptive magnetic fixing device, a locking structure of a safety belt for a vehicle, a sliding rail and a sliding block, a safety pin and the like. The fixing device of each base comprises one or more of the fixing devices for reinforcing the connection between the base and the panel unit module and preventing the universal interface module from loosening caused by the false disassembly or the false operation during the work.
Furthermore, the panel module is only required to be simply connected in a butt joint mode when being combined, and cables and an additional fixedly connecting device are not required, so that quick assembly and disassembly are realized; meanwhile, the panel module realizes backup connection by using the safety pin and is used as strength backup of a fixedly connecting mode, and the panel module is prevented from being detached by mistake during working.
The invention provides a disassembly and assembly mode of a simulation cabin panel module for flight simulation, which comprises the following steps:
1. the panel module of the simulation trainer can be completely contained in the rectangular square cabinet for storage after being folded; when the folding device is installed and used, the bottom base is pulled out firstly, and after the bottom base is fixed in place, the folding device on the front panel base bracket is unfolded, so that the bracket is installed in place.
2. And taking out the upper and lower unit modules of the front panel, inserting the lower unit modules of the front panel into the upper unit modules of the front panel along the sliding rails, locking and fixing the upper unit modules by using the safety belt for the vehicle, combining the upper unit modules and the lower unit modules into the front panel, and then installing the front panel on the backboard of the front panel base to enable the front panel to be in butt joint with the universal interface module of the base. And (5) finishing the installation of the front panel module group.
3. The corresponding unit modules of the side panels are in turn mounted to the side panel base in registry with the universal interface modules of the base.
4. The safety pin is inserted into the corresponding pin hole, and the safety pin cannot be pulled out when the safety pin is disassembled in a non-outage mode. So far, the whole panel module is installed and can be electrified.
5. If long-term use is needed, jackscrew bolts are additionally arranged at corresponding positions of the base to be screwed. Realizing long-term fixation.
6. After the power is on, the self-adaptive magnetic force fixedly-connecting device works to adsorb the panel on the base, so that misoperation and disassembly are prevented.
7. After being electrified, each panel unit module performs self-checking, and the self-checking can work normally. And if the self-test is not passed, the corresponding panel unit module needs to be powered off and replaced.
8. When the self-adaptive magnetic force fixing device is detached after use, the power supply is disconnected, the self-adaptive magnetic force fixing device does not work any more, the safety pins are pulled out one by one, the front panel is separated from the front panel base, the safety belt lock catch for the automobile of the unit module on the front panel is pressed, the lower panel unit module is pulled out along the sliding rail, and the upper unit module and the lower unit module are separated and stored.
9. The folding device on the front panel base bracket is closed, so that the bracket is rotated by 90 degrees to fold and is parallel to the cross rod, thereby being convenient for storage.
10. And sequentially taking down each unit module on the side panel base, and if a jackscrew bolt exists, taking down the jackscrew bolt.
11. Pushing the bottom base into the rectangular cabinet body, and completing folding and storage.
When the panel needs to be replaced, the power supply is firstly disconnected, the self-adaptive magnetic force fixedly-connecting device does not work any more, the core machine does not work any more, and the corresponding panel unit module is replaced.
When the core machine needs to be replaced, the power supply is firstly disconnected, the self-adaptive magnetic force fixedly-connecting device does not work any more, and the core machine does not work any more. And pulling out the data circuit interface of the panel and the data interface of the core machine through corresponding maintenance holes, and then replacing the core machine.
The invention has the advantages that:
1. simple structure, convenient maintenance, and obvious advantages of reliability and cost effectiveness.
2. The interface is universal, the group is matched according to the need, and the advantages of adaptability and popularization are obvious.
3. The method can be used for tightly combining the requirements of multiple-mode application scenes, flexibly configuring the panel unit combination, rapidly realizing the simulation requirements of all cabin interfaces of different types, effectively avoiding the waste of resources and repeated research and development, and creating conditions for standardization, systemization and networking of aviation education, training and innovation experiments.
The above is only a preferred embodiment of the present invention, and is not intended to limit the present invention, but various modifications and variations can be made to the present invention by those skilled in the art. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (1)
1. The simulation cabin panel module for flight simulation is characterized by comprising the following components:
a front panel and two side panels;
the front panel comprises a front panel module group for simulating instruments and equipment on the front face of the cabin and a front panel base matched with the front panel module group, wherein a universal interface module A and at least one self-adaptive magnetic force fixedly-connecting device A are installed on the front panel module group, a universal interface module B is installed on the front panel base corresponding to the universal interface module A, and a self-adaptive magnetic force fixedly-connecting device B is installed on the front panel base corresponding to the self-adaptive magnetic force fixedly-connecting device A; the front panel module group is an upper panel unit module, the surface layer of the upper panel unit module is a simulation interface of the upper half part of the front part of the aircraft cabin, the middle layer is a control circuit for operation and a core machine for display control, and the bottom layer is the universal interface module A and the self-adaptive magnetic force fixedly-connecting device A; or the front panel module group is of a T-shaped structure formed by an upper panel unit module and a lower panel unit module; the surface layer of the upper panel unit module is a simulation interface of the upper half part of the front part of the aircraft cabin, the middle layer is a control circuit for operation and a core machine for display control, and the bottom layer is a universal interface module E, a lock catch A and the self-adaptive magnetic force fixedly-connecting device A; the surface layer of the lower panel unit module is a simulation interface of the lower half part of the front part of the aircraft cabin, the middle layer is a control circuit for operation and a core machine for display control, and the bottom layer is a universal interface module F matched with the universal interface module E, a lock catch B matched with the lock catch A and the universal interface module A; the middle part of the upper panel unit module is provided with a slot for inserting the upper end of the lower panel unit module, the bottom of the slot is provided with a universal interface module E and a lock catch A, the upper end of the lower panel unit module is provided with a universal interface module F and a lock catch B, and after the lock catch A and the lock catch B are locked, the universal interface module E is in butt joint with the universal interface module F;
each side panel comprises a side panel module group for simulating instruments and equipment on two sides of a cabin and a side panel base matched with the side panel module group, wherein at least one universal interface module C and at least one self-adaptive magnetic force fixedly-connecting device C are installed on the side panel module group, a universal interface module D is installed on the side panel base corresponding to the universal interface module C, and a self-adaptive magnetic force fixedly-connecting device D is installed on the side panel base corresponding to the self-adaptive magnetic force fixedly-connecting device C; the surface layer of each side panel unit module is an aircraft cabin side simulation interface, the middle layer is a control circuit for operation and a core machine for display control, and the bottom layer is the universal interface module C and the self-adaptive magnetic force fixedly-connecting device C;
a sliding rail is arranged on the side wall of the slot, and a sliding groove is arranged on the side wall of the lower panel unit module corresponding to the sliding rail;
the upper panel unit module is provided with a pin hole A for the safety pin A to pass through, and the lower panel unit module is provided with a pin hole B for the safety pin A to pass through;
the front panel base is of a pi-shaped structure formed by two support columns and a cross beam;
a backboard is fixed in the middle of the cross beam, a vertical guide rail and a universal interface module B are arranged on the backboard, and a guide block is arranged on the back surface of the upper panel unit module corresponding to the vertical guide rail; the two self-adaptive magnetic force fixedly connected devices B are arranged on the cross beam and positioned on two sides of the back plate, and a supporting plate for bearing the upper panel unit module is arranged on the cross beam; when the guide blocks slide into the vertical guide rails and the upper panel unit modules are propped against the supporting plates, the universal interface module A is in butt joint with the universal interface module B, and the self-adaptive magnetic force fixedly-connecting device A is in butt joint with the self-adaptive magnetic force fixedly-connecting device B;
the support column is provided with a folding device for overturning and folding the cross beam;
the folding device comprises a first fixing piece arranged on the upper support column, a second fixing piece arranged on the lower support column, a lock shaft and a handle, wherein the first fixing piece is hinged on the second fixing piece through a hinge shaft;
the first fixing piece is provided with a guide hole, the second fixing piece is provided with a clamping groove, the lock shaft horizontally penetrates through the guide hole, the middle part of the lock shaft is connected to the second fixing piece through a spring, and the two ends of the lock shaft are hinged with the handles; in an initial state, the lock shaft is clamped into the clamping groove under the action of the spring, and the upper support column and the lower support column of the support column are locked; the handle is pulled upwards, the lock shaft leaves the clamping groove, and the upper support column and the cross beam are turned and folded;
the back of the upper panel unit module is provided with a hanging block used for hanging on the top of the backboard, the hanging block is provided with a pin hole C for the safety pin B to pass through, and the backboard is provided with a pin hole D for the safety pin B to pass through;
the side panel module group is a rectangular structure formed by a plurality of side panel unit modules;
the side panel base is of a rectangular structure;
the universal interface module D is arranged on the universal interface module C corresponding to all the side panel unit modules on the side panel base, and the adaptive magnetic force fixedly connecting device D is arranged on the adaptive magnetic force fixedly connecting device C corresponding to all the side panel unit modules on the side panel base;
the disassembly and assembly mode steps of the simulation cabin panel module for flight simulation are as follows:
step 1: the panel module of the simulation trainer can be completely contained in the rectangular square cabinet for storage after being folded; when the folding device is installed and used, the bottom base is pulled out firstly, and after the bottom base is fixed in place, the folding device on the front panel base bracket is unfolded, and the bracket is installed in place;
step 2: taking out the upper and lower unit modules of the front panel, inserting the lower unit modules of the front panel into the upper unit modules of the front panel along the sliding rails, locking and fixing the upper unit modules by using the safety belt for the vehicle, combining the upper unit modules and the lower unit modules into the front panel, and then installing the front panel on the backboard of the front panel base to enable the front panel to be in butt joint with the universal interface module of the base; the front panel module group is installed;
step 3: sequentially mounting the corresponding unit modules of the side panels to the side panel base so as to be in butt joint with the universal interface module of the base;
step 4: the safety pin is inserted into the corresponding pin hole, and the safety pin cannot be pulled out when the safety pin is disassembled in a non-outage mode; so far, the whole panel module is completely installed, and the power can be supplied;
step 5: if long-term use is needed, jackscrew bolts are additionally arranged at corresponding positions of the base to be screwed; realizing long-term fixation;
step 6: after the power is on, the self-adaptive magnetic force fixedly-connecting device works to adsorb the panel on the base, so that misoperation and disassembly are prevented;
step 7: after being electrified, each panel unit module performs self-checking, and the self-checking can work normally; if the self-test is not passed, the corresponding panel unit module needs to be powered off and replaced;
step 8: when the self-adaptive magnetic force fixing device is disassembled after use, the power supply is disconnected, the self-adaptive magnetic force fixing device does not work any more, the safety pins are pulled out one by one, the front panel is separated from the front panel base, the safety belt lock catch for the vehicle of the unit module on the front panel is pressed, the unit module of the lower panel is pulled out along the sliding rail, and the upper unit module and the lower unit module are separated and stored;
step 9: the folding device on the front panel base bracket is closed, so that the bracket is rotated by 90 degrees to be folded, and is parallel to the cross rod, thereby being convenient for storage;
step 10: sequentially taking down each unit module on the side panel base, and if a jackscrew bolt exists, taking down the jackscrew bolt firstly;
step 11: pushing the bottom base into the rectangular cabinet body, and completing folding and storage.
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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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