CN113872842A - Wireless control system for aviation seat - Google Patents
Wireless control system for aviation seat Download PDFInfo
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- CN113872842A CN113872842A CN202111153767.4A CN202111153767A CN113872842A CN 113872842 A CN113872842 A CN 113872842A CN 202111153767 A CN202111153767 A CN 202111153767A CN 113872842 A CN113872842 A CN 113872842A
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- 230000003993 interaction Effects 0.000 claims abstract description 27
- 238000012795 verification Methods 0.000 claims description 6
- 238000004140 cleaning Methods 0.000 abstract description 7
- 230000036544 posture Effects 0.000 description 20
- 238000000034 method Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
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- 229920001721 polyimide Polymers 0.000 description 2
- 241000700605 Viruses Species 0.000 description 1
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- 230000001070 adhesive effect Effects 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000001580 bacterial effect Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000010985 leather Substances 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 229920000515 polycarbonate Polymers 0.000 description 1
- 239000004417 polycarbonate Substances 0.000 description 1
- 238000012800 visualization Methods 0.000 description 1
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L12/00—Data switching networks
- H04L12/28—Data switching networks characterised by path configuration, e.g. LAN [Local Area Networks] or WAN [Wide Area Networks]
- H04L12/40—Bus networks
- H04L12/40006—Architecture of a communication node
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0639—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with features for adjustment or converting of seats
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- G—PHYSICS
- G08—SIGNALLING
- G08C—TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
- G08C17/00—Arrangements for transmitting signals characterised by the use of a wireless electrical link
- G08C17/02—Arrangements for transmitting signals characterised by the use of a wireless electrical link using a radio link
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04W—WIRELESS COMMUNICATION NETWORKS
- H04W12/00—Security arrangements; Authentication; Protecting privacy or anonymity
- H04W12/06—Authentication
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L12/00—Data switching networks
- H04L12/28—Data switching networks characterised by path configuration, e.g. LAN [Local Area Networks] or WAN [Wide Area Networks]
- H04L12/40—Bus networks
- H04L2012/40208—Bus networks characterized by the use of a particular bus standard
- H04L2012/40215—Controller Area Network CAN
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L12/00—Data switching networks
- H04L12/28—Data switching networks characterised by path configuration, e.g. LAN [Local Area Networks] or WAN [Wide Area Networks]
- H04L12/40—Bus networks
- H04L2012/40267—Bus for use in transportation systems
- H04L2012/4028—Bus for use in transportation systems the transportation system being an aircraft
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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- Engineering & Computer Science (AREA)
- Computer Networks & Wireless Communication (AREA)
- Signal Processing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Computer Security & Cryptography (AREA)
- Seats For Vehicles (AREA)
Abstract
The invention provides an aviation seat wireless control system, which comprises: the mobile terminal, the seat adjusting module and the communication interaction module are connected through wireless communication; the mobile terminal is used for generating a control instruction; the communication interaction module is used for receiving the control instruction and generating an action execution command according to the control instruction; the seat adjusting module is used for adjusting the posture of the aviation seat according to the action execution command. The invention does not need to lay signal wires, thereby reducing the weight of the engine room. Moreover, passengers can adjust the attitude of the aviation seat through the mobile terminal without public PCU, frequent contact and use of public equipment during epidemic situations are reduced, potential safety hazards are avoided, and meanwhile, the cleaning workload of an aviation department is reduced. Moreover, the posture of the aviation seat is adjusted conveniently and quickly through the mobile terminal.
Description
Technical Field
The invention relates to the technical field of aviation seat control, in particular to a wireless control system for an aviation seat.
Background
With the requirement of passengers on riding comfort, aviation seats capable of adjusting the postures of the seats are arranged in commercial aircraft cabins so as to provide comfortable riding environments for the passengers.
The seat control system of the prior aviation seat adopts a wired communication mode. The method specifically comprises the following steps: the external communication of the seat control system adopts a CAN bus communication mode, and the internal communication of the seat control system adopts a CAN bus or RS 485. The passenger needs to use the PCU control handle for seat attitude adjustment.
The existing seat posture control system has the following problems: 1. complex signal wires need to be arranged in the passenger cabin and the aviation seat, so that the wiring is difficult, the laying requirement is high, and the weight of the whole cabin is increased; 2. passengers need to rely on a PCU (Power control Unit) for posture adjustment, the PCU belongs to public equipment, the risk of bacterial and virus propagation can be increased, public safety is damaged, and the cleaning workload of a navigation driver is increased; 3. when the seat is in great hypsokinesis angle, the passenger hardly touches PCU, needs to stand up to adjust, and it is not convenient to use, influences riding comfort.
Disclosure of Invention
In view of the above, there is a need to provide a wireless control system for an aviation seat, which is used to solve the technical problems of potential safety hazards, large cleaning workload and inconvenient operation caused by the fact that the seat control system in the prior art adopts a wired communication method, which results in difficulty in laying, increased cabin weight and posture adjustment of passengers by means of a PCU.
In order to solve the technical problem, the invention provides an aviation seat wireless control system, which comprises: the mobile terminal, the seat adjusting module and the communication interaction module are connected through wireless communication;
the mobile terminal is used for generating a control instruction;
the communication interaction module is used for receiving the control instruction and generating an action execution command according to the control instruction;
the seat adjusting module is used for adjusting the posture of the aviation seat according to the action execution command.
In some possible implementations, the seat adjustment module includes a master control unit and a plurality of seat execution units;
the main control unit is used for receiving the action execution command and identifying the seat execution unit corresponding to the action execution command;
the seat execution unit is used for adjusting the posture of the aviation seat according to the action execution command.
In some possible implementations, the seat adjustment module further includes a seat fine adjustment unit to generate a fine adjustment command;
the main control unit is also used for receiving the fine adjustment command and identifying the seat execution unit corresponding to the fine adjustment command;
the seat execution unit is also used for adjusting the posture of the aviation seat according to the fine adjustment command.
In some possible implementations, the master control unit includes a receiving subunit, a decision subunit, and an identifying subunit;
the receiving subunit is configured to receive the action execution command and/or a fine tuning command;
the decision subunit is configured to determine a valid command of the action execution command and the fine tuning command when the receiving subunit receives the action execution command and the fine tuning command simultaneously;
the identification subunit is used for identifying the seat execution unit corresponding to the effective command.
In some possible implementation manners, the seat adjusting module further comprises a seat state feedback unit, and the seat state feedback unit is used for acquiring seat information of the aviation seat in real time and sending the seat information to the communication interaction module;
the communication interaction module is also used for sending the seat information to the mobile terminal.
In some possible implementations, the seat information includes a seat address and seat posture information corresponding to the seat address.
In some possible implementations, the seat trim unit is a flexible touch adjustment screen.
In some possible implementations, the seat adjustment module further includes a power supply unit and a voltage distribution unit;
the power supply unit is used for providing power supply voltage for the plurality of seat adjusting units;
the voltage distribution unit is used for dividing the power supply voltage into a plurality of sub-voltages which correspond to the seat execution units one by one according to a preset proportion.
In some possible implementations, the wireless control system for the airline seat further includes a crew terminal, and the communication interaction module is configured to send the seat information to the crew terminal; and the crew terminal is used for receiving and displaying the seat information.
In some possible implementation manners, the communication interaction module includes an authority verification unit, where the authority verification unit is configured to verify whether the mobile terminal has an authority, and when the mobile terminal has the authority, the communication interaction module receives the control instruction generated by the mobile terminal.
The beneficial effects of adopting the above embodiment are: according to the wireless control system for the aviation seat, the mobile terminal, the seat adjusting module and the communication interaction module which are connected in a wireless communication mode are arranged, so that the attitude of the aviation seat can be remotely adjusted, compared with the attitude of the aviation seat which is adjusted in a wired communication mode, the attitude of the aviation seat can be adjusted, signal lines do not need to be laid, and the weight of an engine room is reduced. Further, the passenger can realize the regulation to the aviation seat gesture through mobile terminal, need not to adjust through public PCU, reduces the frequent contact use of public equipment during the epidemic situation, has avoided the potential safety hazard, simultaneously, has reduced the cleaning work volume of navigation department. Moreover, the posture of the aviation seat is adjusted conveniently and quickly through the mobile terminal.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without creative efforts.
FIG. 1 is a schematic structural diagram of an embodiment of a wireless control system for an airline seat provided in the present invention;
FIG. 2 is a schematic structural view of one embodiment of a seat adjustment module provided by the present invention;
FIG. 3 is a schematic structural diagram of an embodiment of a seat fine adjustment unit provided in the present invention;
fig. 4 is a schematic structural diagram of a main control unit according to an embodiment of the present invention.
Detailed Description
The technical solution in 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. It is to be understood that the described embodiments are merely exemplary of the invention, and not restrictive of the full scope of the invention. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
In the description of the embodiments of the present invention, "a plurality" means two or more unless otherwise specified. "and/or" describes the association relationship of the associated objects, meaning that three relationships may exist, for example: a and/or B, may represent: a exists alone, A and B exist simultaneously, and B exists alone.
Reference herein to "an embodiment" means that a particular feature, structure, or characteristic described in connection with the embodiment can be included in at least one embodiment of the invention. The appearances of the phrase in various places in the specification are not necessarily all referring to the same embodiment, nor are separate or alternative embodiments mutually exclusive of other embodiments. It is explicitly and implicitly understood by one skilled in the art that the embodiments described herein can be combined with other embodiments.
The invention provides a wireless control system for an aviation seat, which is respectively explained below.
Fig. 1 is a schematic structural diagram of an embodiment of a wireless control system for an airline seat according to an embodiment of the present invention, and as shown in fig. 1, a wireless control system 10 for an airline seat according to an embodiment of the present invention includes: the mobile terminal 100, the communication interaction module 200 and the seat adjusting module 300 are connected through wireless communication;
the mobile terminal 100 is used for generating a control instruction;
the communication interaction module 200 is configured to receive a control instruction and generate an action execution command according to the control instruction;
the seat adjustment module 300 is used to adjust the attitude of the airline seat based on the action execution command.
Compared with the prior art, the aviation seat wireless control system 10 provided by the embodiment of the invention realizes remote adjustment of the attitude of the aviation seat by arranging the mobile terminal 100, the seat adjusting module 300 and the communication interaction module 200 which are connected through wireless communication, and compared with the wired communication connection, the attitude of the aviation seat is adjusted, signal lines do not need to be laid, and the weight of an engine room is reduced. Further, the passengers can adjust the attitude of the aviation seat through the mobile terminal 100 without adjusting through a public PCU, frequent contact use of public equipment during epidemic situations is reduced, potential safety hazards are avoided, and meanwhile, the cleaning workload of an aviation department is reduced. Moreover, the posture of the aviation seat is adjusted conveniently through the mobile terminal 100.
In some embodiments of the present invention, the mobile terminal 100 may be a portable terminal such as a mobile phone or a tablet computer. That is to say: the personal cell phone of each passenger can be used as the mobile terminal 100, and each passenger can adjust the attitude of the aviation seat through the personal cell phone, so that the potential safety hazard can be further reduced, the cleaning amount of an airline department is reduced, and the convenience for adjusting the attitude of the aviation seat is improved.
Since, in order to increase the comfort of the aircraft seat, the aircraft seat comprises a plurality of adjustable components, for example: a backrest, a footrest, a leg rest, a dining table, other peripherals (e.g., life jackets, oxygen masks), etc., so that, in order to avoid the misissuance of motion execution commands, in some embodiments of the present invention, as shown in fig. 2, the seat adjustment module 300 includes a main control unit 310 and a plurality of seat execution units 320;
the main control unit 310 is used for receiving the action execution command and identifying a seat execution unit 320 corresponding to the action execution command;
the seat executing unit 320 is used for adjusting the posture of the aviation seat according to the action executing command.
According to the embodiment of the invention, the main control unit 310 is arranged to identify the seat execution unit 320 corresponding to the action execution command, so that the action execution command is prevented from being mistakenly sent, and the reliability of the posture adjustment of the aircraft seat is improved.
In some embodiments of the present invention, the seat actuation unit 320 may include a back motor, a leg rest motor, a foot pedal flip motor, a foot pedal extension motor, and the like.
Further, since different passengers have different requirements for the airline seats, in some embodiments of the present invention, as shown in fig. 2, the seat adjustment module 300 further includes a seat fine adjustment unit 330, the seat fine adjustment unit 330 being configured to generate fine adjustment commands;
the main control unit 310 is further configured to receive the fine adjustment command, and identify the seat execution unit 320 corresponding to the fine adjustment command;
the seat execution unit 320 is also used for adjusting the posture of the aircraft seat according to the fine adjustment command.
According to the embodiment of the invention, the seat fine-tuning unit 330 is arranged to further adjust the attitude of the aviation seat, so that the individual requirements of different passengers on the aviation seat can be realized. Also, the fine adjustment command generated by the seat fine adjustment unit 330 is shorter in transmission path and faster in adjustment response than the control instruction generated by the mobile terminal 100.
In a preferred embodiment of the present invention, the seat fine-tuning unit 330 may be disposed on an armrest of the aircraft seat to facilitate adjustment by the passenger, thereby improving adjustment speed and convenience.
Further, to improve visualization and durability of the seat trim unit 330, in some embodiments of the present invention, the seat trim unit 330 is a flexible touch-sensitive adjustment screen.
It should be noted that: the flexible touch-adjustment screen can be touched by the passenger's hand, for example: the passenger may slide a finger with a single finger and/or with two fingers on the surface of the flexible touch-sensitive adjustment screen to generate the fine-tune command.
In one embodiment of the present invention, as shown in fig. 3, the seat fine adjustment unit 330 includes a supporting subunit 331, a flexible touch subunit 332, and an overlay 333, and in order to improve display performance, the supporting subunit 331, the flexible touch subunit 332, and the overlay 333 are bonded together by a transparent optical Adhesive (OCA).
The supporting subunit 331 is a flexible supporting subunit, and the supporting subunit 331 can be made of Polyimide (PI). The cover plate 333 is also a flexible cover plate, and the cover plate 333 may be made of any one of Polycarbonate (PC), leather, or fabric.
In order to avoid the technical problem that when the main control unit 310 receives the action execution command and the fine tuning command at the same time, it cannot be determined which command is preferentially identified, which results in disorder or even failure of the main control unit 310, in some embodiments of the present invention, as shown in fig. 4, the main control unit 310 includes a receiving subunit 311, a decision subunit 312, and an identifying subunit 313;
the receiving subunit 311 is configured to receive an action execution command and/or a fine tuning command;
the decision subunit 312 is configured to determine a valid command of the action execution command and the fine tuning command when the receiving subunit receives the action execution command and the fine tuning command simultaneously;
the identification subunit 313 is configured to identify the seat execution unit corresponding to the valid command.
According to the embodiment of the invention, the decision subunit 312 is arranged to determine the effective command in the action execution command and the fine adjustment command, so that the failure of the main control unit 310 caused by the fact that the identification subunit 313 cannot determine which command is identified when the receiving subunit 311 receives the action execution command and the fine adjustment command simultaneously can be avoided, the working order of the main control unit 310 is improved, and the reliability of the attitude adjustment of the aviation seat is further improved.
It should be noted that: the specific manner in which the decision subunit 312 determines the valid command of the action execution command and the trim command may be adjusted according to the actual situation. For example: in a particular embodiment, the action execution command has a higher priority than the trim command. Namely: when the receiving sub-unit 311 receives the action execution command and the fine adjustment command at the same time, the action execution command is a valid command.
Further, in order to facilitate the passengers to master the seat states and enable the passengers to quickly acquire the failure information when the aircraft seat fails, in some embodiments of the present invention, as shown in fig. 2, the seat adjusting module 300 further includes a seat state feedback unit 340, and the seat state feedback unit 340 is configured to acquire the seat information of the aircraft seat in real time and send the seat information to the communication interaction module 200;
the communication interaction module 200 is further configured to send the seat information to the mobile terminal 100.
By sending the seat information to the mobile terminal 100 through the communication interaction module 200, the passenger can obtain the real-time seat information through the mobile terminal, and the passenger can conveniently master the real-time seat state.
In a specific embodiment of the present invention, the seat state feedback unit 340 may include a plurality of sensors disposed on different components of the airline seat, and the seat information of the airline seat is obtained by the plurality of sensors.
Specifically, the sensors may include a backrest motor position sensor, a leg rest motor position sensor, a foot turn motor position sensor, a foot extension motor position sensor, and the like.
In a preferred embodiment of the present invention, the seat information includes a seat address and seat posture information corresponding to the seat address.
Specifically, the method comprises the following steps: the seat addresses are the addresses of the various components of the aircraft seat, for example: the addresses of the back rest and the foot rest are different.
According to the embodiment of the invention, the seat information including the seat address is set, so that passengers can quickly acquire the seat posture information of different parts of the aviation seat without recognizing the seat posture information.
Further, since the operating voltages required by the seat execution units 320 corresponding to different components of the aircraft seat are different, in order to avoid the technical problem that the seat execution units 320 fail to operate at their operating voltages due to unreasonable voltage distribution, and thus the seat execution units 320 fail, in some embodiments of the present invention, as shown in fig. 2, the seat adjustment module 300 further includes a power supply unit 350 and a voltage distribution unit 360;
the power supply unit 350 is used for supplying a power supply voltage to the plurality of seat execution units 320;
the voltage distribution unit 360 is configured to divide the power voltage into a plurality of sub-voltages corresponding to the plurality of seat actuators 320 in a one-to-one manner according to a preset ratio.
According to the embodiment of the invention, the voltage distribution unit 360 is arranged to divide the power supply voltage provided by the power supply unit 350 into the plurality of sub-voltages which are in one-to-one correspondence with the plurality of seat execution units 320, so that the reasonability of the distribution of the power supply voltage can be improved, the plurality of seat execution units 320 are ensured to work under the working voltages thereof, and the stability and the reliability of the work of the plurality of seat execution units 320 are improved.
In the embodiment of the present invention, since the operating voltage of the seat actuator unit 320 is a dc voltage of 28V or 5V, and the power supply unit 350 is an airplane voltage obtained through a cable, the airplane voltage is typically an ac voltage of 115V or 400Hz, and therefore, the power supply unit 350 is also used to convert the airplane voltage of 115V or 400Hz into a dc voltage of 28V or 5V.
Further, in order to enable the crew member to also grasp the seat information of the airline seat in real time, in some embodiments of the present invention, as shown in fig. 1, the airline seat wireless control system 10 further includes a crew terminal 400, and the communication interaction module 200 is configured to transmit the seat information to the crew terminal 400; the attendant terminal 400 is used to receive and display seat information.
By arranging the crew terminal 400 to receive the seat information, the crew can conveniently master the aviation seat in real time, and the crew can check the seat information of the aviation seat when on-duty, and can know the seat information without walking to the side of the aviation seat, so that the work efficiency of the navigation department is improved.
Further, since a plurality of airline seats are included in the cabin, in order to avoid that the airline seats are misoperated by other passengers and affect the riding comfort of the passengers, in some embodiments of the present invention, as shown in fig. 1, the communication interaction module 200 includes an authority verification unit 210, where the authority verification unit 210 is configured to verify whether the mobile terminal 100 has an authority, and when the mobile terminal 100 has the authority, the communication interaction module 200 receives the control command generated by the mobile terminal 100.
It should also be understood that: the mobile terminal 100 may include the following functional units thereon: the device comprises a backrest backward tilting and resetting unit, a leg rest extending and resetting unit, a leg rest overturning and resetting unit, a key unfolding unit, a key resetting unit, a key adjusting to working mode unit, a key adjusting to entertainment mode unit, a key adjusting to rest mode unit and the like. Specifically, the method comprises the following steps: the rest mode unit can be the posture of the corresponding aviation seat when the passenger lies for rest. Other modes are similar and are not described in detail herein.
The crew terminal 400 may include the following information prompting unit: whether the seat has a sitting unit or not, whether the backrest is an upright unit or not, whether the leg rest is an initial position unit or not, whether the dining table is an initial position unit or not, whether the motor has a fault unit or not, whether the life jacket is a tamper unit or not, and the like.
According to the wireless control system for the aviation seat, the mobile terminal, the seat adjusting module and the communication interaction module which are connected in a wireless communication mode are arranged, so that the attitude of the aviation seat can be remotely adjusted. Further, the passenger can realize the regulation to the aviation seat gesture through mobile terminal, need not to adjust through public PCU, reduces the frequent contact use of public equipment during the epidemic situation, has avoided the potential safety hazard, simultaneously, has reduced the cleaning work volume of navigation department. Moreover, the posture of the aviation seat is adjusted conveniently and quickly through the mobile terminal.
Furthermore, the main control unit is arranged to identify the seat execution unit corresponding to the action execution command, so that the action execution command is prevented from being mistakenly sent, and the reliability of posture adjustment of the aviation seat is improved. The seat fine-tuning unit is arranged to further adjust the posture of the aviation seat, so that personalized requirements of different passengers on the aviation seat can be met.
The aviation seat wireless control system provided by the invention is described in detail, and the principle and the implementation mode of the invention are explained by applying specific examples, and the description of the examples is only used for helping to understand the method and the core idea of the invention; meanwhile, for those skilled in the art, according to the idea of the present invention, there may be variations in the specific embodiments and the application scope, and in summary, the content of the present specification should not be construed as a limitation to the present invention.
Claims (10)
1. An airline seat wireless control system, comprising: the mobile terminal, the seat adjusting module and the communication interaction module are connected through wireless communication;
the mobile terminal is used for generating a control instruction;
the communication interaction module is used for receiving the control instruction and generating an action execution command according to the control instruction;
the seat adjusting module is used for adjusting the posture of the aviation seat according to the action execution command.
2. The wireless control system of an airline seat according to claim 1, wherein the seat adjustment module includes a main control unit and a plurality of seat execution units;
the main control unit is used for receiving the action execution command and identifying the seat execution unit corresponding to the action execution command;
the seat execution unit is used for adjusting the posture of the aviation seat according to the action execution command.
3. The wireless control system of an airline seat according to claim 2, wherein the seat adjustment module further includes a seat fine adjustment unit for generating fine adjustment commands;
the main control unit is also used for receiving the fine adjustment command and identifying the seat execution unit corresponding to the fine adjustment command;
the seat execution unit is also used for adjusting the posture of the aviation seat according to the fine adjustment command.
4. The wireless control system for an airline seat according to claim 3, wherein the main control unit includes a receiving subunit, a decision subunit, and an identification subunit;
the receiving subunit is configured to receive the action execution command and/or a fine tuning command;
the decision subunit is configured to determine a valid command of the action execution command and the fine tuning command when the receiving subunit receives the action execution command and the fine tuning command simultaneously;
the identification subunit is used for identifying the seat execution unit corresponding to the effective command.
5. The wireless control system of an aircraft seat according to any one of claims 1-4, wherein the seat adjusting module further comprises a seat state feedback unit, and the seat state feedback unit is configured to acquire seat information of the aircraft seat in real time and send the seat information to the communication interaction module;
the communication interaction module is also used for sending the seat information to the mobile terminal.
6. The airline seat wireless control system according to claim 5, wherein the seat information includes a seat address and seat attitude information corresponding to the seat address.
7. The wireless control system of an airline seat according to claim 3, wherein the seat fine-tuning unit is a flexible touch-sensitive adjustment screen.
8. The wireless control system of an airline seat according to claim 2, wherein the seat adjustment module further includes a power supply unit and a voltage distribution unit;
the power supply unit is used for providing power supply voltage for the plurality of seat adjusting units;
the voltage distribution unit is used for dividing the power supply voltage into a plurality of sub-voltages which correspond to the seat execution units one by one according to a preset proportion.
9. The wireless control system of an airline seat according to claim 5, further comprising a crew terminal, wherein the communication interaction module is configured to send the seat information to the crew terminal; and the crew terminal is used for receiving and displaying the seat information.
10. The wireless control system for the aircraft seat according to claim 1, wherein the communication interaction module comprises an authority verification unit, the authority verification unit is used for verifying whether the mobile terminal has the authority, and when the mobile terminal has the authority, the communication interaction module receives the control command generated by the mobile terminal.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202111153767.4A CN113872842B (en) | 2021-09-29 | 2021-09-29 | Wireless control system of aviation seat |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111153767.4A CN113872842B (en) | 2021-09-29 | 2021-09-29 | Wireless control system of aviation seat |
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| CN113872842A true CN113872842A (en) | 2021-12-31 |
| CN113872842B CN113872842B (en) | 2023-10-03 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116039929A (en) * | 2023-03-31 | 2023-05-02 | 成都旺美达航空科技有限公司 | Intelligent aviation seat adjusting method, intelligent aviation seat adjusting equipment and medium |
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| CN113872842B (en) | 2023-10-03 |
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