CN111874262A - Aircraft wheel brake disc wearing and tearing detecting system - Google Patents
Aircraft wheel brake disc wearing and tearing detecting system Download PDFInfo
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- CN111874262A CN111874262A CN202010652099.9A CN202010652099A CN111874262A CN 111874262 A CN111874262 A CN 111874262A CN 202010652099 A CN202010652099 A CN 202010652099A CN 111874262 A CN111874262 A CN 111874262A
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- 238000001514 detection method Methods 0.000 claims abstract description 69
- 238000012423 maintenance Methods 0.000 claims abstract description 48
- 238000005299 abrasion Methods 0.000 claims abstract description 38
- 238000004458 analytical method Methods 0.000 claims abstract description 23
- 238000007405 data analysis Methods 0.000 claims abstract description 23
- 230000005540 biological transmission Effects 0.000 claims description 6
- 238000004891 communication Methods 0.000 claims description 6
- 230000001413 cellular effect Effects 0.000 claims description 4
- 238000007689 inspection Methods 0.000 abstract description 6
- 238000000034 method Methods 0.000 abstract description 2
- 238000011179 visual inspection Methods 0.000 abstract description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 5
- 229910052799 carbon Inorganic materials 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 238000004364 calculation method Methods 0.000 description 2
- 238000007728 cost analysis Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 238000004132 cross linking Methods 0.000 description 1
- 238000013479 data entry Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 235000016709 nutrition Nutrition 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/60—Testing or inspecting aircraft components or systems
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/40—Maintaining or repairing aircraft
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L67/00—Network arrangements or protocols for supporting network services or applications
- H04L67/01—Protocols
- H04L67/12—Protocols specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04Q—SELECTING
- H04Q9/00—Arrangements in telecontrol or telemetry systems for selectively calling a substation from a main station, in which substation desired apparatus is selected for applying a control signal thereto or for obtaining measured values therefrom
Abstract
The embodiment of the invention discloses a wear detection system for a brake disc of an airplane wheel of an airplane, which comprises: the system comprises airborne detection equipment, ground service maintenance equipment and operation data analysis equipment; the airborne detection equipment is connected with the brake disc and is configured to detect the brake disc abrasion loss, analyze the brake disc abrasion loss on a single airplane and send an analysis result to at least one of the airborne avionic system and the ground service maintenance equipment; the ground service maintenance equipment is configured to receive the data information sent by the airborne detection equipment and upload the data information to the operation data analysis equipment; and the operation data analysis equipment is configured to collect data information sent by the ground service maintenance equipment, and integrate and analyze the received data according to the requirements of the users. The embodiment of the invention solves the problems that the existing method for detecting the abrasion state of the brake disc of the airplane depends on manual visual inspection, increases the ground inspection time in the course operation, and brings inconvenience to the course use analysis of the brake disc and the like.
Description
Technical Field
The application relates to but not limited to the technical field of airplane wheel brake control, in particular to an airplane wheel brake disc wear detection system.
Background
In an airplane wheel brake control system, a brake disc is a key component influencing the landing safety of an airplane, and the performance and the abrasion state of the brake disc directly influence whether the airplane can land normally and ensure the safety of personnel and an airplane.
When the brake disc is worn to a certain thickness, the operation safety of the airplane must be ensured by replacing the brake disc with a new one. Therefore, with regard to the brake disc wear state, the ground crew must carry out inspection items after each landing of the aircraft. However, currently, the general airplane wheel brake wear indicating device is still in a mechanical indicating form, that is, the wear state of the brake disc needs to be checked by human eyes, the workload of ground service personnel is increased by the manual checking mode, the wear data of the brake disc is not easy to obtain, the thickness of the brake disc needs to be measured by eyes, and the wear data of the brake disc needs to be recorded by adopting a certain form to perform steps such as data entry, so that the ground checking time in the operation of the airline is increased, and inconvenience is brought to the airline use and analysis of the brake disc.
Disclosure of Invention
In order to solve the technical problems, the embodiment of the invention provides an aircraft wheel brake disc wear detection system, which aims to solve the problems that the existing detection of the wear state of an aircraft brake disc depends on manual visual inspection, the ground inspection time in the operation of a route is prolonged, the use and analysis of the route of the brake disc are inconvenient, and the like.
The embodiment of the invention provides an abrasion detection system for a brake disc of an airplane wheel, which comprises: the system comprises airborne detection equipment, ground service maintenance equipment and operation data analysis equipment;
the airborne detection equipment is connected with the airplane wheel brake disc and is configured to detect the brake disc abrasion loss, analyze the brake disc abrasion loss on a single airplane and send an analysis result to at least one of an airborne avionics system and the ground service maintenance equipment;
the ground service maintenance equipment is configured to receive data information of an analysis result sent by the airborne detection equipment, so as to instruct ground service personnel to maintain and record the brake disc according to the data information, and upload the data information to the operation data analysis equipment;
the operation data analysis equipment is configured to collect data information sent by the ground service maintenance equipment, and integrate and analyze the received data according to the requirements of users.
Optionally, in the system for detecting wear of a brake disc of an airplane wheel as described above, the onboard detection device includes: the brake wear indicator and the brake wear detection unit are connected;
wherein the brake wear indicator is connected with the wheel brake disc and is configured to acquire the wear amount of the wheel brake disc;
the brake wear detection unit is configured to receive the brake disc wear amount sent by the brake wear indicator, calculate and analyze the brake disc wear amount to obtain brake disc wear information, and send the brake disc wear information and corresponding brake disc information to at least one of the airborne avionics system and the ground service maintenance equipment.
Optionally, in the system for detecting wear of a brake disc of an airplane wheel as described above, the brake disc wear information includes: the abrasion loss of the brake disc, the residual amount of the brake disc, the residual landing times and the replacement information of the brake disc.
Optionally, in the aircraft wheel brake disc wear detection system as described above, the ground service maintenance equipment includes at least one handheld terminal device;
each handheld terminal device is configured to receive and display the data information sent by the brake wear detection unit, and upload the data information to the operation data analysis device so as to instruct ground staff to perform related recording and maintenance work of brake disc replacement, equipment maintenance and information recording according to the data information; the received data information includes: the aircraft comprises an aircraft serial number, a brake main engine wheel number, a brake disc part number, a brake disc abrasion loss, a brake disc residual amount, a residual landing frequency, brake disc replacement information and airborne equipment maintenance information.
Optionally, in the aircraft wheel brake disc wear detection system as described above, the operation data analysis device includes: an operation data center and at least one client terminal;
the operation data center is configured to collect and store data information sent by the handheld terminal equipment, and send the data information to the corresponding client terminal;
and the client terminal is configured to call the relevant data information stored in the operation data center according to a client analysis purpose, and perform secondary data analysis on the relevant data information.
Optionally, in the system for detecting abrasion of the brake disc of the airplane wheel, the brake abrasion detecting unit and the handheld intelligent terminal perform data transmission in a wireless fidelity, bluetooth or zigbee wireless communication manner.
Optionally, in the system for detecting abrasion of the brake disc of the airplane wheel as described above, the handheld intelligent terminal and the operation data center perform data transmission through a mobile cellular network or an ethernet network.
Optionally, in the system for detecting abrasion of a brake disc of an airplane wheel as described above, data transmission is performed between the operation data center and the client terminal through ethernet.
The abrasion detection system for the airplane wheel brake disc provided by the embodiment of the invention can realize automatic inspection of the abrasion state of the airplane wheel brake disc, and enables a pilot to know the current use state, expected use times and the like of the airplane wheel brake disc in real time through data processing and information sending; the ground service maintainers can know the replacement state of the brake disc, the maintenance state of the airborne detection equipment and the like; the aviation company can acquire the using state of the brake disc of the airplane in the fleet and the working state of airborne detection equipment; the brake disc manufacturer can obtain the use information of the brake disc and the like. The embodiment of the invention can simplify the checking step of the brake wear amount of ground service maintainers, shorten the ground checking time, provide a boundary airplane brake wear use analysis mode for an airline company, facilitate the operation cost analysis of the airline company, provide the product outfield use state data statistics for a brake disc manufacturer, and facilitate the development of product quality improvement work. The embodiment of the invention utilizes the idea of brake wear data informatization, has strong expansibility and has great engineering popularization value.
Drawings
The accompanying drawings are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the example serve to explain the principles of the invention and not to limit the invention.
Fig. 1 is a schematic structural diagram of a wear detection system for a brake disc of an airplane wheel according to an embodiment of the present invention;
fig. 2 is a schematic structural diagram of another aircraft wheel brake disc wear detection system according to an embodiment of the present invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, embodiments of the present invention will be described in detail below with reference to the accompanying drawings. It should be noted that the embodiments and features of the embodiments in the present application may be arbitrarily combined with each other without conflict.
The following specific embodiments of the present invention may be combined, and the same or similar concepts or processes may not be described in detail in some embodiments.
Fig. 1 is a schematic structural diagram of a wear detection system for a brake disc of an airplane wheel according to an embodiment of the present invention. The system for detecting the abrasion of the brake disc of the airplane wheel provided by the embodiment of the present invention can be used for detecting the abrasion state of the brake disc of the airplane wheel, as shown in fig. 1, the system for detecting the abrasion of the brake disc of the airplane wheel provided by the embodiment of the present invention may include: airborne detection equipment, ground service maintenance equipment and operation data analysis equipment. The abrasion detection system for the brake disc of the airplane wheel can be applied to monitoring and analyzing the brake abrasion of various airplanes adopting the brake wheel.
In the wear detection system for the airplane wheel brake disc in the embodiment of the invention, the airborne detection equipment is connected with the airplane wheel brake disc and is configured to detect the wear amount of the brake disc, analyze the wear amount of the brake disc on a single airplane and send the analysis result to at least one of the airborne avionics system and ground service maintenance equipment.
The airborne detection equipment in the embodiment of the invention can automatically check the abrasion state of the brake disc of the airplane wheel of the airplane in a connection mode with the brake disc of the airplane, the airborne avionic system is an airborne system on the airplane, and the airborne avionic system enables a pilot to know the current use state, the expected use times and the like of the brake disc of the airplane in fact through the received abrasion loss analysis result related to the brake disc of the pilot. In addition, the airborne detection equipment can send the analysis result to the airborne avionics system according to the requirement and the sending frequency, or send the analysis result to the ground service maintenance equipment, or send the analysis result to the airborne avionics system and the ground service maintenance equipment.
The ground service maintenance equipment in the embodiment of the invention is configured to be used for receiving data information sent by the airborne detection equipment by ground service personnel, wherein the data information includes but is not limited to an airplane serial number, a brake main engine wheel number, a brake disc part number, a brake disc abrasion loss, a brake disc residual amount, a residual landing frequency, brake disc replacement information, airborne equipment maintenance information and the like, so as to indicate that the ground service maintenance personnel can perform related maintenance work such as brake disc replacement, equipment maintenance, information recording and the like after receiving the related information. In addition, the ground service maintenance equipment can upload the acquired data information to the operation data analysis equipment at the same time.
The operation data analysis equipment in the embodiment of the invention is configured to collect data information sent by ground service maintenance equipment, wherein the data information comprises but is not limited to an airplane serial number, a brake host wheel number, a brake disc part number, a brake disc abrasion loss, a brake disc residual amount, a residual landing frequency, brake disc replacement information, airborne detection equipment maintenance information and the like; in addition, the operation data analysis equipment can integrate and analyze the received data according to the requirements of users, such as the statistics of the number of times of remaining brakes of the fleet, the statistics of the number of times of maintenance of the fleet airborne detection equipment, the corresponding relation between the abrasion loss of the carbon brake disc and the number of times of landing, the replacement early warning of the aircraft carbon brake disc and the like.
The operation data analysis equipment in the embodiment of the invention can integrate and analyze the collected data information according to the requirements of users, such as the statistics of the number of times of remaining brakes of a fleet, the statistics of the number of times of maintenance of onboard detection equipment of the fleet, the corresponding relation between the abrasion loss of the carbon brake disc and the number of times of landing, the replacement and early warning of the carbon brake disc of an airplane, and the like.
Optionally, fig. 2 is a schematic structural diagram of another aircraft wheel brake disc wear detection system provided in the embodiment of the present invention. On the basis of the embodiment shown in fig. 1, in the wear detection system for the brake disc of the airplane wheel provided by the embodiment of the invention, the airborne detection device comprises: the brake wear indicator and the brake wear detection unit are connected.
In the embodiment of the invention, a brake wear indicator is specifically connected with the brake disc of the airplane wheel, and the brake wear indicator is, for example, a linear displacement sensor and is configured to acquire the wear amount of the brake disc;
and the brake wear detection unit is configured to receive the brake disc wear amount sent by the brake wear indicator, calculate and analyze the received brake disc wear amount to obtain brake disc wear information, and then send the brake disc wear information and corresponding brake disc information to at least one of the airborne avionic system and the ground service maintenance equipment through a communication protocol.
In practical application, the analyzing and obtaining the brake disc wear information in the embodiment of the present invention may include: the abrasion loss of the brake disc, the residual amount of the brake disc, the residual landing times, the replacement information of the brake disc and other related data.
The ground service maintenance device in the embodiment of the present invention may include at least one handheld terminal device, for example, four handheld terminal devices are illustrated in fig. 2, that is, a handheld terminal device _1, a handheld terminal device _2, a handheld terminal device _3, and a handheld terminal device _ 4.
Each handheld terminal device in the embodiment of the invention is configured to receive and display data information sent by the brake wear detection unit, and upload the data information to an operation data analysis device so as to instruct ground service personnel to maintain and record a brake disc according to the data information; the received data information includes: the aircraft comprises an aircraft serial number, a brake main engine wheel number, a brake disc part number, a brake disc abrasion loss, a brake disc residual amount, a residual landing frequency, brake disc replacement information and airborne equipment maintenance information.
As shown in fig. 2, the nutritional data analysis device in the embodiment of the present invention includes: an operation data center and at least one client terminal; as illustrated in fig. 2, three client terminals, i.e., client terminal _1, client terminal _2, and client terminal _3 are shown.
The operation data center in the embodiment of the invention is configured to collect and store data information sent by the handheld terminal equipment and send the data information to corresponding client terminals;
and the client terminal is configured to call the brake disc information stored in the operation data center according to a client analysis purpose, and perform secondary data analysis on the brake disc information.
Further, data information is transmitted between the brake wear detection unit and the handheld intelligent terminal through wireless communication modes such as wireless fidelity (WIFI), Bluetooth (Bluetooth) or Zigbee (Zigbee).
Further, in the embodiment of the present invention, the handheld intelligent terminal and the operation data center transmit data information through a mobile cellular network or an ethernet network.
Further, the operation data center and the client terminal in the embodiment of the present invention transmit data information through the ethernet.
The abrasion detection system for the airplane wheel brake disc provided by the embodiment of the invention can realize automatic inspection of the abrasion state of the airplane wheel brake disc, and enables a pilot to know the current use state, expected use times and the like of the airplane wheel brake disc in real time through data processing and information sending; the ground service maintainers can know the replacement state of the brake disc, the maintenance state of the airborne detection equipment and the like; the aviation company can acquire the using state of the brake disc of the airplane in the fleet and the working state of airborne detection equipment; the brake disc manufacturer can obtain the use information of the brake disc and the like. The embodiment of the invention can simplify the checking step of the brake wear amount of ground service maintainers, shorten the ground checking time, provide a boundary airplane brake wear use analysis mode for an airline company, facilitate the operation cost analysis of the airline company, provide the product outfield use state data statistics for a brake disc manufacturer, and facilitate the development of product quality improvement work. The embodiment of the invention utilizes the idea of brake wear data informatization, has strong expansibility and has great engineering popularization value.
The following describes in detail the implementation of the aircraft wheel brake disc wear detection system provided by the present invention with some specific embodiments.
The application scenario of the airplane wheel brake wear detection system provided by the embodiment of the invention can be divided into three implementation cases.
First embodiment
The implementation case is used for completing an on-board display scene of the brake wear of the airplane wheel of the airplane. As shown in fig. 2, when the airplane is in a stationary state, and the onboard power supply, the avionics and other related systems, the brake wear indicator, and the brake wear detection unit are in a working state, the brake wear indicator sends brake wear data information of the current airplane wheel in real time, and the brake wear detection unit receives the brake wear information of all the airplane wheels, analyzes the information, and obtains the maximum wear amount data of the current airplane wheel as the wear indication data of the current airplane wheelmAnd comparing the measured values with a preset maximum wear thresholdTCalculating the residual wear amountRThe calculation formula is as follows:
R＝m-T(ii) a And pass a known single average amount of wearaverageAnd calculating to obtain the residual landing times, wherein the calculation formula is as follows: n ═ NR/average. The brake wear detection unit is in cross-linking with the airborne avionic system, information such as residual wear amount of braking of each airplane wheel, residual landing times, carbon brake disc replacement reminding and the like is uploaded to the airborne avionic system through communication, and the airborne avionic system receives relevant information and then sends the information to the cockpit display system. Further, the pilot may navigate through the cockpit display systemThe landing gear display page in the system can observe the residual abrasion loss of each wheel brake on the airplane, the residual landing times, whether the brake needs to be replaced and other related information.
Second embodiment
The implementation case is used for completing the ground detection scene before the takeoff of the airplane. As shown in fig. 2, when the airplane is in a stationary state, and the onboard power system, the brake wear detection unit, and the brake wear indicator are in a working state, the brake wear indicator sends wear data of the current airplane wheel in real time, and after the brake wear detection unit receives the brake wear data of all the airplane wheels, the remaining wear amount of the airplane wheel, the remaining landing times, the brake disc replacement information, the maintenance information of the onboard detection device, and the like are obtained through analysis. Ground service maintainer uses handheld intelligent terminal, is connected through wireless communication with brake wear detecting element, and brake wear detecting element will after connecting information and aircraft serial number send to handheld intelligent terminal, handheld intelligent terminal is according to receiving information combines the airline operation maintenance strategy, will information and corresponding maintenance strategy feed back to ground service maintainer, if change brake disc, machine carries check-out equipment etc.. And the ground service maintainer carries out the maintenance of the airplane wheel brake and the airborne detection equipment according to the information and the maintenance strategy.
Third embodiment
The implementation case is used for completing the analysis scene of the brake disc route operation data. As shown in fig. 2, after the local staff uses the handheld intelligent terminal to complete the maintenance and inspection of the brake wear amount of the airplane wheel of the airplane on the same day, the brake wear information of the airplane wheel and the maintenance information of the onboard equipment are uploaded to the operation data center from the handheld intelligent terminal through the mobile cellular network or the ethernet network, and the operation data center stores the received data in a classified manner according to the serial number of the airplane, the number of the brake disc pieces, and the like.
The airline company uses the customer terminal to read the stored data in the operation data center through the Ethernet, and carries out analysis formula customization on the customer terminal, such as information of the change of the abrasion loss of each landing brake under a certain airplane serial number, the replacement times of a brake disc of a certain airplane serial number, the use landing times of a brake disc part number and the like, and carries out deep analysis by combining the airline operation cost data.
The brake disc manufacturer reads the stored data in the operation data center through the Ethernet by using a client terminal, and carries out analysis formula customization on the client terminal, such as the landing times used by a certain brake disc part number, the residual abrasion loss and the residual landing times of a certain brake disc part number, and the average abrasion loss of the brake disc target machine type by combining the brake disc production and manufacturing informationaverageUpdating is performed while optimizing the production manufacturing process.
Although the embodiments of the present invention have been described above, the above description is only for the convenience of understanding the present invention, and is not intended to limit the present invention. It will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the spirit and scope of the invention as defined by the appended claims.
Claims (8)
1. An aircraft wheel brake disc wear detection system, comprising: the system comprises airborne detection equipment, ground service maintenance equipment and operation data analysis equipment;
the airborne detection equipment is connected with the airplane wheel brake disc and is configured to detect the brake disc abrasion loss, analyze the brake disc abrasion loss on a single airplane and send an analysis result to at least one of an airborne avionics system and the ground service maintenance equipment;
the ground service maintenance equipment is configured to receive data information of an analysis result sent by the airborne detection equipment, so as to instruct ground service personnel to maintain and record the brake disc according to the data information, and upload the data information to the operation data analysis equipment;
the operation data analysis equipment is configured to collect data information sent by the ground service maintenance equipment, and integrate and analyze the received data according to the requirements of users.
2. An aircraft wheel brake disc wear detection system as claimed in claim 1, wherein the on-board detection apparatus comprises: the brake wear indicator and the brake wear detection unit are connected;
wherein the brake wear indicator is connected with the wheel brake disc and is configured to acquire the wear amount of the wheel brake disc;
the brake wear detection unit is configured to receive the brake disc wear amount sent by the brake wear indicator, calculate and analyze the brake disc wear amount to obtain brake disc wear information, and send the brake disc wear information and corresponding brake disc information to at least one of the airborne avionics system and the ground service maintenance equipment.
3. An aircraft wheel brake disc wear detection system according to claim 2, wherein the brake disc wear information includes: the abrasion loss of the brake disc, the residual amount of the brake disc, the residual landing times and the replacement information of the brake disc.
4. An aircraft wheel brake disc wear detection system according to claim 2, wherein the ground service maintenance equipment includes at least one hand-held terminal device;
each handheld terminal device is configured to receive and display the data information sent by the brake wear detection unit, and upload the data information to the operation data analysis device so as to instruct ground staff to perform related recording and maintenance work of brake disc replacement, equipment maintenance and information recording according to the data information; the received data information includes: the aircraft comprises an aircraft serial number, a brake main engine wheel number, a brake disc part number, a brake disc abrasion loss, a brake disc residual amount, a residual landing frequency, brake disc replacement information and airborne equipment maintenance information.
5. An aircraft wheel brake disc wear detection system according to claim 3, wherein the operational data analysis device includes: an operation data center and at least one client terminal;
the operation data center is configured to collect and store data information sent by the handheld terminal equipment, and send the data information to the corresponding client terminal;
and the client terminal is configured to call the relevant data information stored in the operation data center according to a client analysis purpose, and perform secondary data analysis on the relevant data information.
6. The aircraft wheel brake disc wear detection system of claim 5, wherein the brake wear detection unit and the hand-held intelligent terminal are in data transmission through wireless fidelity, Bluetooth or Zigbee wireless communication.
7. The aircraft wheel brake disc wear detection system of claim 5, wherein the hand-held intelligent terminal and the operation data center are in data transmission through a mobile cellular network or an Ethernet network.
8. An aircraft wheel brake disc wear detection system according to claim 5, characterized in that data transmission between the operations data center and the client terminal is performed through Ethernet.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010652099.9A CN111874262A (en) | 2020-07-08 | 2020-07-08 | Aircraft wheel brake disc wearing and tearing detecting system |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202010652099.9A CN111874262A (en) | 2020-07-08 | 2020-07-08 | Aircraft wheel brake disc wearing and tearing detecting system |
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| CN111874262A true CN111874262A (en) | 2020-11-03 |
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| CN202010652099.9A Pending CN111874262A (en) | 2020-07-08 | 2020-07-08 | Aircraft wheel brake disc wearing and tearing detecting system |
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| CN1446158A (en) * | 2000-08-04 | 2003-10-01 | 都恩罗普空间技术有限公司 | Brake condition monitoring |
| US20060144997A1 (en) * | 2004-11-18 | 2006-07-06 | Schmidt R K | Method and system for health monitoring of aircraft landing gear |
| US20070112489A1 (en) * | 2005-11-16 | 2007-05-17 | Avery Robert L | Integrated maintenance and materials services for fleet aircraft using aircraft data to improve maintenance quality |
| CN102963533A (en) * | 2012-12-14 | 2013-03-13 | 中国航空工业集团公司上海航空测控技术研究所 | Helicopter health and usage monitoring system (HUMS) and method thereof |
| CN104074897A (en) * | 2013-03-27 | 2014-10-01 | 梅西耶-布加蒂-道提公司 | Method of managing the lifetime of a stack of disks of an aircraft brake |
| US20150025735A1 (en) * | 2013-07-16 | 2015-01-22 | Honeywell International Inc. | Aircraft brake health monitoring system and method |
| CN110194279A (en) * | 2018-02-27 | 2019-09-03 | 空中客车营运有限公司 | Monitoring brake equipment |
-
2020
- 2020-07-08 CN CN202010652099.9A patent/CN111874262A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1446158A (en) * | 2000-08-04 | 2003-10-01 | 都恩罗普空间技术有限公司 | Brake condition monitoring |
| US20060144997A1 (en) * | 2004-11-18 | 2006-07-06 | Schmidt R K | Method and system for health monitoring of aircraft landing gear |
| US20070112489A1 (en) * | 2005-11-16 | 2007-05-17 | Avery Robert L | Integrated maintenance and materials services for fleet aircraft using aircraft data to improve maintenance quality |
| CN102963533A (en) * | 2012-12-14 | 2013-03-13 | 中国航空工业集团公司上海航空测控技术研究所 | Helicopter health and usage monitoring system (HUMS) and method thereof |
| CN104074897A (en) * | 2013-03-27 | 2014-10-01 | 梅西耶-布加蒂-道提公司 | Method of managing the lifetime of a stack of disks of an aircraft brake |
| US20150025735A1 (en) * | 2013-07-16 | 2015-01-22 | Honeywell International Inc. | Aircraft brake health monitoring system and method |
| CN110194279A (en) * | 2018-02-27 | 2019-09-03 | 空中客车营运有限公司 | Monitoring brake equipment |
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