CN111159818A - Airplane composite material structure outfield damage maintenance scheme pushing system and method thereof - Google Patents
Airplane composite material structure outfield damage maintenance scheme pushing system and method thereof Download PDFInfo
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- 239000002131 composite material Substances 0.000 title claims abstract description 62
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Abstract
This application belongs to aircraft combined material structure outfield damage maintenance scheme propelling movement design technical field, concretely relates to aircraft combined material structure outfield damage maintenance scheme propelling movement system, include: the outfield damage type management module is used for storing various outfield damage types of the aircraft composite material structure; a maintenance scheme management module for storing a plurality of maintenance schemes, each maintenance scheme being associated with a respective outfield damage type; the outfield damage information acquisition module is used for acquiring outfield damage information of the composite material structure of the airplane; and the maintenance scheme analysis and pushing module is used for analyzing the outfield damage information to obtain an outfield damage type corresponding to the outfield damage information and pushing a maintenance scheme associated with the outfield damage type. And relates to an aircraft composite structure outfield damage maintenance scheme pushing method implemented based on the aircraft composite structure outfield damage maintenance scheme pushing system.
Description
Technical Field
The application belongs to the technical field of pushing design of outfield damage maintenance schemes of composite structures of airplanes, and particularly relates to a pushing system and a pushing method of the outfield damage maintenance schemes of composite structures of airplanes.
Background
In order to meet the requirement of weight reduction of the current airplane structure, a large number of composite material parts are used on the airplane, so that the airplane is provided with a large number of composite material structures, the composite material structures on the airplane are inevitably damaged by high-strength use of the airplane, and if the damage cannot be maintained in time, the damage can seriously affect the safe flight of the airplane and even cause disastrous results.
At present, the damage type of the outfield damage of the composite structure of the airplane is difficult to quickly judge, and a related maintenance scheme is quickly given, so that the outfield damage of the composite structure of the airplane is difficult to timely, quickly and effectively maintain.
The present application is made in view of the above-mentioned drawbacks of the prior art.
Disclosure of Invention
The application aims to provide a pushing system and a pushing method for an outfield damage maintenance scheme of an aircraft composite material structure, so as to overcome or alleviate at least one defect of the prior art.
The technical scheme of the application is as follows:
one aspect provides an aircraft composite structure outfield damage maintenance scheme push system, including:
the outfield damage type management module is used for storing various outfield damage types of the aircraft composite material structure;
a maintenance scheme management module for storing a plurality of maintenance schemes, each maintenance scheme being associated with a respective outfield damage type;
the outfield damage information acquisition module is used for acquiring outfield damage information of the composite material structure of the airplane;
and the maintenance scheme analysis and pushing module is used for analyzing the outfield damage information to obtain an outfield damage type corresponding to the outfield damage information and pushing a maintenance scheme associated with the outfield damage type.
According to at least one embodiment of the present application, further comprising:
and the outfield damage type positioning module is used for positioning and marking the outfield damage type to the corresponding position of the airplane composite material structure graph.
According to at least one embodiment of the present application, further comprising:
the outfield damage airplane information recording module is used for recording airplane information corresponding to the outfield damage information;
and the airplane outfield damage type retrieval module is used for responding to the airplane information and retrieving the outfield damage type corresponding to the airplane information.
According to at least one embodiment of the present application, the aircraft information includes an aircraft number;
and the airplane outfield damage type retrieval module is used for responding to the airplane number and retrieving the outfield damage type corresponding to the airplane number.
According to at least one embodiment of the present application, further comprising:
and the airplane outfield damage type derivation module is used for responding to the airplane information and deriving the outfield damage type corresponding to the airplane information in a preset format.
According to at least one embodiment of the present application, the aircraft information includes aircraft model, aircraft composite structure;
the outfield damage type counting module is used for responding to the airplane model and counting to obtain an outfield damage type corresponding to the airplane model; and responding to the aircraft composite material structure, and counting the outfield damage type corresponding to the aircraft composite material structure.
According to at least one embodiment of the present application, further comprising: and the external field damage type statistic derivation module is used for deriving the external field damage type obtained through statistics in a preset format.
In accordance with at least one embodiment of the present application, a repair materials information base to store a plurality of repair materials, each repair material associated with a respective repair solution;
the maintenance protocol analysis pushing module also pushes maintenance materials associated with the maintenance protocol pushed by the maintenance protocol analysis pushing module.
In accordance with at least one embodiment of the present application, a repair materials information repository to store a plurality of repair tools, each repair tool associated with a respective repair solution;
the maintenance plan analysis pushing module also pushes the maintenance tool associated with the maintenance plan pushed by the maintenance plan analysis pushing module.
On the other hand, the method for pushing the outfield damage information maintenance scheme of the composite material structure of the airplane comprises the following steps:
storing a plurality of external field damage types of the composite material structure of the airplane;
storing a plurality of maintenance schemes, each maintenance scheme being associated with a respective outfield damage type;
storing a plurality of repair materials, each repair material associated with a respective repair protocol;
storing a plurality of service tools, each service tool associated with a respective service plan;
acquiring outfield damage information of an airplane composite material structure;
analyzing the external field damage information to obtain an external field damage type corresponding to the external field damage information, and pushing a maintenance scheme associated with the external field damage type.
Drawings
Fig. 1 is a flowchart of a pushing method for an outfield damage maintenance scheme of an aircraft composite structure according to an embodiment of the present application.
Detailed Description
The present application will be described in further detail with reference to the following drawings and examples. It is to be understood that the specific embodiments described herein are merely illustrative of the relevant application and are not limiting of the application. It should be noted that, for convenience of description, only the portions related to the present application are shown in the drawings.
It should be noted that the embodiments and features of the embodiments in the present application may be combined with each other without conflict. The present application will be described in detail below with reference to the embodiments with reference to the attached drawings.
It should be noted that in the description of the present application, the terms of direction or positional relationship 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, which are merely for convenience of description, and do not indicate or imply that the device or element must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present application. 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.
Furthermore, it should be noted that, in the description of the present application, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as being fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present application can be understood by those skilled in the art as the case may be.
The present application is described in further detail below with reference to fig. 1.
One aspect provides an aircraft composite structure outfield damage maintenance scheme push system, including:
the outfield damage type management module is used for storing various outfield damage types of the aircraft composite material structure;
a maintenance scheme management module for storing a plurality of maintenance schemes, each maintenance scheme being associated with a respective outfield damage type;
the outfield damage information acquisition module is used for acquiring outfield damage information of the composite material structure of the airplane;
and the maintenance scheme analysis and pushing module is used for analyzing the outfield damage information to obtain an outfield damage type corresponding to the outfield damage information and pushing a maintenance scheme associated with the outfield damage type.
For the system for pushing the outfield damage maintenance scheme of the aircraft composite material structure disclosed in the above embodiment, as can be understood by those skilled in the art, the maintenance scheme analysis pushing module may analyze and obtain the outfield damage type corresponding to the outfield damage information according to the obtained outfield damage information, and push the maintenance scheme associated with the outfield damage type according to the obtained outfield damage information, wherein the outfield damage type and the maintenance scheme are stored by the outfield damage type management module and the maintenance scheme management module and are associated with each other according to a certain rule, that is, different outfield damage types may be maintained by the maintenance scheme associated with them, based on which the system may realize fast pushing of the outfield damage maintenance scheme based on the outfield damage information, and the relevant maintenance personnel may fast push the outfield damage maintenance scheme based on the pushed maintenance scheme, And (5) effective maintenance.
For the aircraft composite structure outfield damage maintenance scheme pushing system disclosed in the above embodiments, it can be further understood by those skilled in the art that one outfield damage type may be associated with multiple maintenance schemes, that is, for one outfield damage type maintenance scheme, the pushing module is analyzed to push multiple maintenance schemes, and relevant maintenance personnel may select the most appropriate maintenance scheme among the multiple maintenance schemes to maintain the outfield damage according to the fact.
In some optional embodiments, further comprising:
and the outfield damage type positioning module is used for positioning and marking the outfield damage type to the corresponding position of the airplane composite material structure graph so as to realize the visualization of the outfield damage type on the airplane composite material structure.
In some optional embodiments, further comprising:
the outfield damage airplane information recording module is used for recording airplane information corresponding to the outfield damage information;
and the airplane outfield damage type retrieval module is used for responding to the airplane information and retrieving the outfield damage type corresponding to the airplane information.
For the pushing system for the outfield damage maintenance scheme of the composite material structure of the airplane disclosed in the above embodiment, those skilled in the art can understand that the aircraft outfield damage type retrieval module can retrieve the outfield damage type corresponding to the aircraft information in response to the aircraft information, so as to realize the tracing and statistics of the outfield damage type of the composite material structure of the corresponding airplane, thereby facilitating the analysis and evaluation of the outfield damage of the corresponding aircraft by the relevant personnel, and providing guidance for the maintenance and the maintenance of the outfield damage of the composite material structure of the aircraft.
In some optional embodiments, the aircraft information includes an aircraft number;
and the airplane outfield damage type retrieval module is used for responding to the airplane number and retrieving the outfield damage type corresponding to the airplane number.
In some optional embodiments, further comprising:
and the airplane outfield damage type derivation module is used for responding to the airplane information and deriving the outfield damage type corresponding to the airplane information in a preset format, wherein the preset format can comprise a file format for deriving the outfield damage type and can also comprise a presentation mode for deriving the outfield damage type.
In some alternative embodiments, the aircraft information includes aircraft model, aircraft composite structure;
the outfield damage type counting module is used for responding to the airplane model and counting to obtain an outfield damage type corresponding to the airplane model; and responding to the aircraft composite material structure, and counting the outfield damage type corresponding to the aircraft composite material structure.
For the pushing system for the outfield damage maintenance scheme of the aircraft composite material structure disclosed in the above embodiment, those skilled in the art can understand that the classification statistics of the outfield damage types according to the model of the damaged aircraft or according to the aircraft composite material structure can be realized through the outfield damage type statistics module, so that the classification analysis of the outfield damage types can be facilitated, and a certain reference is provided for the maintenance of the outfield damage.
In some optional embodiments, further comprising:
and the outfield damage type statistic derivation module is used for deriving the outfield damage type obtained by statistics in a preset format, wherein the preset format can comprise a file format for deriving the outfield damage type, and can also comprise a presentation mode for deriving the outfield damage type, and the presentation mode can be presented in a bar chart or a pie chart.
In some alternative embodiments, a repair materials information repository to store a plurality of repair materials, each repair material associated with a respective repair protocol;
the maintenance plan analysis pushing module also pushes the maintenance materials associated with the maintenance plan pushed by the maintenance plan analysis pushing module, namely, the maintenance materials required by the maintenance plan are pushed simultaneously while the maintenance plan is pushed.
In some alternative embodiments, a repair materials information repository to store a plurality of repair tools, each repair tool associated with a respective repair scenario;
the maintenance scheme analysis pushing module also pushes the maintenance tool associated with the maintenance scheme pushed by the maintenance scheme analysis pushing module, namely, the tool required by the maintenance scheme is pushed simultaneously while the maintenance scheme is pushed.
On the other hand, the method for pushing the outfield damage information maintenance scheme of the composite material structure of the airplane comprises the following steps:
storing a plurality of external field damage types of the composite material structure of the airplane;
storing a plurality of maintenance schemes, each maintenance scheme being associated with a respective outfield damage type;
storing a plurality of repair materials, each repair material associated with a respective repair protocol;
storing a plurality of service tools, each service tool associated with a respective service plan;
acquiring outfield damage information of an airplane composite material structure;
analyzing the external field damage information to obtain an external field damage type corresponding to the external field damage information, and pushing a maintenance scheme associated with the external field damage type.
For the pushing method for the outfield damage maintenance scheme of the aircraft composite material structure disclosed in the above embodiment, those skilled in the art can understand that the method is implemented based on the pushing device for the outfield damage maintenance scheme of the aircraft composite material structure disclosed in the above embodiment, and can realize the fast pushing of the outfield damage maintenance scheme based on the outfield damage information, and the related maintenance personnel can carry out fast and effective maintenance on the outfield damage according to the pushed maintenance scheme.
So far, the technical solutions of the present application have been described in connection with the preferred embodiments shown in the drawings, but it is easily understood by those skilled in the art that the scope of the present application is obviously not limited to these specific embodiments. Equivalent changes or substitutions of related technical features can be made by those skilled in the art without departing from the principle of the present application, and the technical scheme after the changes or substitutions will fall into the protection scope of the present application.
Claims (10)
1. The utility model provides an aircraft combined material structure outfield damage maintenance scheme push system which characterized in that includes:
the outfield damage type management module is used for storing various outfield damage types of the aircraft composite material structure;
a maintenance scheme management module for storing a plurality of maintenance schemes, each maintenance scheme being associated with a respective outfield damage type;
the outfield damage information acquisition module is used for acquiring outfield damage information of the composite material structure of the airplane;
and the maintenance scheme analysis and pushing module is used for analyzing the outfield damage information to obtain an outfield damage type corresponding to the outfield damage information and pushing a maintenance scheme associated with the outfield damage type.
2. The aircraft composite structure outfield damage repair scenario pushing system of claim 1, wherein:
further comprising:
and the outfield damage type positioning module is used for positioning and marking the outfield damage type to the corresponding position of the airplane composite material structure graph.
3. The aircraft composite structure outfield damage repair scenario pushing system of claim 1, wherein:
further comprising:
the outfield damage airplane information recording module is used for recording airplane information corresponding to the outfield damage information;
and the airplane outfield damage type retrieval module is used for responding to the airplane information and retrieving the outfield damage type corresponding to the airplane information.
4. The aircraft composite structure outfield damage repair scenario pushing system of claim 3,
the airplane information comprises an airplane number;
and the airplane outfield damage type retrieval module is used for responding to the airplane number and retrieving the outfield damage type corresponding to the airplane number.
5. The aircraft composite structure outfield damage repair scenario pushing system of claim 3,
further comprising:
and the airplane outfield damage type derivation module is used for responding to the airplane information and deriving the outfield damage type corresponding to the airplane information in a preset format.
6. The aircraft composite structure outfield damage repair scenario pushing system of claim 3,
the airplane information comprises airplane model and airplane composite material structure;
the outfield damage type counting module is used for responding to the airplane model and counting to obtain an outfield damage type corresponding to the airplane model; and responding to the aircraft composite material structure, and counting the outfield damage type corresponding to the aircraft composite material structure.
7. The aircraft composite structure outfield damage repair scenario push system of claim 6,
further comprising:
and the external field damage type statistic derivation module is used for deriving the external field damage type obtained through statistics in a preset format.
8. The aircraft composite structure outfield damage repair scenario push system of claim 1,
a maintenance material information base for storing a plurality of maintenance materials, each maintenance material being associated with a respective maintenance profile;
the maintenance protocol analysis pushing module also pushes maintenance materials associated with the maintenance protocol pushed by the maintenance protocol analysis pushing module.
9. The aircraft composite structure outfield damage repair scenario push system of claim 1,
a repair materials information base for storing a plurality of repair tools, each repair tool associated with a respective repair plan;
the maintenance plan analysis pushing module also pushes the maintenance tool associated with the maintenance plan pushed by the maintenance plan analysis pushing module.
10. A method for pushing an outfield damage information maintenance scheme of an aircraft composite structure is characterized by comprising the following steps:
storing a plurality of external field damage types of the composite material structure of the airplane;
storing a plurality of maintenance schemes, each maintenance scheme being associated with a respective outfield damage type;
storing a plurality of repair materials, each repair material associated with a respective repair protocol;
storing a plurality of service tools, each service tool associated with a respective service plan;
acquiring outfield damage information of an airplane composite material structure;
analyzing the external field damage information to obtain an external field damage type corresponding to the external field damage information, and pushing a maintenance scheme associated with the external field damage type.
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| CN201911378725.3A CN111159818A (en) | 2019-12-27 | 2019-12-27 | Airplane composite material structure outfield damage maintenance scheme pushing system and method thereof |
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| CN201911378725.3A CN111159818A (en) | 2019-12-27 | 2019-12-27 | Airplane composite material structure outfield damage maintenance scheme pushing system and method thereof |
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Application publication date: 20200515 |