CN211568282U - Carbon fiber retaining wall for air cargo machine - Google Patents
Carbon fiber retaining wall for air cargo machine Download PDFInfo
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- CN211568282U CN211568282U CN201922388903.2U CN201922388903U CN211568282U CN 211568282 U CN211568282 U CN 211568282U CN 201922388903 U CN201922388903 U CN 201922388903U CN 211568282 U CN211568282 U CN 211568282U
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- carbon fiber
- baffle
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- board
- frame
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Abstract
Adopt the embodiment of the utility model provides a carbon fiber barricade for air cargo machine, utilize first baffle and second baffle, effective and stable set up the composite sheet between cockpit and warehouse, the structure of composite sheet adopts high strength carbon fiber board, and set up the filler between first carbon fiber board and second carbon fiber board, kinetic energy when can effectual absorption first carbon fiber board or second carbon fiber board are strikeed, set up additional strengthening between first carbon fiber board and second carbon fiber board, the intensity of composite sheet has further been strengthened, the realization separates aircraft warehouse and cockpit, and make the barricade that sets up between them possess the intensity that meets the requirements.
Description
Technical Field
The utility model relates to an aeronautical equipment technical field especially relates to a carbon fiber barricade for aviation cargo aircraft.
Background
With the continuous development and progress of the society, air transportation is widely applied to daily life, for example, large express companies such as Shunfeng express and the like can use the air transportation, and the transportation efficiency of the express can be effectively improved by utilizing the air transportation so as to adapt to the current nervous work and life rhythm.
Because of the large demand, the current means is to refit the passenger plane with poorer performance into a cargo plane, in the refitting process, the strength of the partition between the cockpit and the cargo compartment of the airplane needs to be enhanced to ensure that the partition can effectively bear the weight of the container when the container placed in the cargo compartment is loosened and impacts the partition in the descending process of the airplane.
SUMMERY OF THE UTILITY MODEL
An object of the embodiment of the utility model is to provide a carbon fiber barricade for air cargo machine to the realization separates aircraft storehouse and cockpit, and makes the setting possess the intensity that meets the requirements at the fender between them. The specific technical scheme is as follows:
the embodiment of the utility model provides a carbon fiber barricade for air cargo machine, include: a fixed frame and a composite plate;
the composite plate is arranged in the fixed frame;
the fixed frame comprises a first baffle plate and a second baffle plate; the plane where the first baffle is located is parallel to the plane where the second baffle is located; the first baffle plate is welded between a cab and a cargo compartment of the airplane, and the plane of the baffle plate is vertical to the plane of the floor of the airplane;
the second baffle is arranged between a cab and a cargo compartment of the airplane, the second baffle is detachably connected with the top wall, the bottom wall and the two side walls of the airplane respectively, and the first baffle is positioned at one side close to the cab;
the composite board comprises a first carbon fiber board, a second carbon fiber board, a carbon fiber side board, a carbon fiber frame, a filler and a reinforcing structure;
the carbon fiber frame is a plate-shaped frame; the first carbon fiber plate covers one surface of the carbon fiber frame; the second carbon fiber plate covers the second face of the carbon fiber frame;
the reinforcing structure is fixedly arranged between the first carbon fiber plate and the second carbon fiber plate and is used for supporting the first carbon fiber plate and the second carbon fiber plate;
the filler is filled between the first carbon fiber sheet and the second carbon fiber sheet.
Optionally, the reinforcing structure is shaped like an i.
Optionally, the filler is a foam or a honeycomb plate.
Optionally, the second baffle is detachably fixed to the top wall, the bottom wall, and the two side walls of the aircraft by bolts.
The embodiment of the utility model provides a carbon fiber barricade for air cargo aircraft, in the course of passenger plane repacking cargo aircraft, weld the first baffle on the diapire of aircraft, lateral wall, roof, have good stability, place the composite sheet on the face of first baffle, and utilize the second baffle to fix the composite sheet between first baffle and second baffle, wherein, the second baffle adopts the bolt fastening, facilitate the user's dismouting, weld the first baffle in the one side that is close to the cockpit, when the container placed in the warehouse appears the circumstances of assaulting the barricade, the first baffle can effectively support the composite sheet between warehouse and cockpit, in the embodiment of the utility model, the composite sheet includes first carbon fiber board, second carbon fiber board, carbon fiber curb plate, carbon fiber frame, filler, additional strengthening, adopt above-mentioned structure, can the weight of maximum reduction composite sheet, but is higher than the baffle intensity of current high strength steel, sets up additional strengthening in the composite sheet, has further improved the intensity of composite sheet, adopt the embodiment of the utility model provides a carbon fiber barricade that aircraft cargo airplane used utilizes first baffle and second baffle, effective and stable sets up the composite sheet between cockpit and storehouse, the structure of composite sheet adopts high strength carbon fiber board, and set up the filler between first carbon fiber board and second carbon fiber board, kinetic energy when can effectual absorption first carbon fiber board or second carbon fiber board are strikeed sets up additional strengthening between first carbon fiber board and second carbon fiber board, the intensity of composite sheet has further been strengthened, the realization is separated aircraft storehouse and cockpit, and make the barricade that sets up between them possess the intensity that meets the requirements.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below.
Fig. 1 is a schematic structural diagram of a carbon fiber retaining wall for an air cargo machine according to an embodiment of the present invention;
fig. 2 is a schematic structural diagram of a composite board according to an embodiment of the present invention.
Detailed Description
The technical solution in the embodiment of the present invention will be described below with reference to the accompanying drawings in the embodiment of the present invention.
In order to realize separating aircraft warehouse and cockpit to make the shelves that set up between possess the intensity that meets the requirements, the embodiment of the utility model provides a carbon fiber barricade for air cargo machine.
Referring to fig. 1 and 2, an embodiment of the present invention provides a carbon fiber retaining wall for an air cargo machine, including: a fixed frame, a composite board 2;
the composite plate 2 is arranged in the fixed frame;
the fixed frame comprises a first baffle plate 3 and a second baffle plate 4; the plane of the first baffle 3 is parallel to the plane of the second baffle 4; the first baffle 3 is welded between a cab and a cargo compartment of the airplane, and the plane of the baffle is vertical to the plane of the floor of the airplane;
the second baffle 4 is arranged between a cockpit and a cargo compartment of the airplane, the second baffle 4 is detachably connected with the top wall, the bottom wall and two side walls of the airplane respectively, and the first baffle 3 is positioned at one side close to the cockpit;
the composite board 2 comprises a first carbon fiber board 5, a second carbon fiber board 6, a carbon fiber side board 7, a carbon fiber frame 8, a filler 9 and a reinforcing structure 10;
the carbon fiber frame is a plate-shaped frame; the first carbon fiber plate 5 is covered on one surface of the carbon fiber frame 8; the second carbon fiber plate 6 is covered on the second surface of the carbon fiber frame 8;
the reinforcing structure 10 is fixedly arranged between the first carbon fiber plate 5 and the second carbon fiber plate 6, and the reinforcing structure 10 is used for supporting the first carbon fiber plate 5 and the second carbon fiber plate 6;
the filler 9 is filled between the first carbon fiber sheet 5 and the second carbon fiber sheet 6.
Specifically, the embodiment of the utility model provides a carbon fiber barricade for air cargo aircraft, at the in-process of passenger plane repacking cargo aircraft, with first baffle 3 welding on the diapire of aircraft, lateral wall, roof, have good stability, arrange composite sheet 2 in on the face of first baffle 3, and utilize second baffle 4 to fix composite sheet 2 between first baffle 3 and second baffle 4, wherein, second baffle 4 adopts bolt fastening, convenience of customers dismouting, with first baffle 3 welding in the one side of being close to the cockpit, when the container of placing in the warehouse appears impacting the barricade the condition, first baffle 3 can effectually support composite sheet 2 between warehouse and cockpit, in the embodiment of the utility model, composite sheet 2 includes first carbon fiber plate 5, second carbon fiber plate 6, carbon fiber curb plate 7, carbon fiber frame 8, filler 9, The reinforcing structure 10 can reduce the weight of the composite board 2 to the greatest extent by adopting the structure, but the strength is higher than that of the baffle plate of the existing high-strength steel, the reinforcing structure 10 is arranged in the composite board 2, the strength of the composite board 2 is further improved, the carbon fiber retaining wall for the air cargo machine provided by the embodiment of the invention effectively and stably arranges the composite board 2 between the cockpit and the cargo hold by utilizing the first baffle plate 3 and the second baffle plate 4, the structure of the composite board 2 adopts a high-strength carbon fiber plate, the filler 9 is arranged between the first carbon fiber plate 5 and the second carbon fiber plate 6, the kinetic energy of the first carbon fiber plate or the second carbon fiber plate 6 when being impacted can be effectively absorbed, the reinforcing structure 10 is arranged between the first carbon fiber plate 5 and the second carbon fiber plate 6, the strength of the composite board 2 is further reinforced, the cargo hold of the airplane is separated from the cockpit, and the retaining wall arranged between the retaining walls has the strength meeting the requirement.
Optionally, the reinforcing structure 10 is shaped like an i.
Optionally, the filler 9 is a foam or a honeycomb plate.
Optionally, the second baffle is detachably fixed to the top wall, the bottom wall, and the two side walls of the aircraft by bolts.
The embodiment of the utility model provides a pair of carbon fiber barricade for air cargo aircraft, at the in-process of passenger plane repacking cargo aircraft, with first baffle 3 welding on the diapire of aircraft, the lateral wall, the roof, good stability has, arrange composite sheet 2 in on the face of first baffle 3, and utilize second baffle 4 to fix composite sheet 2 between first baffle 3 and second baffle 4, wherein, second baffle 4 adopts the bolt fastening, convenience of customers dismouting, with first baffle 3 welding in the one side of being close to the cockpit, when the container of placing in the warehouse appears strikeing the condition of barricade, first baffle 3 can effectually support composite sheet 2 between warehouse and cockpit, in the embodiment of the utility model, composite sheet 2 includes first carbon fiber board 5, second carbon fiber board 6, carbon fiber curb plate 7, carbon fiber frame 8, filler 9, The reinforcing structure 10 can reduce the weight of the composite board 2 to the greatest extent by adopting the structure, but the strength is higher than that of the baffle plate of the existing high-strength steel, the reinforcing structure 10 is arranged in the composite board 2, the strength of the composite board 2 is further improved, the carbon fiber retaining wall for the air cargo machine provided by the embodiment of the invention effectively and stably arranges the composite board 2 between the cockpit and the cargo hold by utilizing the first baffle plate 3 and the second baffle plate 4, the structure of the composite board 2 adopts a high-strength carbon fiber plate, the filler 9 is arranged between the first carbon fiber plate 5 and the second carbon fiber plate 6, the kinetic energy of the first carbon fiber plate or the second carbon fiber plate 6 when being impacted can be effectively absorbed, the reinforcing structure 10 is arranged between the first carbon fiber plate 5 and the second carbon fiber plate 6, the strength of the composite board 2 is further reinforced, the cargo hold of the airplane is separated from the cockpit, and the retaining wall arranged between the retaining walls has the strength meeting the requirement.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
All the embodiments in the present specification are described in a related manner, and the same and similar parts among the embodiments may be referred to each other, and each embodiment focuses on the differences from the other embodiments. The above description is only a preferred embodiment of the present invention, and is not intended to limit the scope of the present invention. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention shall fall within the protection scope of the present invention.
Claims (4)
1. A carbon fiber retaining wall for an air cargo machine, comprising: a fixed frame and a composite plate;
the composite plate is arranged in the fixed frame;
the fixed frame comprises a first baffle plate and a second baffle plate; the plane where the first baffle is located is parallel to the plane where the second baffle is located; the first baffle plate is welded between a cab and a cargo compartment of the airplane;
the second baffle is arranged between a cab and a cargo compartment of the airplane, the second baffle is detachably connected with the top wall, the bottom wall and the two side walls of the airplane respectively, and the first baffle is positioned at one side close to the cab;
the composite board comprises a first carbon fiber board, a second carbon fiber board, a carbon fiber side board, a carbon fiber frame, a filler and a reinforcing structure;
the carbon fiber frame is a plate-shaped frame; the first carbon fiber plate covers one surface of the carbon fiber frame; the second carbon fiber plate covers the second face of the carbon fiber frame;
the reinforcing structure is fixedly arranged between the first carbon fiber plate and the second carbon fiber plate and is used for supporting the first carbon fiber plate and the second carbon fiber plate;
the filler is filled between the first carbon fiber sheet and the second carbon fiber sheet.
2. The carbon fiber retaining wall for air cargo machines of claim 1, wherein said reinforcing structure is i-shaped.
3. The carbon fiber retaining wall for air cargo machines according to claim 1, wherein said filler is a foam or a honeycomb plate.
4. The carbon fiber retaining wall for air cargo aircraft as defined in claim 1, wherein said second retaining plate is detachably fixed to said top, bottom and both side walls of said aircraft by bolts.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922388903.2U CN211568282U (en) | 2019-12-26 | 2019-12-26 | Carbon fiber retaining wall for air cargo machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922388903.2U CN211568282U (en) | 2019-12-26 | 2019-12-26 | Carbon fiber retaining wall for air cargo machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211568282U true CN211568282U (en) | 2020-09-25 |
Family
ID=72551424
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922388903.2U Active CN211568282U (en) | 2019-12-26 | 2019-12-26 | Carbon fiber retaining wall for air cargo machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211568282U (en) |
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2019
- 2019-12-26 CN CN201922388903.2U patent/CN211568282U/en active Active
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