CN209103664U - A kind of Noise Aerospace implementation platform - Google Patents
A kind of Noise Aerospace implementation platform Download PDFInfo
- Publication number
- CN209103664U CN209103664U CN201821825874.0U CN201821825874U CN209103664U CN 209103664 U CN209103664 U CN 209103664U CN 201821825874 U CN201821825874 U CN 201821825874U CN 209103664 U CN209103664 U CN 209103664U
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- window board
- siding
- aerospace
- noise
- frame
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- 238000012549 training Methods 0.000 abstract description 24
- 230000000694 effects Effects 0.000 description 9
- 230000008520 organization Effects 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 229920000742 Cotton Polymers 0.000 description 1
- 235000006508 Nelumbo nucifera Nutrition 0.000 description 1
- 240000002853 Nelumbo nucifera Species 0.000 description 1
- 235000006510 Nelumbo pentapetala Nutrition 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 239000007767 bonding agent Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000012797 qualification Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
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Abstract
A kind of Noise Aerospace implementation platform of the utility model, including siding, frame, stringer, siding bracket, window board and window board baffle, wherein the siding covering is arranged on the frame；The multiple frame is arranged perpendicular to ground；The window board baffle is arranged on siding；The multiple stringer is fixedly connected in parallel to each other on the frame other than window board baffle；The siding bracket is fixedly connected on two frame bottoms to keep to the side；The window board is mounted on window board baffle.The utility model provides a kind of in order to which the training of Noise Aerospace implementation can save trained cost, facilitate the Noise Aerospace implementation platform of teaching according to the training platform of the training needs covering of replacement riveting in real time.
Description
Technical field
The utility model belongs to aviation teaching mode technical field more particularly to a kind of Noise Aerospace implementation platform.
Background technique
According to training program in the portion CCAR-147 regulations and the relevant regulations in the portion CCAR-66 examination outline, aircraft is tieed up
Repairing middle Noise Aerospace has strict requirements, and the mechanism for being currently undertaken by aircraft maintenance training is more to equipment used in student's practical operation
Numeral system is made relatively rough, since the diameter, radian, thickness of the aircraft skin of different model are different, gives implementation training
Very big inconvenience is brought, and training organization can add expenses of trainees when covering is replaced again, in addition many training organizations can not
Prototype part is provided and carries out real training, so that student cannot smoothly be engaged in prototype maintenance mans after training terminates to enter work position
Make, therefore, research and develop a kind of Noise Aerospace implementation platform there are market prospects very much.
Utility model content
The purpose of the utility model is to provide a kind of structures simply, is convenient for operation training, to meet aviation actually required
Rivet implementation platform, teaching equipment need to all be replaced by overcoming when present student's practical operation, it is at high cost, influence training effect the problem of.
In view of the deficiencies in the prior art and insufficient, the technical solution of the utility model is as follows:
A kind of Noise Aerospace implementation platform, including siding, frame, stringer, siding bracket, window board and
Window board baffle, wherein
The siding covering is arranged on the frame；
The multiple frame is arranged perpendicular to ground；
The window board baffle is arranged on siding；
The multiple stringer is fixedly connected in parallel to each other on the frame other than window board baffle；
The siding bracket is fixedly connected on two frame bottoms to keep to the side；
The window board is mounted on window board baffle.
Preferably, the central area riveting of the window board has covering.
Preferably, the window board is replaceable, and different model aircraft skin can be used in the covering.
Preferably, the window board is consistent with the radian of siding.
Preferably, the frame be five, by siding it is longitudinally split be four regions.
Preferably, there are two the window board baffle settings, it is located at the upper and lower part in two regions of keeping to the side.
Preferably, the siding uses covering.
Compared with the prior art, the utility model has the following advantages:
(1) the utility model uses interchangeable window board, carries out riveting training on window board, has used and has more renewed
Window board, next bit student carry out again implementation training, under the premise of guaranteeing training effect, it is maximum saving training organization at
This.
(2) the utility model has the advantages of convenient installation, can meet student and complete various types of rivet implementation practices.
(3) the utility model structure is simple, uses convenient for teaching.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model Noise Aerospace implementation platform；
The appended drawing reference of the utility model lists as follows:
1- siding, 2- frame, 3- stringer, 4- siding bracket, 5- window board, 6- window board baffle.
Specific embodiment
Specific embodiment of the present invention is described with reference to the accompanying drawings and embodiments:
It should be noted that structure, ratio, the size etc. illustrated in this specification institute attached drawing, only to cooperate explanation
The revealed content of book is not intended to limit the utility model enforceable so that those skilled in the art understands and reads
Qualifications, the modification of any structure, the change of proportionate relationship or the adjustment of size, can be generated not influencing the utility model
The effect of and the purpose that can reach under, should all still fall in the revealed technology contents of the utility model and obtain the range that can cover
It is interior.
Also, it is understood that term " center ", " longitudinal direction ", " transverse direction ", "upper", "lower", "front", "rear", " left side ",
The orientation or positional relationship of the instructions such as " right side ", "vertical", "horizontal", "top", "bottom", "inner", "outside" is based on the figure
Orientation or positional relationship is merely for convenience of describing the present invention and simplifying the description, rather than the dress of indication or suggestion meaning
It sets or element must have a particular orientation, be constructed and operated in a specific orientation, rather than can be real to limit the utility model
The range applied, relativeness are altered or modified, under the content of no substantial changes in technology, can be real when being also considered as the utility model
The scope applied.In addition, term " first ", " second " etc. is used for description purposes only, and is not understood to indicate or imply relatively heavy
The quantity of the property wanted or technical characteristic shown in implicitly indicating.The feature for defining " first ", " second " etc. as a result, can be expressed
Or implicitly indicate the quantity of indicated technical characteristic.Define as a result, " first ", " second " etc. feature can express or
Person implicitly includes one or more of the features.In the description of the present invention, unless otherwise indicated, " multiple " contain
Justice is two or more.
The utility model uses window board form, can replace in aviation training, be trained in real time as needed meeting
Under the premise of effect, aviation training organization cost is reduced.
The utility model is described further below in conjunction with attached drawing.
Embodiment 1
Shown in referring to Fig.1, a kind of Noise Aerospace implementation platform, including siding 1, frame 2, stringer 3, siding bracket 4, window board
5 and window board baffle 6, wherein
The covering of siding 1 is arranged on the frame 2；Siding 1 and frame 2 all compare the bulkhead of aircraft in kind, have certain
Radian.
The multiple frame 2 is arranged perpendicular to ground；Frame 2 is arranged in length and breadth with stringer 3, reaches maximum stability.
The window board baffle 6 is arranged on siding 1, marks off fixed area with window board baffle 6, is convenient for changing window
Plate 5.
The multiple stringer 3 is fixedly connected in parallel to each other on the frame 2 other than window board baffle 6；Stringer (also referred to as purlin
Item) it is the component being connected with covering and rib, effect has aerodynamic loading in stringer, it is generally involved in wing in modern wing
Overall stress --- bear wing bending moment caused by part axial force, be one of the important primary structure member in longitudinal framework, remove
Above-mentioned load effect is outer, and stringer and rib play certain supporting function to covering together.
The siding bracket 4 is fixedly connected on two 2 bottoms of frame kept to the side, and plays the role of fixed support.
The window board 5 is mounted on window board baffle 6.
Further, the central area riveting of the window board 5 has covering；Aircraft skin, which refers to, is enclosed in airframe knot
Structure is outer and is fixed on skeleton with bonding agent or rivet, forms the dimension shape component of airplane aerodynamic shape.Aircraft skin and skeleton
The stressed-skin construction constituted has compared with large bearing capacity and rigidity, and it is very light to be self-possessed, and plays receiving and transmits the work of aerodynamic loading
With.Active force is transmitted on connected fuselage wing skeleton by covering after bearing aerodynamic effect, and stress is complicated, in addition covering
It is directly contacted with the external world, so not requiring nothing more than, skin material intensity is high, plasticity is good, also requires surface smooth, has higher against corrosion
Ability.Phase or low-speed small airplane cloth (fiber crops, cotton) be used as covering, covering at this time can only bear the limited pneumatic load in part
Lotus does not participate in whole stress.The common covering of current aircraft has metal skin, laminated composite covering, sandwich covering etc..
Further, the window board 5 is replaceable, and different model aircraft skin can be used in the covering on the window board 5,
Covering after doing rivet training cannot not be reusable, because that repeated multiple times can be trained in student's practical operation, covering
Replacement rate is very high, replaces new covering by the way of replacing window board 5, greatly reduces the cost of training organization, more conducively
Training uses.
Further, the window board 5 is consistent with the radian of siding 1, guarantees Noise Aerospace implementation platform to the maximum extent
1:1 approaches prototype, brings more vivid practical operation to experience to student.
Further, the frame 2 be five, by siding 1 it is longitudinally split be four regions, ensure that entire implementation platform wall
The stability of plate will not cause entire siding to be detached from frame 2 and stringer 3 because of personnel's frequent operation during practical operation.
Further, there are two the settings of window board baffle 6, it is located at the upper and lower part in two regions of keeping to the side.
In training, generally has two groups of students while carrying out, it is to allow every group of one of student carrying out that two windows, which are arranged,
When operation, other students can have enough spaces to view and emulate, so two windows of setting are advisable.
Further, the siding 1 uses covering, and the covering that siding 1 uses does not need to replace, and effect is for implementation instruction
The practical operation sense that prototype is simulated in white silk, increases the Experience Degree of student.
The course of work:
In training process, every group of student carries out rivet training on window board 5, and post exercise covering is can not be again
, interchangeable fritter window board 5 rivets on window board 5, used the window board more renewed, next bit student again into
The training of row implementation；Window board 5 can replace the covering of different type of machines as needed.
In conclusion Noise Aerospace implementation platform according to prototype one make a comparison example make, sharpen understanding convenient for institute, according to
147 syllabus, every group of student at least completes various types of rivet implementation practices, using interchangeable fritter window
Plate rivets on window board, has used the window board more renewed, has not only facilitated boundary but also save the cost, and can guarantee learning effect.
The preferred embodiments of the present invention have been described in detail above with reference to the accompanying drawings, but the utility model is not limited to
Above embodiment can also not depart from the utility model within the knowledge of a person skilled in the art
It is made a variety of changes under the premise of objective.
Many other changes and modifications may be made without departing from the spirit and scope of the utility model.It should be appreciated that this reality
It is not limited to specific embodiment with novel, the scope of the utility model is defined by the following claims.
Claims (7)
1. a kind of Noise Aerospace implementation platform, it is characterised in that: including siding, frame, stringer, siding bracket, window board and window
Plate baffle, wherein
The siding covering is arranged on the frame；
The multiple frame is arranged perpendicular to ground；
The window board baffle is arranged on siding；
The multiple stringer is fixedly connected in parallel to each other on the frame other than window board baffle；
The siding bracket is fixedly connected on two frame bottoms to keep to the side；
The window board is mounted on window board baffle.
2. Noise Aerospace implementation platform according to claim 1, it is characterised in that: the central area of the window board rivets
There is covering.
3. Noise Aerospace implementation platform according to claim 2, it is characterised in that: the window board is replaceable, the illiteracy
Micromicro uses different model aircraft skin.
4. Noise Aerospace implementation platform according to claim 3, it is characterised in that: the radian one of the window board and siding
It causes.
5. Noise Aerospace implementation platform according to claim 4, it is characterised in that: the frame is five, by siding longitudinal direction
It is divided into four regions.
6. Noise Aerospace implementation platform according to claim 5, it is characterised in that: the window board baffle is provided with two
It is a, it is located at the upper and lower part in two regions of keeping to the side.
7. Noise Aerospace implementation platform according to claim 1-6, it is characterised in that: the siding is using illiteracy
Skin.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821825874.0U CN209103664U (en) | 2018-11-07 | 2018-11-07 | A kind of Noise Aerospace implementation platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821825874.0U CN209103664U (en) | 2018-11-07 | 2018-11-07 | A kind of Noise Aerospace implementation platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209103664U true CN209103664U (en) | 2019-07-12 |
Family
ID=67158380
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821825874.0U Active CN209103664U (en) | 2018-11-07 | 2018-11-07 | A kind of Noise Aerospace implementation platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209103664U (en) |
-
2018
- 2018-11-07 CN CN201821825874.0U patent/CN209103664U/en active Active
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| GR01 | Patent grant | ||
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| TR01 | Transfer of patent right |
Effective date of registration: 20231219 Address after: No. 339 Zhannan Avenue, Urban Rural Integration Demonstration Zone, Anyang City, Henan Province, 455100 Patentee after: Henan Jinyu Aviation Technology Co.,Ltd. Address before: 710071 room 101-102, No. 16, zhangba'er Road, high tech Zone, Xi'an, Shaanxi Province Patentee before: XI'AN GOLDENPOOL TECHNOLOGY ENGINEERING Co.,Ltd. |