CN206243494U - Airplane complete machine plain cotton fabric and Aircraft protection device - Google Patents
Airplane complete machine plain cotton fabric and Aircraft protection device Download PDFInfo
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- CN206243494U CN206243494U CN201621341152.9U CN201621341152U CN206243494U CN 206243494 U CN206243494 U CN 206243494U CN 201621341152 U CN201621341152 U CN 201621341152U CN 206243494 U CN206243494 U CN 206243494U
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Abstract
The utility model provides a kind of airplane complete machine plain cotton fabric and Aircraft protection device.Airplane complete machine plain cotton fabric is divided into leading portion plain cotton fabric, middle leading portion plain cotton fabric, posterior segment plain cotton fabric and back segment plain cotton fabric, and leading portion plain cotton fabric is detachably connected with middle leading portion plain cotton fabric, and middle leading portion plain cotton fabric is detachably connected with posterior segment plain cotton fabric, and posterior segment plain cotton fabric is detachably connected with back segment plain cotton fabric；Leading portion plain cotton fabric is used to be detachably connected with aircraft leading portion, and middle leading portion plain cotton fabric is used to be detachably connected with leading portion in aircraft, and posterior segment plain cotton fabric is used to be used to be detachably connected with aircraft back segment with the washable connection in aircraft posterior segment, back segment plain cotton fabric.Each block of plain cotton fabric protects fuselage different parts, and whole machine is protected jointly, also easily wears off, is easy to storage.Aircraft protection device includes above-mentioned airplane complete machine plain cotton fabric, and also including inductor, controller and alarm, inductor is arranged at aircraft outside and is coupled with controller; alarm is coupled with controller; if position where the non-shade inductor of plain cotton fabric, alarm equipment alarm, ensure that airplane complete machine plain cotton fabric is installed in place.
Description
Technical field
The utility model is related to aviation machine to manufacture field, and in particular to a kind of airplane complete machine plain cotton fabric and aircraft protection dress
Put.
Background technology
Aircraft is outdoor when parking, particularly helicopter, is easily corroded by dust, night frost, thunderstorm, ice and snow etc..Therefore,
The protection of aircraft is particularly important.Existing aircraft protects plain cotton fabric, is primarily adapted for use in driving cabin, it is impossible to which aircraft is integrally protected
Shield；And even for the overall protection plain cotton fabric of aircraft, generally one entirety, thus more difficult wear off, it is more difficult to receive.
Utility model content
In view of this, the utility model provides a kind of airplane complete machine plain cotton fabric and Aircraft protection device, and aircraft is integrally carried out
Protect, and this airplane complete machine plain cotton fabric also easily wears off, and is easy to storage.
What embodiment of the present utility model was realized in：
A kind of first aspect, there is provided airplane complete machine plain cotton fabric, including leading portion plain cotton fabric, middle leading portion plain cotton fabric, posterior segment plain cotton fabric and
Back segment plain cotton fabric；Leading portion plain cotton fabric is detachably connected with middle leading portion plain cotton fabric, and middle leading portion plain cotton fabric is detachably connected with posterior segment plain cotton fabric, in after
Duan Mengbu is detachably connected with back segment plain cotton fabric；Leading portion plain cotton fabric be used for detachable shade outside aircraft cockpit, middle leading portion plain cotton fabric
For detachable shade in aircraft leading portion, posterior segment plain cotton fabric be used for detachable shade in aircraft posterior segment, back segment plain cotton fabric is used for
Detachable shade is in aircraft back segment.
In the utility model preferred embodiment, leading portion plain cotton fabric is including leading portion plain cotton fabric main body, for protecting plane nose
First overlap of head plain cotton fabric and middle leading portion plain cotton fabric overlap joint, the first fixture that leading portion plain cotton fabric main body is fixed on aircraft；
First overlap, head plain cotton fabric are connected with leading portion plain cotton fabric main body, and the first fixture is connected with leading portion plain cotton fabric main body.
In the utility model preferred embodiment, middle leading portion plain cotton fabric includes that middle leading portion plain cotton fabric main body and leading portion plain cotton fabric are overlapped
The second overlap and the second fixture that middle leading portion plain cotton fabric main body is fixed on aircraft；Second overlap is covered with middle leading portion
Cloth main body is connected, and the second fixture is connected with middle leading portion plain cotton fabric main body.
In the utility model preferred embodiment, posterior segment plain cotton fabric includes that posterior segment plain cotton fabric main body and middle leading portion plain cotton fabric are taken
The 3rd overlap for connecing and the 3rd fixture that posterior segment plain cotton fabric main body is fixed on aircraft；3rd overlap and posterior segment
Plain cotton fabric main body is connected, and the 3rd fixture is connected with posterior segment plain cotton fabric main body.
In the utility model preferred embodiment, back segment plain cotton fabric includes what back segment plain cotton fabric main body and posterior segment plain cotton fabric were overlapped
4th overlap and the 4th fixture that back segment plain cotton fabric main body is fixed on aircraft；4th overlap and back segment plain cotton fabric main body
Connection, the 4th fixture is connected with back segment plain cotton fabric main body.
In the utility model preferred embodiment, the first fixture, the second fixture, the 3rd fixture and the 4th fix
Part is frenulum or pull stap.
In the utility model preferred embodiment, the second overlap, the 3rd overlap, the 4th overlap edge are respectively provided with
There is rubber tube.
In the utility model preferred embodiment, leading portion plain cotton fabric main body, middle leading portion plain cotton fabric main body, posterior segment plain cotton fabric master are made
The cloth of body, back segment plain cotton fabric main body, head plain cotton fabric, the first overlap, the second overlap, the 3rd overlap and the 4th overlap
Be double-decker, including the outer layer cloth with water resistance and thermal property inner layer cloth.
In the utility model preferred embodiment, leading portion plain cotton fabric, middle leading portion plain cotton fabric, posterior segment plain cotton fabric and back segment plain cotton fabric are
Anti-fungus material is made.
A kind of second aspect, there is provided Aircraft protection device, including above-mentioned airplane complete machine plain cotton fabric, are also arranged at winged including multiple
Controller that inductor on the outside of machine is coupled with inductor and the alarm coupled with controller.
The beneficial effect of the utility model embodiment is：The utility model provides a kind of airplane complete machine plain cotton fabric and aircraft is protected
Protection unit.Airplane complete machine plain cotton fabric is divided into leading portion plain cotton fabric, middle leading portion plain cotton fabric, posterior segment plain cotton fabric and back segment plain cotton fabric, leading portion plain cotton fabric with
Middle leading portion plain cotton fabric is detachably connected, and middle leading portion plain cotton fabric is detachably connected with posterior segment plain cotton fabric, and posterior segment plain cotton fabric can with back segment plain cotton fabric
Dismounting connection；Leading portion plain cotton fabric is used to be detachably connected with aircraft leading portion, and middle leading portion plain cotton fabric is used to detachably connect with leading portion in aircraft
Connect, posterior segment plain cotton fabric is used to be used to be detachably connected with aircraft back segment with the washable connection in aircraft posterior segment, back segment plain cotton fabric.Use
Polylith plain cotton fabric, every block of plain cotton fabric is used to protect fuselage different parts, and whole machine can be protected jointly, and the airplane complete machine plain cotton fabric has
There is the advantage for easily wearing off, being easy to storage.Beyond Aircraft protection device is except above-mentioned airplane complete machine plain cotton fabric, also including inductor,
Controller, alarm, inductor are arranged at aircraft different parts, and inductor is coupled with controller, and alarm is coupled with controller,
When position where the incomplete shade inductor of plain cotton fabric, alarm reminds staff, ensures that airplane complete machine plain cotton fabric is installed in place.
Brief description of the drawings
In order to illustrate more clearly of the technical scheme of the utility model embodiment, below will be to be used needed for embodiment
Accompanying drawing be briefly described, it will be appreciated that the following drawings illustrate only some embodiments of the present utility model, therefore should not be by
Regard the restriction to scope as, for those of ordinary skill in the art, on the premise of not paying creative work, may be used also
Other related accompanying drawings are obtained with according to these accompanying drawings.
Fig. 1 is arranged at schematic diagram when on aircraft for airplane complete machine plain cotton fabric that the utility model first embodiment is provided；
The structural representation of the leading portion plain cotton fabric that Fig. 2 is provided for the utility model first embodiment；
The structural representation of the middle leading portion plain cotton fabric that Fig. 3 is provided for the utility model first embodiment；
The structural representation of the posterior segment plain cotton fabric that Fig. 4 is provided for the utility model first embodiment；
The structural representation of the back segment plain cotton fabric that Fig. 5 is provided for the utility model first embodiment；
The structured flowchart of the warning device that Fig. 6 is provided for the utility model second embodiment.
Icon：100- airplane complete machine plain cotton fabrics；110- leading portion plain cotton fabrics；Leading portion plain cotton fabric in 120-；130- posterior segments plain cotton fabric；140-
Back segment plain cotton fabric；112- leading portion plain cotton fabric main bodys；114- head plain cotton fabrics；The overlaps of 116- first；The fixtures of 118- first；121- sizes
Adjustment portion；Leading portion plain cotton fabric main body in 122-；The overlaps of 126- second；The fixtures of 128- second；132- posterior segments plain cotton fabric main body；
The overlaps of 136- the 3rd；The fixtures of 138- the 3rd；142- back segment plain cotton fabric main bodys；The overlaps of 146- the 4th；The fixtures of 148- the 4th；
210- warning devices；212- inductors；214- controllers；216- alarms.
Specific embodiment
It is new below in conjunction with this practicality to make the purpose, technical scheme and advantage of the utility model embodiment clearer
Accompanying drawing in type embodiment, is clearly and completely described, it is clear that retouched to the technical scheme in the utility model embodiment
The embodiment stated is a part of embodiment of the utility model, rather than whole embodiments.Generally described in accompanying drawing herein and
The component of the utility model embodiment for showing can be arranged and designed with a variety of configurations.
Therefore, the detailed description of embodiment of the present utility model below to providing in the accompanying drawings is not intended to limit requirement
The scope of the present utility model of protection, but it is merely representative of selected embodiment of the present utility model.Based in the utility model
Embodiment, the every other embodiment that those of ordinary skill in the art are obtained under the premise of creative work is not made, all
Belong to the scope of the utility model protection.
It should be noted that：Similar label and letter represents similar terms in following accompanying drawing, therefore, once a certain Xiang Yi
It is defined in individual accompanying drawing, then it need not be further defined and explained in subsequent accompanying drawing.
In description of the present utility model, it is necessary to explanation, term " on ", D score, "left", "right", " interior ", " outward ",
" orientation or position relationship of the instruction such as " center " be based on orientation shown in the drawings or position relationship, or the utility model produce
The orientation or position relationship usually put when product are used, are for only for ease of description the utility model and simplify description, rather than
Indicate or imply signified device or element and must have specific orientation, with specific azimuth configuration and operation, therefore can not
It is interpreted as to limitation of the present utility model.Additionally, term " first ", " second ", " the 3rd ", " the 4th " etc. are only used for differentiation and retouch
State, and it is not intended that indicating or implying relative importance.
Additionally, the term such as term " level ", " vertical " " hanging " is not offered as requiring part abswolute level or pendency, but
Can be slightly tilted.It is not the expression structure one if " level " refers to only its direction with respect to more level for " vertical "
It is calmly fully horizontal, and can be to be slightly tilted.
In description of the present utility model, in addition it is also necessary to explanation, unless otherwise clearly defined and limited, term " sets
Put ", " connected ", " connection " etc. should be interpreted broadly, for example, it may be fixedly connected, or be detachably connected, or one
Ground connection；Can mechanically connect, or electrically connect；Can be joined directly together, it is also possible to by the indirect phase of intermediary
Even, can be two connections of element internal.For the ordinary skill in the art, can understand above-mentioned with concrete condition
Concrete meaning of the term in the utility model.
First embodiment
Refer to Fig. 1.The present embodiment provides a kind of airplane complete machine plain cotton fabric 100, including leading portion plain cotton fabric 110, middle leading portion plain cotton fabric
120th, posterior segment plain cotton fabric 130 and back segment plain cotton fabric 140, leading portion plain cotton fabric 110 are detachably connected with middle leading portion plain cotton fabric 120, middle leading portion
Plain cotton fabric 120 is detachably connected with posterior segment plain cotton fabric 130, and posterior segment plain cotton fabric 130 is detachably connected with back segment plain cotton fabric 140.Leading portion is covered
Cloth 110 is used to protect aircraft leading portion, and, for protecting leading portion in aircraft, posterior segment plain cotton fabric 130 is for protecting winged for middle leading portion plain cotton fabric 120
Machine posterior segment, back segment plain cotton fabric 140 is used to protect aircraft back segment.
Because the making material of airplane complete machine plain cotton fabric 100 is cloth, simple structure chart not can be shown that airplane complete machine plain cotton fabric
100 form, therefore only give airplane complete machine plain cotton fabric 100 here and be arranged at schematic diagram when on aircraft.
Refer to Fig. 2.Leading portion plain cotton fabric 110 include leading portion plain cotton fabric main body 112, head plain cotton fabric 114, the first overlap 116 with
And first fixture 118；First overlap 116, head plain cotton fabric 114, the first fixture 118 are connected with leading portion plain cotton fabric main body 112.
Leading portion plain cotton fabric main body 112, head plain cotton fabric 114, the first overlap 116 and the first fixture 118 are entered separately below
Row explanation.
Leading portion plain cotton fabric main body 112 is used for shade aircraft leading portion, such as driving cabin position.
Head plain cotton fabric 114 is applied to shade plane nose position, is generally positioned at one end of leading portion plain cotton fabric main body 112, makes
Leading portion plain cotton fabric 110 can more comprehensively, snugly cover aircraft leading portion.
Because the airplane complete machine plain cotton fabric 100 that the utility model is provided is made up of four discrete plain cotton fabrics, between different plain cotton fabrics
Lap-joint may leak, thus in leading portion plain cotton fabric main body 112 head plain cotton fabric 114 offside, be provided with and middle leading portion cover
First overlap 116 of the overlap joint of cloth 120.
Leading portion plain cotton fabric 110 should wrap aircraft leading portion and fix, therefore is provided with aircraft leading portion plain cotton fabric main body 112
Multipair first fixture 118, the first fixture 118 can be frenulum or pull stap.
Leading portion plain cotton fabric main body 112, head plain cotton fabric 114, the first overlap 116 should have waterproof, insulation effect, thus use
Cloth with double-decker, inner layer cloth has heat-insulating property, and outer layer cloth has water resistance.Such as, outer layer is waterproof
Cloth, internal layer is panne velvet cloth.
To prevent leading portion plain cotton fabric 110 from going mouldy, make leading portion plain cotton fabric main body 112, head plain cotton fabric 114, the first overlap 116 with
And first the material of fixture 118 should be by mould proof treatment.Can using impregnating, pad, the method such as coating or spraying is by antibacterial
Agent is applied on cloth.
Refer to Fig. 3.Middle leading portion plain cotton fabric 120 includes that middle leading portion plain cotton fabric main body 122, the second overlap 126 and second are solid
Determine part 128；Second overlap 126, the second fixture 128 are connected with middle leading portion plain cotton fabric main body 122.
Middle leading portion plain cotton fabric main body 122, the second overlap 126 and the second fixture 128 are illustrated separately below.
Middle leading portion plain cotton fabric main body 122 is used for leading portion, such as a part for aircraft cabin in shade aircraft.
In order to prevent roof leaking, the second overlap overlapped with leading portion plain cotton fabric 110 is provided with middle leading portion plain cotton fabric main body 122
126。
In order that plain cotton fabric equably fitted with aircraft corresponding site, not pocket water, go for a drive, installation portion is close at plain cotton fabric edge
Position, is provided with rubber tube, to prevent heavy rain, heavy snow, dust storm and the intrusion of hail in the edge of the second overlap 126.Additionally, also
Can be using the method for plain cotton fabric liner aviation balloon adhesive plaster.
Middle leading portion plain cotton fabric 120 should wrap leading portion and fixation in aircraft, therefore in leading portion plain cotton fabric main body 122 in aircraft
Multipair second fixture 128 is provided with, the second fixture 128 can be frenulum or pull stap.
Middle leading portion plain cotton fabric main body 122, the second overlap 126 should have waterproof, insulation effect, thus be tied using with double-deck
The cloth of structure, inner layer cloth has heat-insulating property, and outer layer cloth has water resistance.Such as, outer layer is waterproof cloth, and internal layer is flat
Flannelette.
Due to there is certain radian to change at aircraft cabin to empennage, middle leading portion plain cotton fabric 120 is away from the second overlap 126
Side is provided with size adjusting portion 121.Size adjusting portion 121 is frenulum, pull stap, slide fastener, VELCRO etc., in adjustment
Leading portion plain cotton fabric 120 is near the edge of posterior segment plain cotton fabric 130 and the laminating degree of airframe.
To prevent leading portion plain cotton fabric 110 from going mouldy, leading portion plain cotton fabric main body 122, the second overlap 126 and second are fixed in making
The material of part 128 should be by mould proof treatment.Can using impregnating, pad, the method such as coating or spraying antiseptic is applied to cloth
On material.
Refer to Fig. 4.Posterior segment plain cotton fabric 130 includes that posterior segment plain cotton fabric main body 132, the 3rd overlap 136 and the 3rd are solid
Determine part 138；3rd overlap 136, the 3rd fixture 138 are connected with posterior segment plain cotton fabric main body 132.
Posterior segment plain cotton fabric main body 132, the 3rd overlap 136 and the 3rd fixture 138 are illustrated separately below.
Posterior segment plain cotton fabric main body 132 is for shade aircraft posterior segment, such as a part for aircraft cabin.
In order to prevent roof leaking, the 3rd overlap joint overlapped with middle leading portion plain cotton fabric 120 is provided with posterior segment plain cotton fabric main body 132
Area 136.
In order that plain cotton fabric equably fitted with aircraft corresponding site, not pocket water, go for a drive, installation portion is close at plain cotton fabric edge
Position, is provided with rubber tube, to prevent heavy rain, heavy snow, dust storm and the intrusion of hail in the edge of the 3rd overlap 136.Additionally, also
Can be using the method for plain cotton fabric liner aviation balloon adhesive plaster.
Posterior segment plain cotton fabric 130 should wrap aircraft posterior segment and fixed, therefore in aircraft posterior segment plain cotton fabric main body 132
Multipair 3rd fixture 138 is provided with, the 3rd fixture 138 can be frenulum or pull stap.
Posterior segment plain cotton fabric main body 132, the 3rd overlap 136 should have waterproof, an insulation effect, thus using having double-deck knot
The cloth of structure, inner layer cloth has heat-insulating property, and outer layer cloth has water resistance.Such as, outer layer is waterproof cloth, and internal layer is flat
Flannelette.
To prevent leading portion plain cotton fabric 110 from going mouldy, make posterior segment plain cotton fabric main body 132, the 3rd overlap 136 and the 3rd and fix
The material of part 138 should be by mould proof treatment.Can using impregnating, pad, the method such as coating or spraying antiseptic is applied to cloth
On material.
Refer to Fig. 5.Back segment plain cotton fabric 140 includes back segment plain cotton fabric main body 142, the 4th overlap 146 and the 4th fixture
148；4th overlap 146, the 4th fixture 148 are connected with back segment plain cotton fabric main body 142.
Back segment plain cotton fabric main body 142, the 4th overlap 146 and the 4th fixture 148 are illustrated separately below.
Back segment plain cotton fabric main body 142 is used for shade aircraft back segment, such as aircraft tail.
In order to prevent roof leaking, the 4th overlap overlapped with posterior segment plain cotton fabric 130 is provided with back segment plain cotton fabric main body 142
146。
In order that plain cotton fabric equably fitted with aircraft corresponding site, not pocket water, go for a drive, installation portion is close at plain cotton fabric edge
Position, is provided with rubber tube, to prevent heavy rain, heavy snow, dust storm and the intrusion of hail in the edge of the 4th overlap 146.Additionally, also
Can be using the method for plain cotton fabric liner aviation balloon adhesive plaster.
Back segment plain cotton fabric 140 should wrap aircraft back segment and fix, therefore is provided with aircraft back segment plain cotton fabric main body 142
Multipair 4th fixture 148, the 4th fixture 148 can be frenulum or pull stap.
Back segment plain cotton fabric main body 142, the 4th overlap 146 should have waterproof, insulation effect, thus using with double-decker
Cloth, inner layer cloth has heat-insulating property, and outer layer cloth has water resistance.Such as, outer layer is waterproof cloth, and internal layer is velveteen
Cloth.
To prevent leading portion plain cotton fabric 110 from going mouldy, back segment plain cotton fabric main body 142, the 4th overlap 146 and the 4th fixture are made
148 material should be by mould proof treatment.Can using impregnating, pad, the method such as coating or spraying antiseptic is applied to cloth
On.
Generally speaking, a kind of airplane complete machine plain cotton fabric 100, including leading portion plain cotton fabric 110, middle leading portion plain cotton fabric are present embodiments provided
120th, posterior segment plain cotton fabric 130 and back segment plain cotton fabric 140.Four blocks of plain cotton fabrics envelope aircraft jointly, when reduction aircraft is parked out of doors,
The influence of wind and rain, hail, frost and snow to aircraft.The setting of polylith plain cotton fabric, be difficult to wear off when effectively prevent plain cotton fabric for an entirety,
It is difficult to the problem of folding storage；Plain cotton fabric has insulation, water-proof function, meets use demand；Mould proof treatment is carried out, is prevented in tide
Plain cotton fabric goes mouldy under wet environment or other poor environments；Overlap is provided between plain cotton fabric, part overlap edge is provided with rubber
Sebific duct, effectively prevent the intrusion of heavy rain, heavy snow, dust storm and hail.
Second embodiment
Refer to Fig. 6.Aircraft protection device includes airplane complete machine plain cotton fabric 100 and warning device 210.Airplane complete machine plain cotton fabric
100 is identical with first embodiment, and warning device 210 includes inductor 212, controller 214 and alarm 216.
Inductor 212 is photo resistance, infrared sensor etc., at least two, it is arranged on airframe；Each inductor
212 couple with the input of controller 214 respectively, and controller 214 can be ARM chips, single-chip microcomputer etc.；Alarm 216 and control
The output end coupling of device 214, alarm 216 can be loudspeaker, buzzer etc..
When non-212 position of shade inductor of airplane complete machine plain cotton fabric 100, inductor 212 sends a signal to controller
214, after controller 214 is processed input signal, control alarm 216 is alarmed, and reminds staff's adjustment plain cotton fabric, so as to
Aircraft is preferably protected.
In sum, the utility model provides a kind of airplane complete machine plain cotton fabric 100 and Aircraft protection device, and airplane complete machine is covered
Cloth 100 include leading portion plain cotton fabric 110, middle leading portion plain cotton fabric 120, posterior segment plain cotton fabric 130 and back segment plain cotton fabric 140, leading portion plain cotton fabric 110 with
Middle leading portion plain cotton fabric 120 is detachably connected, and middle leading portion plain cotton fabric 120 is detachably connected with posterior segment plain cotton fabric 130, posterior segment plain cotton fabric 130
It is detachably connected with back segment plain cotton fabric 140；Outside aircraft cockpit, middle leading portion plain cotton fabric 120 can for the detachable shade of leading portion plain cotton fabric 110
Dismounting shade leading portion in aircraft, the detachable shade of posterior segment plain cotton fabric 130 detachably hides in aircraft posterior segment, back segment plain cotton fabric 140
Cover in aircraft back segment.Four blocks of plain cotton fabrics are protected to aircraft jointly, with being easy to wear off, the advantage of convenient for collecting.Aircraft is protected
Device includes foregoing airplane complete machine plain cotton fabric 100, also including inductor 212, controller 214 and alarm 216, when aircraft portion
Position not by complete shade, by warning reminding staff so that the complete shade aircraft of airplane complete machine plain cotton fabric 100, so as to aircraft
Protection it is more perfect.
Preferred embodiment of the present utility model is the foregoing is only, the utility model is not limited to, for this
For the technical staff in field, the utility model can have various modifications and variations.It is all it is of the present utility model spirit and principle
Within, any modification, equivalent substitution and improvements made etc. should be included within protection domain of the present utility model.
Claims (10)
1. a kind of airplane complete machine plain cotton fabric, it is characterised in that including leading portion plain cotton fabric, middle leading portion plain cotton fabric, posterior segment plain cotton fabric and back segment
Plain cotton fabric；The leading portion plain cotton fabric is detachably connected with the middle leading portion plain cotton fabric, and the middle leading portion plain cotton fabric can with the posterior segment plain cotton fabric
Dismounting connection, the posterior segment plain cotton fabric is detachably connected with the back segment plain cotton fabric；The leading portion plain cotton fabric be used for detachable shade in
Outside aircraft cockpit, the middle leading portion plain cotton fabric is used for detachable shade leading portion in aircraft, and the posterior segment plain cotton fabric is used for can
In aircraft posterior segment, the back segment plain cotton fabric is used for detachable shade in aircraft back segment to dismounting shade.
2. airplane complete machine plain cotton fabric according to claim 1, it is characterised in that the leading portion plain cotton fabric includes leading portion plain cotton fabric master
First overlap of body, the head plain cotton fabric for protecting plane nose and middle leading portion plain cotton fabric overlap joint, by the leading portion plain cotton fabric main body
The first fixture being fixed on aircraft；First overlap, the head plain cotton fabric are connected with the leading portion plain cotton fabric main body, institute
The first fixture is stated to be connected with the leading portion plain cotton fabric main body.
3. airplane complete machine plain cotton fabric according to claim 2, it is characterised in that the middle leading portion plain cotton fabric includes middle leading portion plain cotton fabric
Main body and leading portion plain cotton fabric overlap joint the second overlap and by the middle leading portion plain cotton fabric main body be fixed on aircraft second fixation
Part；Second overlap is connected with the middle leading portion plain cotton fabric main body, second fixture and the middle leading portion plain cotton fabric main body
Connection.
4. airplane complete machine plain cotton fabric according to claim 3, it is characterised in that the posterior segment plain cotton fabric includes posterior segment plain cotton fabric
3rd overlap of main body and middle leading portion plain cotton fabric overlap joint and the 3rd consolidate what the posterior segment plain cotton fabric main body was fixed on aircraft
Determine part；3rd overlap is connected with the posterior segment plain cotton fabric main body, the 3rd fixture and the posterior segment plain cotton fabric master
Body is connected.
5. airplane complete machine plain cotton fabric according to claim 4, it is characterised in that the back segment plain cotton fabric includes back segment plain cotton fabric master
Body and posterior segment plain cotton fabric the 4th overlap for overlapping and the 4th fixation that the back segment plain cotton fabric main body is fixed on aircraft
Part；4th overlap is connected with the back segment plain cotton fabric main body, and the 4th fixture is connected with the back segment plain cotton fabric main body.
6. airplane complete machine plain cotton fabric according to claim 5, it is characterised in that first fixture, described second are fixed
Part, the 3rd fixture and the 4th fixture are frenulum or pull stap.
7. airplane complete machine plain cotton fabric according to claim 5, it is characterised in that second overlap, the 3rd overlap joint
Area, the 4th overlap edge are provided with rubber tube.
8. airplane complete machine plain cotton fabric according to claim 5, it is characterised in that make the leading portion plain cotton fabric main body, it is described in
Leading portion plain cotton fabric main body, the posterior segment plain cotton fabric main body, the back segment plain cotton fabric main body, the head plain cotton fabric, first overlap,
The cloth of second overlap, the 3rd overlap and the 4th overlap is double-decker, including with waterproof
The outer layer cloth of performance and the inner layer cloth of thermal property.
9. airplane complete machine plain cotton fabric according to claim 1, it is characterised in that the leading portion plain cotton fabric, the middle leading portion plain cotton fabric,
The posterior segment plain cotton fabric and the back segment plain cotton fabric are made up of anti-fungus material.
10. a kind of Aircraft protection device, it is characterised in that covered including the airplane complete machine described in any one in claim 1-9
Cloth, be also arranged at including multiple controller that the inductor on the outside of aircraft couples with the inductor and with the controller
The alarm of coupling.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621341152.9U CN206243494U (en) | 2016-12-08 | 2016-12-08 | Airplane complete machine plain cotton fabric and Aircraft protection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621341152.9U CN206243494U (en) | 2016-12-08 | 2016-12-08 | Airplane complete machine plain cotton fabric and Aircraft protection device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206243494U true CN206243494U (en) | 2017-06-13 |
Family
ID=59005378
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621341152.9U Active CN206243494U (en) | 2016-12-08 | 2016-12-08 | Airplane complete machine plain cotton fabric and Aircraft protection device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206243494U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741990A (en) * | 2016-12-28 | 2017-05-31 | 玉环天润航空机械制造有限公司 | A kind of full machine sheet of helicopter and helicopter protection device |
| CN110104204A (en) * | 2019-05-23 | 2019-08-09 | 山东威西特斯航空科技有限公司 | A kind of installation method of airplane cloth |
| WO2021007761A1 (en) * | 2019-07-16 | 2021-01-21 | 田庆亮 | Method for mounting protective fabric cover at air inlet of aircraft engine |
-
2016
- 2016-12-08 CN CN201621341152.9U patent/CN206243494U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741990A (en) * | 2016-12-28 | 2017-05-31 | 玉环天润航空机械制造有限公司 | A kind of full machine sheet of helicopter and helicopter protection device |
| CN106741990B (en) * | 2016-12-28 | 2018-11-20 | 玉环天润航空机械制造有限公司 | A kind of full machine sheet of helicopter and helicopter protective device |
| CN110104204A (en) * | 2019-05-23 | 2019-08-09 | 山东威西特斯航空科技有限公司 | A kind of installation method of airplane cloth |
| WO2021007761A1 (en) * | 2019-07-16 | 2021-01-21 | 田庆亮 | Method for mounting protective fabric cover at air inlet of aircraft engine |
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