CN106741990A - A kind of full machine sheet of helicopter and helicopter protection device - Google Patents
A kind of full machine sheet of helicopter and helicopter protection device Download PDFInfo
- Publication number
- CN106741990A CN106741990A CN201611232863.7A CN201611232863A CN106741990A CN 106741990 A CN106741990 A CN 106741990A CN 201611232863 A CN201611232863 A CN 201611232863A CN 106741990 A CN106741990 A CN 106741990A
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- China
- Prior art keywords
- sheet
- main body
- fuselage
- helicopter
- fixture
- Prior art date
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- 239000004744 fabric Substances 0.000 claims description 58
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 19
- 230000000855 fungicidal effect Effects 0.000 claims description 16
- 206010049244 Ankyloglossia congenital Diseases 0.000 claims description 12
- 230000008901 benefit Effects 0.000 abstract description 6
- 238000005516 engineering process Methods 0.000 abstract description 4
- 230000002633 protecting effect Effects 0.000 abstract description 4
- 238000004519 manufacturing process Methods 0.000 abstract description 2
- 239000000463 material Substances 0.000 description 32
- 238000000034 method Methods 0.000 description 12
- 239000000428 dust Substances 0.000 description 10
- 239000011248 coating agent Substances 0.000 description 9
- 238000000576 coating method Methods 0.000 description 9
- 238000005507 spraying Methods 0.000 description 9
- 230000002421 anti-septic effect Effects 0.000 description 8
- 238000005253 cladding Methods 0.000 description 7
- 229920000742 Cotton Polymers 0.000 description 4
- 238000009434 installation Methods 0.000 description 4
- 238000012545 processing Methods 0.000 description 4
- 239000000853 adhesive Substances 0.000 description 3
- 230000001070 adhesive effect Effects 0.000 description 3
- 230000008878 coupling Effects 0.000 description 3
- 238000010168 coupling process Methods 0.000 description 3
- 238000005859 coupling reaction Methods 0.000 description 3
- -1 go for a drive Substances 0.000 description 3
- 239000011505 plaster Substances 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000010030 laminating Methods 0.000 description 2
- 238000003860 storage Methods 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 239000003242 anti bacterial agent Substances 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000004549 pulsed laser deposition Methods 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000004078 waterproofing Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Catching Or Destruction (AREA)
Abstract
The present invention relates to a kind of full machine sheet of helicopter and helicopter protection device, belong to aero-manufacturing technology field.The full machine sheet of the helicopter includes：Rotor sheet, weapon carrier sheet and fuselage sheet.The fuselage sheet includes：Leading portion sheet, fuselage posterior segment sheet and aft body sheet in nosing sheet, fuselage.Leading portion sheet, fuselage posterior segment sheet and the aft body sheet are detachably connected successively in the nosing sheet, the fuselage；The rotor sheet and the weapon carrier sheet are detachably connected with the fuselage sheet, the fuselage sheet is used for the fuselage of detachable shade helicopter, the weapon carrier sheet is used for the weapon carrier of helicopter described in detachable shade, and the rotor sheet is used for the rotor of helicopter described in detachable shade.For compared to existing protection sheet, possess the advantages of being easy to wear/take off, receive, helicopter can be given and more in place, more fully protected, protecting effect is greatly improved.
Description
Technical field
The invention belongs to aero-manufacturing technology field, and in particular to a kind of full machine sheet of helicopter and helicopter protection dress
Put.
Background technology
As industrial or agricultural and the development of science and technology, aircraft industry are in eruptive growth, the aircraft of various uses is directed to.By
In aircraft is outdoor park when, particularly helicopter is easily corroded by dust, night frost, thunderstorm, ice and snow etc..Therefore, helicopter
Protection it is particularly important.Existing helicopter protects plain cotton fabric, is primarily adapted for use in driving cabin, it is impossible to which helicopter is integrally protected
Shield；And even for the overall protection plain cotton fabric of helicopter, generally one entirety is being arranged or is dismantling the mistake of protection plain cotton fabric
Cheng Zhong, because helicopter head is larger, thus more difficult wear/takes off, it is more difficult to receive, secondly as the construction of helicopter is not advise
Then, it is thus impossible to give each part of helicopter protection next to the skin, cause protecting effect not good, or even some positions cannot obtain
To protection.
The content of the invention
In consideration of it, it is an object of the invention to provide a kind of full machine sheet of helicopter and helicopter protection device, with effective
Ground improves above mentioned problem.
What embodiments of the invention were realized in：
A kind of full machine sheet of helicopter is the embodiment of the invention provides, including：Rotor sheet, weapon carrier sheet and fuselage
Sheet.The fuselage sheet includes：Leading portion sheet, fuselage posterior segment sheet and aft body cloth in nosing sheet, fuselage
Cover.In the nosing sheet, the fuselage leading portion sheet, fuselage posterior segment sheet and the aft body sheet according to
It is secondary to be detachably connected；The rotor sheet and the weapon carrier sheet are detachably connected with the fuselage sheet, the machine
Body sheet is used for the fuselage of detachable shade helicopter, and the weapon carrier sheet is used for the force of helicopter described in detachable shade
Device hanger, the rotor sheet is used for the rotor of helicopter described in detachable shade.
In preferred embodiments of the present invention, the rotor sheet includes：Multiple rotor sheet main bodys, each described rotor
The first fixture for the rotor sheet main body to be fixed on the helicopter is provided with sheet main body.
In preferred embodiments of the present invention, the weapon carrier sheet includes：Multiple weapon carrier sheet main bodys, each
It is provided with the weapon carrier sheet main body for the weapon carrier sheet main body to be fixed on the helicopter
Second fixture.
In preferred embodiments of the present invention, the nosing sheet includes：See round the clock and retouch capstan head sheet, driving cabin cloth
Cover and head sheet, capstan head sheet is retouched in the sight round the clock to be included：See round the clock and retouch capstan head sheet main body and for being seen described round the clock
The 3rd fixture that capstan head sheet main body is fixed on fuselage is retouched, the 3rd fixture and described sight round the clock retouch capstan head sheet master
Body is connected；The head sheet includes：Head sheet main body and for head sheet main body to be fixed on head the 4th is consolidated
Determine part, the head sheet main body is connected with the 4th fixture；The driving cabin sheet includes：Driving cabin sheet main body,
With the first overlap of leading portion sheet overlap joint in the fuselage and for the driving cabin sheet main body to be fixed on fuselage
5th fixture, first overlap and the 5th fixture are connected with the driving cabin sheet main body.
In preferred embodiments of the present invention, leading portion sheet includes in the fuselage：Leading portion sheet main body and institute in fuselage
State the second overlap of nosing sheet overlap joint and leading portion sheet main body in the fuselage is fixed on the helicopter
The 6th fixture；Second overlap and the 6th fixture are connected with leading portion sheet main body in the fuselage.
In preferred embodiments of the present invention, fuselage posterior segment sheet includes：Fuselage posterior segment sheet main body and institute
State the 3rd overlap of leading portion sheet overlap joint in fuselage and the fuselage posterior segment sheet main body is fixed on the helicopter
On the 7th fixture；3rd overlap and the 7th fixture are connected with the fuselage posterior segment sheet main body.
In preferred embodiments of the present invention, the aft body sheet includes：Empennage sheet and tail sheet, the tail
Wing sheet includes：Multiple empennage sheet main bodys, are provided with for by the empennage sheet in each described empennage sheet main body
The 8th fixture that main body is fixed on empennage；The tail sheet includes：Tail sheet main body and fuselage posterior segment cloth
The 9th fixture for covering the 4th overlap of overlap joint and the tail sheet main body being fixed on the helicopter；Described 4th
Overlap and the 9th fixture are connected with the tail sheet main body.
In preferred embodiments of the present invention, first fixture, second fixture, the 3rd fixture,
4th fixture, the 5th fixture, the 6th fixture, the 7th fixture, the 8th fixture and
9th fixture is frenulum or pull stap, second overlap, the 3rd overlap, the 4th overlap
Edge is provided with rubber tube.
In preferred embodiments of the present invention, described sight round the clock retouches capstan head sheet main body, the driving cabin sheet main body, institute
State leading portion sheet main body, the posterior segment sheet main body, each described empennage sheet master in head sheet main body, the fuselage
Body, the tail sheet main body, each described rotor sheet main body, each described weapon carrier sheet main body are double-deck knot
Structure, including：Outer layer and the internal layer for possessing heat-insulating property and submissive performance with fungicidal properties and water resistance.
The embodiment of the present invention additionally provides a kind of helicopter protection device, including：Controller, alarm, switch, be arranged at
The full machine sheet of multiple sensors and above-mentioned helicopter on the outside of helicopter, the output end of each sensor with the control
The input coupling of device processed, the switch couples with the power end of the controller, the output end of the controller and the report
The input coupling of alert device.
The embodiment of the invention provides a kind of full machine sheet of helicopter and helicopter protection device.The full machine cloth of helicopter
Cover includes：Rotor sheet, weapon carrier sheet and fuselage sheet, the fuselage sheet include：Before in nosing sheet, fuselage
Section sheet, fuselage posterior segment sheet and aft body sheet.The sheet by the way of breaking the whole up into parts, using multistage sheet come right
Helicopter implements comprehensive protection, and every section of sheet is designed according to the specification of helicopter, and leaves only enough adjustment chis
It is very little, it is to avoid because of sheet deformation (for example, sheet shrink) etc., and be unable to reach the situation that protection requires and occur.Compared to existing
Protection plain cotton fabric for, on the one hand, because by the way of breaking the whole up into parts, so when using or dismantling sheet, very just
Victory, secondly, be also convenient for storage, greatly enhance the efficiency worn/take off, so as to reduce human and material resources, financial resources and when
Between, save cost；On the other hand, due to the sheet designed using the different parts for helicopter, can be to helicopter
Privileged site (for example, weapon carrier, rotor etc.) give and more in place, more fully protect, for using overall sheet, more
Laminating helicopter, protecting effect is greatly improved, and improves the maintenance efficiency of helicopter, further saves cost.
Other features and advantages of the present invention will illustrate in subsequent specification, also, partly become from specification
It is clear that or being understood by implementing the embodiment of the present invention.The purpose of the present invention and other advantages can be by being write
Specifically noted structure is realized and obtained in specification, claims and accompanying drawing.
Brief description of the drawings
In order to illustrate more clearly about the embodiment of the present invention or technical scheme of the prior art, below will be to institute in embodiment
The accompanying drawing for needing to use is briefly described, it should be apparent that, drawings in the following description are only some implementations of the invention
Example, for those of ordinary skill in the art, on the premise of not paying creative work, can also obtain according to these accompanying drawings
Obtain other accompanying drawings.By the way that shown in accompanying drawing, above and other purpose of the invention, feature and advantage will become apparent from.In whole
Identical reference indicates identical part in accompanying drawing.Deliberately accompanying drawing, emphasis are not drawn by actual size equal proportion scaling
It is that purport of the invention is shown.
Fig. 1 shows that a kind of full machine sheet of helicopter provided in an embodiment of the present invention is arranged at signal when on helicopter
Figure.
Fig. 2 shows the structural representation of the rotor sheet main body in rotor sheet provided in an embodiment of the present invention.
Fig. 3 shows the structural representation of the weapon on-hook sheet main body in weapon carrier sheet provided in an embodiment of the present invention
Figure.
Fig. 4 shows the first visual angle of the tower sheet of scanning round the clock in nosing sheet provided in an embodiment of the present invention
Structural representation.
Fig. 5 shows the second visual angle of the tower sheet of scanning round the clock in nosing sheet provided in an embodiment of the present invention
Structural representation.
Fig. 6 shows driving cabin sheet and head the sheet connection in nosing sheet provided in an embodiment of the present invention
Structural representation.
Fig. 7 shows the structural representation of leading portion sheet in fuselage provided in an embodiment of the present invention.
Fig. 8 shows the structural representation of fuselage posterior segment provided in an embodiment of the present invention sheet.
Fig. 9 shows the structural representation of the empennage sheet main body in aft body sheet provided in an embodiment of the present invention.
Figure 10 shows the structural representation of the tail sheet in aft body sheet provided in an embodiment of the present invention.
Figure 11 shows the structured flowchart of the warning device in a kind of helicopter protection device provided in an embodiment of the present invention.
Icon：The full machine sheet of 10- helicopters；11- rotor sheets；111- rotor sheet main bodys；112- first is fixed
Part；13- weapon carrier sheets；131- weapon carrier sheet main bodys；The fixtures of 132- second；21- nosing sheets；
210- sees retouch capstan head sheet round the clock；211- sees retouch capstan head sheet main body round the clock；The fixtures of 212- the 3rd；213- head ends
Cover；214- head sheet main bodys；The fixtures of 215- the 4th；216- driving cabin sheets；217- driving cabin sheet main bodys；
The overlaps of 218- first；The fixtures of 219- the 5th；Leading portion sheet in 23- fuselages；Leading portion sheet main body in 231- fuselages；
The overlaps of 232- second；The fixtures of 233- the 6th；234- size adjustings portion；25- fuselages posterior segment sheet；251- fuselages
Posterior segment sheet main body；The overlaps of 252- the 3rd；The fixtures of 253- the 7th；27- aft body sheets；271- empennage cloth
Cover；272- empennage sheet main bodys；The fixtures of 273- the 8th；274- tail sheets；275- tail sheet main bodys；276-
Four overlaps；The fixtures of 277- the 9th；30- warning devices；40- sensors；41- controllers；43- alarms；45- is opened
Close.
Specific embodiment
To make the purpose, technical scheme and advantage of the embodiment of the present invention clearer, below in conjunction with the embodiment of the present invention
In accompanying drawing, the technical scheme in the embodiment of the present invention is clearly and completely described, it is clear that described embodiment is
A part of embodiment of the present invention, rather than whole embodiments.Present invention implementation generally described and illustrated in accompanying drawing herein
The component of example can be arranged and designed with a variety of configurations.
Therefore, the detailed description of embodiments of the invention below to providing in the accompanying drawings is not intended to limit claimed
The scope of the present invention, but be merely representative of selected embodiment of the invention.Based on the embodiment in the present invention, this area is common
The every other embodiment that technical staff is obtained under the premise of creative work is not made, belongs to the model of present invention protection
Enclose.
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 the description of the invention, it is necessary to explanation, term " on ", D score, "left", "right", " interior ", " outward " etc. indicate
Orientation or position relationship be that, based on orientation shown in the drawings or position relationship, or the invention product is usually put when using
Orientation or position relationship, be for only for ease of the description present invention and simplify and describe, rather than indicating or imply signified device
Or element with specific orientation, with specific azimuth configuration and operation, therefore must be not considered as limiting the invention.
Additionally, term " first ", " second ", " the 3rd " etc. are only used for distinguishing description, and it is not intended that indicating or implying relatively important
Property.
In the description of the invention, in addition it is also necessary to explanation, unless otherwise clearly defined and limited, term " setting ",
" installation ", " connected ", " connection ", " coupling " should be interpreted broadly, for example, it may be being fixedly connected, or detachably connecting
Connect, or be integrally connected；Can mechanically connect, or electrically connect；Can be joined directly together, it is also possible to by middle matchmaker
Jie is indirectly connected to, and can be two connections of element internal.For the ordinary skill in the art, can be with concrete condition
Understand above-mentioned term concrete meaning in the present invention.
A kind of full machine sheet 10 of helicopter is the embodiment of the invention provides, as shown in Figure 1.The full machine sheet 10 of the helicopter is wrapped
Include：Rotor sheet 11, weapon carrier sheet 13 and fuselage sheet.Because the making material of the full machine sheet 10 of helicopter is cloth,
Simple structure chart not can be shown that the form of the full machine sheet 10 of helicopter, therefore this give 10 sets of the full machine sheet of helicopter
Schematic diagram when on helicopter.
The rotor sheet 11 is used for the rotor of detachable shade helicopter.Due to the quantity of the rotor of different helicopters
The rotor quantity of difference, such as light helicopter can be 2, and the rotor quantity of Medium Helicopter can be 4 or 5, weight
The rotor quantity of type helicopter can be 6 or 8.In the present embodiment, as shown in Figure 2, it is preferable that the rotor sheet 11
Including：Multiple rotor sheet main bodys 111, each rotor sheet main body 111 is used for a piece of rotor of detachable shade helicopter.
In order to ensure intrusion of the lifting airscrew from heavy rain, heavy snow, dust storm and hail, the rotor sheet main body 111
Certain quality requirement should be met, such as at aspects such as water resistance, fungicidal properties, heat-insulating properties.In the present embodiment, preferably
Ground, the rotor sheet main body 111 uses the cloth of double-decker, including：Outer layer material with fungicidal properties and water resistance
Expect and possess the inner layer material of heat-insulating property and submissive performance, for example, outer layer is waterproof cloth, internal layer is panne velvet cloth.
Wherein, as shown in Fig. 2 being provided with each rotor sheet main body 111 for by the rotor sheet main body 111
The first fixture 112 being fixed on helicopter.In the present embodiment, it is preferable that first fixture 112 can be frenulum
Or pull stap.Preferably, the quantity of first fixture 112 is multiple, and multiple first fixtures 112 are arranged at intervals at often
In individual rotor sheet main body 111.
Wherein, to prevent rotor sheet 11 from going mouldy, the material for making rotor sheet main body 111 and the first fixture 112 can
With by mould proof treatment.For example, can using impregnating, pad, be applied to antiseptic on cloth by the method such as coating or spraying.
It should be understood that the rotor sheet 11 can also be an entirety, for the entirety rotation of detachable shade helicopter
The wing.Therefore the rotor sheet 11 for being shown in the present embodiment includes the rotation of multiple a piece of rotors for detachable shade helicopter
The structure of wing sheet main body 111 shall not be construed as limitation of the present invention.
The weapon carrier sheet 13 is used for the weapon carrier of detachable shade helicopter.Due to the force of different helicopters
Device hanger quantity is different, and the quantity of the weapon carrier of such as some helicopters can be 2 (each one of left and right), some helicopters
Weapon carrier quantity can be 4 (each two of left and right), some helicopters are even without weapon carrier etc..In the present embodiment
In, as shown in Figure 3, it is preferable that the weapon carrier sheet 13 includes：Multiple weapon carrier sheet main bodys 131, each weapon is hung
Frame sheet main body 131 is used for a weapon carrier of detachable shade helicopter.
In order to ensure intrusion of the helicopter weapon carrier from heavy rain, heavy snow, dust storm and hail, the weapon carrier sheet
Main body 131 should meet certain quality requirement, such as at aspects such as water resistance, fungicidal properties, heat-insulating properties.In the present embodiment
In, it is preferable that the weapon carrier sheet main body 131 uses the cloth of double-decker, including：With fungicidal properties and water proofing property
The cladding material of energy and the inner layer material for possessing heat-insulating property and submissive performance, for example, outer layer is waterproof cloth, internal layer is velveteen
Cloth.
Wherein, as shown in figure 3, being provided with each weapon carrier sheet main body 131 for by the weapon carrier cloth
The second fixture 132 that cover main body 131 is fixed on helicopter.In the present embodiment, it is preferable that second fixture 132
Can be frenulum or pull stap.Preferably, the quantity of second fixture 132 is between multiple, multiple second fixtures 132
Every being arranged in each weapon carrier sheet main body 131.
Wherein, to prevent weapon carrier sheet 13 from going mouldy, weapon carrier sheet main body 131 and the second fixture 132 are made
Material can be by mould proof treatment.For example, can using impregnating, pad, the method such as coating or spraying antiseptic is applied to cloth
On material.
The fuselage sheet is used for the fuselage of detachable shade helicopter.In the present embodiment, it is preferable that the fuselage cloth
Cover includes：Leading portion sheet 23, fuselage posterior segment sheet 25 and aft body sheet 27 in nosing sheet 21, fuselage.Wherein,
Leading portion sheet 23, fuselage posterior segment sheet 25 and the aft body cloth in the nosing sheet 21, the fuselage
Cover 27 is detachably connected successively.
The nosing sheet 21 is used for the positions such as the leading portion of detachable shade fuselage, such as driving cabin and head.It is excellent
Selection of land, the nosing sheet 21 includes：See round the clock and retouch capstan head sheet 210, driving cabin sheet 216 and head sheet 213.
The sight round the clock is retouched capstan head sheet 210 and retouches capstan head for the sight round the clock of detachable shade helicopter.In the present embodiment
In, refer to Fig. 4 and Fig. 5, it is preferable that capstan head sheet 210 is retouched in the sight round the clock to be included：Described sight round the clock retouches capstan head sheet main body
211 and for described sight round the clock to be retouched into the 3rd fixture 212 that capstan head sheet main body 211 is fixed on fuselage, the described 3rd consolidates
Determine part 212 and the sight round the clock is retouched capstan head sheet main body 211 and connected.
It is described to see round the clock in order to ensure that seeing round the clock for helicopter retouches intrusion of the capstan head from heavy rain, heavy snow, dust storm and hail
Retouching capstan head sheet main body 211 should meet certain quality requirement, such as at aspects such as water resistance, fungicidal properties, heat-insulating properties.
In the present embodiment, it is preferable that described sight round the clock retouches the cloth that capstan head sheet main body 211 uses double-decker, including：With anti-
The cladding material of mouldiness energy and water resistance and the inner layer material for possessing heat-insulating property and submissive performance, for example, outer layer is waterproof
Cloth, internal layer is panne velvet cloth.
Wherein, see to retouch round the clock and multiple 3rd fixtures 212 are provided with capstan head sheet main body 211.It is excellent in the present embodiment
Selection of land, the 3rd fixture 212 can be frenulum or pull stap.Preferably, multiple 3rd fixtures 212 are arranged at intervals at
See round the clock and retouch in capstan head sheet main body 211.
Wherein, retouch capstan head sheet 210 and go mouldy to prevent from seeing round the clock, make to see round the clock and retouch capstan head sheet main body 211 and the 3rd
The material of fixture 212 can be by mould proof treatment.For example, can using impregnating, pad, the method such as coating or spraying is by antiseptic
It is applied on cloth.
Wherein, due to seeing the leading portion for retouching capstan head in helicopter round the clock, using round the clock see retouch capstan head sheet 210 when should be under
Up it is inserted in, until all be inserted in it turret part by root, then is tightened with the 3rd fixture 212.Capstan head is retouched because seeing round the clock
Transparent place is provided with, the internal layer velveteen cloth can be not frayed with protection equipment.
The head sheet 213 is used for the head of detachable shade helicopter.In the present embodiment, as shown in fig. 6, it is preferred that
Ground head sheet 213 includes：Head sheet main body 214 and for head sheet main body 214 to be fixed on head the 4th is consolidated
Determine part 215, the head sheet main body 214 is connected with the 4th fixture 215.
In order to ensure the intrusion of the head from heavy rain, heavy snow, dust storm and hail of helicopter, the head sheet main body
214 and certain quality requirement should be met, such as at aspects such as water resistance, fungicidal properties, heat-insulating properties.In the present embodiment
In, it is preferable that the head sheet main body 214 uses the cloth of double-decker, including：With fungicidal properties and water resistance
Cladding material and the inner layer material for possessing heat-insulating property and submissive performance, for example, outer layer is waterproof cloth, internal layer is panne velvet cloth.
Wherein, multiple 4th fixtures 215 are provided with head sheet main body 214.In the present embodiment, it is preferable that institute
It can be frenulum or pull stap to state the 4th fixture 215.Preferably, multiple 4th fixtures 215 are arranged at intervals at head end
In cover main body 214.
Wherein, to prevent head sheet 213 from going mouldy, the material for making head sheet main body 214 and the 4th fixture 215 can
With by mould proof treatment.For example, can using impregnating, pad, be applied to antiseptic on cloth by the method such as coating or spraying.
The driving cabin sheet 216 is used for the driving cabin of detachable shade helicopter.In the present embodiment, as shown in fig. 6,
Preferably, the driving cabin sheet 216 includes：Driving cabin sheet main body 217, in the fuselage leading portion sheet 23 overlap joint
First overlap 218 and the 5th fixture 219 for the driving cabin sheet main body 217 to be fixed on fuselage.Wherein, institute
The first overlap 218 and the 5th fixture 219 is stated to be connected with the driving cabin sheet main body 217.
In the present embodiment, it is preferable that the driving cabin sheet main body 217 and the first overlap 218 are tied using double-deck
The cloth of structure, including：Cladding material and the internal layer for possessing heat-insulating property and submissive performance with fungicidal properties and water resistance
Material, for example, outer layer is waterproof cloth, internal layer is panne velvet cloth.
Wherein, multiple 5th fixtures 219 are provided with driving cabin sheet main body 217.In the present embodiment, it is preferable that
5th fixture 219 can be frenulum or pull stap.Preferably, multiple 5th fixtures 219 are arranged at intervals at driving
In cabin sheet main body 217.
Wherein, because fuselage sheet is made up of multiple separate sheets, the lap-joint between different sheets may leak,
The first overlap 218 for being overlapped with leading portion sheet 23 in the fuselage is thus provided with driving cabin sheet main body 217.
Wherein, to prevent driving cabin sheet 216 from going mouldy, driving cabin sheet main body 217, the first overlap 218 and the are made
The material of five fixtures 219 can be by mould proof treatment.For example, can using impregnating, pad, the method such as coating or spraying is by antibacterial
Agent is applied on cloth.
Leading portion sheet 23 is used for the middle leading portion of detachable shade fuselage in the fuselage.In the present embodiment, such as Fig. 7 institutes
Show, it is preferable that leading portion sheet 23 includes in the fuselage：Leading portion sheet main body 231 and the nosing sheet 21 in fuselage
Second overlap 232 of overlap joint and the 6th fixture that leading portion sheet main body 231 in the fuselage is fixed on helicopter
233, second overlap 232 and the 6th fixture 233 are connected with leading portion sheet main body 231 in the fuselage.
In the present embodiment, it is preferable that leading portion sheet main body 231 and the second overlap 232 are using double in the fuselage
The cloth of Rotating fields, including：Cladding material with fungicidal properties and water resistance and possess heat-insulating property and submissive performance
Inner layer material, for example, outer layer is waterproof cloth, internal layer is panne velvet cloth.
Wherein, multiple 6th fixtures 233 are provided with fuselage in leading portion sheet main body 231.In the present embodiment, preferably
Ground, the 6th fixture 233 can be frenulum or pull stap.Preferably, multiple 6th fixtures 233 are arranged at intervals at machine
In body in leading portion sheet main body 231.
Wherein, because fuselage sheet is made up of multiple separate sheets, the lap-joint between different sheets may leak,
The second overlap for being overlapped with the nosing sheet 21 is thus provided with leading portion sheet main body 231 in fuselage
232。
Wherein, in order that sheet equably fitted with helicopter corresponding site, not pocket water, go for a drive, cloth shroud rim need tightly
Patch installation position, is provided with rubber tube, to prevent invading for heavy rain, heavy snow, dust storm and hail in the edge of the second overlap 232
Enter.Additionally, can also be using the method for sheet liner aviation balloon adhesive plaster.
Due to there is certain radian to change at helicopter cabin to empennage, leading portion sheet 23 is away from the second overlap in fuselage
232 side is provided with size adjusting portion 234.Size adjusting portion 234 is frenulum, pull stap, slide fastener, VELCRO etc., for adjusting
Leading portion sheet 23 is near the edge of fuselage posterior segment sheet 25 and the laminating degree of helicopter fuselage in whole fuselage.
Wherein, in preventing fuselage leading portion sheet 23 go mouldy, make fuselage in leading portion sheet main body 231, the second overlap
232 and the 6th the material of fixture 233 can be by mould proof treatment.For example, can using impregnate, pad, coating or spraying etc. just
Be applied to antiseptic on cloth by method.
Fuselage posterior segment sheet 25 is used for the posterior segment of detachable shade fuselage.In the present embodiment, such as Fig. 8 institutes
Show, it is preferable that fuselage posterior segment sheet 25 includes：Leading portion sheet in fuselage posterior segment sheet main body 251 and the fuselage
3rd overlap 252 of 23 overlap joints and the 7th fixation that the fuselage posterior segment sheet main body 251 is fixed on helicopter
Part 253.Wherein, the 3rd overlap 252 and the 7th fixture 253 with the fuselage posterior segment sheet main body 251
Connection.
In the present embodiment, it is preferable that the fuselage posterior segment sheet main body 251 and the 3rd overlap 252 are using double
The cloth of Rotating fields, including：Cladding material with fungicidal properties and water resistance and possess heat-insulating property and submissive performance
Inner layer material, for example, outer layer is waterproof cloth, internal layer is panne velvet cloth.
Wherein, multiple 7th fixtures 253 are provided with fuselage posterior segment sheet main body 251.In the present embodiment, preferably
Ground, the 7th fixture 253 can be frenulum or pull stap.Preferably, multiple 7th fixtures 253 are arranged at intervals at machine
In body posterior segment sheet main body 251.
Wherein, because fuselage sheet is made up of multiple separate sheets, the lap-joint between different sheets may leak,
The 3rd overlap for being overlapped with leading portion sheet 23 in the fuselage is thus provided with fuselage posterior segment sheet main body 251
252。
Wherein, in order that sheet equably fitted with helicopter corresponding site, not pocket water, go for a drive, cloth shroud rim need tightly
Patch installation position, is provided with rubber tube, to prevent invading for heavy rain, heavy snow, dust storm and hail in the edge of the 3rd overlap 252
Enter.Additionally, can also be using the method for sheet liner aviation balloon adhesive plaster.
Wherein, to prevent fuselage posterior segment sheet 25 from going mouldy, fuselage posterior segment sheet main body 251, the 3rd overlap are made
252 and the 7th the material of fixture 253 can be by mould proof treatment.For example, can using impregnate, pad, coating or spraying etc. just
Be applied to antiseptic on cloth by method.
The aft body sheet 27 is used for the positions such as the back segment of detachable shade fuselage, such as empennage and tail.It is preferred that
Ground, the aft body sheet 27 includes：Empennage sheet 271 and tail sheet 274.
The empennage sheet 271 is used for the empennage of detachable shade helicopter.In the present embodiment, it is preferable that the tail
Wing sheet 271 includes：Multiple empennage sheet main bodys 272, each empennage sheet main body 272 is used for the one of detachable shade helicopter
Individual empennage.
In order to ensure intrusion of the empennage of helicopter from heavy rain, heavy snow, dust storm and hail, the empennage sheet main body 272
Certain quality requirement should be met, such as at aspects such as water resistance, fungicidal properties, heat-insulating properties.In the present embodiment, preferably
Ground, the empennage sheet main body 272 uses the cloth of double-decker, including：Outer layer material with fungicidal properties and water resistance
Expect and possess the inner layer material of heat-insulating property and submissive performance, for example, outer layer is waterproof cloth, internal layer is panne velvet cloth.
Wherein, as shown in figure 9, being provided with each empennage sheet main body 272 for by the empennage sheet main body 272
The 8th fixture 273 being fixed on helicopter.In the present embodiment, it is preferable that the 8th fixture 273 can be frenulum
Or pull stap.Preferably, the quantity of the 8th fixture 273 is multiple, and multiple 8th fixtures 273 are arranged at intervals at often
In individual empennage sheet main body 272.
Wherein, to prevent empennage sheet 271 from going mouldy, the material for making empennage sheet main body 272 and the 8th fixture 273 can
With by mould proof treatment.For example, can using impregnating, pad, be applied to antiseptic on cloth by the method such as coating or spraying.
The tail sheet 274 is used for the tail of detachable shade helicopter.Preferably, as shown in Figure 10, the tail
Sheet 274 includes：The 4th overlap 276 and incite somebody to action described that tail sheet main body 275 and fuselage posterior segment sheet 25 are overlapped
The 9th fixture 277 that tail sheet main body 275 is fixed on helicopter.Wherein, the 4th overlap 276 and the described 9th
Fixture 277 is connected with the tail sheet main body 275.
In the present embodiment, it is preferable that the tail sheet main body 275 and the 4th overlap 276 use double-decker
Cloth, including：Cladding material and the internal layer material for possessing heat-insulating property and submissive performance with fungicidal properties and water resistance
Material, for example, outer layer is waterproof cloth, internal layer is panne velvet cloth.
Wherein, multiple 9th fixtures 277 are provided with tail sheet main body 275.In the present embodiment, it is preferable that institute
It can be frenulum or pull stap to state the 9th fixture 277.Preferably, multiple 9th fixtures 277 are arranged at intervals at tail cloth
In cover main body 275.
Wherein, because fuselage sheet is made up of multiple separate sheets, the lap-joint between different sheets may leak,
The 4th overlap 276 for being overlapped with fuselage posterior segment sheet 25 is thus provided with tail sheet main body 275.
Wherein, in order that sheet equably fitted with helicopter corresponding site, not pocket water, go for a drive, cloth shroud rim need tightly
Patch installation position, is provided with rubber tube, to prevent invading for heavy rain, heavy snow, dust storm and hail in the edge of the 4th overlap 276
Enter.Additionally, can also be using the method for sheet liner aviation balloon adhesive plaster.
Wherein, to prevent tail sheet 274 from going mouldy, tail sheet main body 275, the 4th overlap 276 and the 9th are made solid
The material for determining part 277 can be by mould proof treatment.For example, can using impregnating, pad, the method such as coating or spraying applies antiseptic
It is added on cloth.
The embodiment of the present invention additionally provides a kind of helicopter protection device, including：Warning device 30 and above-mentioned helicopter
Full machine sheet 10, as shown in figure 11.Wherein, the structured flowchart of warning device 30 is illustrate only in Figure 11.
The warning device 30 includes：Controller 41, alarm 43, switch 45 and the multiple sensings being arranged on the outside of helicopter
Device 40.
When the complete not complete shade helicopter of machine sheet 10 of helicopter, exposed sensor 40 will send a signal to
The controller 41.Further, the output end of the sensor 40 is coupled with the input of the controller 41.In this implementation
In example, the sensor 40 can be light sensor, for example, it may be photo resistance, infrared sensor etc..
The controller 41 is used to receive the signal of the transmission of the sensor 40, and the signal is processed, and identifies
Just control alarm 43 to be alarmed after the signal, staff's adjustment full machine sheet 10 of helicopter is reminded, so as to helicopter
Preferably protected.
Wherein, the controller 41 can be a kind of IC chip, the disposal ability with signal.Above-mentioned control
Device 41 can be general processor, including central processing unit (Central Processing Unit, CPU), network processing unit
(Network Processor, NP) etc.；Can also be digital signal processor (Digital Signal Processing,
DSP), application specific integrated circuit (Application Specific Integrated Circuit, ASIC), ready-made programmable gate
Array (Field Programmable Gate Array, FPGA) or other PLDs, discrete gate or crystal
Pipe logical device, discrete hardware components.General processor can be microprocessor or the processor can also be any routine
Processor etc..
The input of the alarm 43 is coupled with the output end of the controller 41.The alarm 43 is used in failure work
Alarm is sent under condition, staff's adjustment full machine sheet 10 of helicopter is reminded, preferably to be protected to helicopter.
Further, when the controller 41 identifies the signal that sensor 40 sends, alarm 43 is just controlled to send alarm, should
The mode of prompting can be combination of auditory tone cues, or signal lamp flash for prompting, or both etc..In the present embodiment
In, the alarm 43 can be audible-visual annunciator, or buzzer, can also be warning lamp, or by buzzer and
Warning device of warning lamp composition etc..It is not further qualified herein.
The switch 45 is used to control the on/off electricity of controller 41.Further, one end of the switch 45 connects with power supply
Connect, the other end of the switch 45 is connected with the power end of controller 41.Preferably, when switch 45 close when, controller 41 with
Conducting between power supply, controller 41 can be with normal work, when 45 disconnection is switched, and the electricity between controller 41 and power supply breaks
Open, controller 41 can not work.
When the full machine sheet 10 of shade helicopter is not needed, controller 41 can be controlled to work by switch 45,
In case alarm 43 is constantly in alarm condition.
In sum, a kind of full machine sheet of helicopter and helicopter protection device be the embodiment of the invention provides.It is described straight
Rising the full machine sheet of machine includes：Rotor sheet, weapon carrier sheet and fuselage sheet, the fuselage sheet include：Nosing cloth
Leading portion sheet, fuselage posterior segment sheet and aft body sheet in cover, fuselage.On the one hand, the full machine sheet useization of the helicopter
Whole is zero mode, can be fitted with helicopter even closer when in use, is preferably protected to helicopter, reduces helicopter and exists
When open air is parked, the influence of wind and rain, hail, frost and snow to helicopter.On the other hand, the setting of polylith sheet, effectively prevent cloth
The problem for being difficult to wear off, be difficult to folding storage during for an entirety is covered, the efficiency worn/take off is greatly enhanced, so as to subtract
Lack human and material resources, financial resources and time, save cost.Meanwhile, rotor sheet, weapon carrier sheet, nosing sheet,
Leading portion sheet, fuselage posterior segment sheet and aft body sheet are using the outer layer with fungicidal properties and water resistance in fuselage
Preferably protected to helicopter with the double-decker of the internal layer for possessing heat-insulating property and submissive performance, prevent in wet environment or
Sheet goes mouldy under other poor environments.Overlap is provided between sheet, part overlap edge is provided with rubber tube, has
Effect prevents the intrusion of heavy rain, heavy snow, dust storm and hail.The full machine sheet of the helicopter possesses that simple structure, protecting effect are good, makes
With it is convenient, with low cost the advantages of, it is easy to utilize.
The preferred embodiments of the present invention are the foregoing is only, is not intended to limit the invention, for the skill of this area
For art personnel, the present invention can have various modifications and variations.It is all within the spirit and principles in the present invention, made any repair
Change, equivalent, improvement etc., should be included within the scope of the present invention.
Claims (10)
1. the full machine sheet of a kind of helicopter, it is characterised in that including：Rotor sheet, weapon carrier sheet and fuselage sheet, it is described
Fuselage sheet includes：Leading portion sheet, fuselage posterior segment sheet and aft body sheet, the machine in nosing sheet, fuselage
Leading portion sheet, fuselage posterior segment sheet and the aft body sheet are detachable successively in body leading portion sheet, the fuselage
Connection；The rotor sheet and the weapon carrier sheet are detachably connected with the fuselage sheet, and the fuselage sheet is used
In the fuselage of detachable shade helicopter, the weapon carrier sheet is used for the weapon carrier of helicopter described in detachable shade,
The rotor sheet is used for the rotor of helicopter described in detachable shade.
2. the full machine sheet of helicopter according to claim 1, it is characterised in that the rotor sheet includes：Multiple rotors
Sheet main body, is provided with each described rotor sheet main body for the rotor sheet main body to be fixed on into the helicopter
On the first fixture.
3. the full machine sheet of helicopter according to claim 2, it is characterised in that the weapon carrier sheet includes：It is multiple
Weapon carrier sheet main body, is provided with for by the weapon carrier sheet main body in each described weapon carrier sheet main body
The second fixture being fixed on the helicopter.
4. the full machine sheet of helicopter according to claim 3, it is characterised in that the nosing sheet includes：Round the clock
Capstan head sheet, driving cabin sheet and head sheet are retouched in sight, and capstan head sheet is retouched in the sight round the clock to be included：See round the clock and retouch capstan head sheet master
Body and for by it is described round the clock see retouch the 3rd fixture that capstan head sheet main body is fixed on fuselage, the 3rd fixture and institute
To state see round the clock and retouch the connection of capstan head sheet main body；The head sheet includes：Head sheet main body and for by head sheet main body
The 4th fixture being fixed on head, the head sheet main body is connected with the 4th fixture；The driving cabin sheet
Including：First overlap of leading portion sheet overlap joint and for by the driving cabin cloth in driving cabin sheet main body and the fuselage
The 5th fixture that cover main body is fixed on fuselage, first overlap and the 5th fixture with the driving cabin cloth
Cover main body is connected.
5. the full machine sheet of helicopter according to claim 4, it is characterised in that leading portion sheet includes in the fuselage：Machine
Second overlap of leading portion sheet main body and nosing sheet overlap joint and by leading portion sheet master in the fuselage in body
The 6th fixture that body is fixed on the helicopter；Second overlap and the 6th fixture with the fuselage in
Leading portion sheet main body is connected.
6. the full machine sheet of helicopter according to claim 5, it is characterised in that fuselage posterior segment sheet includes：Machine
3rd overlap of leading portion sheet overlap joint and by fuselage posterior segment sheet in body posterior segment sheet main body and the fuselage
The 7th fixture that main body is fixed on the helicopter；3rd overlap and the 7th fixture with the fuselage
Posterior segment sheet main body connection.
7. the full machine sheet of helicopter according to claim 6, it is characterised in that the aft body sheet includes：Empennage
Sheet and tail sheet, the empennage sheet include：Multiple empennage sheet main bodys, are respectively provided with each described empennage sheet main body
There is the 8th fixture for the empennage sheet main body to be fixed on empennage；The tail sheet includes：Tail sheet master
The 4th overlap and the tail sheet main body is fixed on the helicopter that body and fuselage posterior segment sheet are overlapped
The 9th fixture；4th overlap and the 9th fixture are connected with the tail sheet main body.
8. the full machine sheet of helicopter according to claim 7, it is characterised in that first fixture, described second are consolidated
Determine part, the 3rd fixture, the 4th fixture, the 5th fixture, the 6th fixture, the 7th fixation
Part, the 8th fixture and the 9th fixture are frenulum or pull stap, and second overlap, the described 3rd take
Connect area, the 4th overlap edge and be provided with rubber tube.
9. the full machine sheet of helicopter according to claim 7, it is characterised in that it is described see round the clock retouch capstan head sheet main body,
Leading portion sheet main body, the posterior segment sheet master in the driving cabin sheet main body, the head sheet main body, the fuselage
Body, each described empennage sheet main body, the tail sheet main body, each described rotor sheet main body, each described weapon are hung
Frame sheet main body is double-decker, including：Outer layer with fungicidal properties and water resistance and possesses heat-insulating property and submissive
The internal layer of performance.
10. a kind of helicopter protection device, it is characterised in that including：Controller, alarm, switch, be arranged at helicopter outside
Multiple sensors and the full machine sheet of the helicopter as described in claim 1-9 any one, the output of each sensor
Hold input with the controller to couple, the switch is coupled with the power end of the controller, the controller it is defeated
Go out end to be coupled with the input of the alarm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611232863.7A CN106741990B (en) | 2016-12-28 | 2016-12-28 | A kind of full machine sheet of helicopter and helicopter protective device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611232863.7A CN106741990B (en) | 2016-12-28 | 2016-12-28 | A kind of full machine sheet of helicopter and helicopter protective device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106741990A true CN106741990A (en) | 2017-05-31 |
| CN106741990B CN106741990B (en) | 2018-11-20 |
Family
ID=58921423
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611232863.7A Active CN106741990B (en) | 2016-12-28 | 2016-12-28 | A kind of full machine sheet of helicopter and helicopter protective device |
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| Country | Link |
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| CN (1) | CN106741990B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107972880A (en) * | 2017-12-05 | 2018-05-01 | 长沙展朔轩兴信息科技有限公司 | Multi-rotor unmanned aerial vehicle protective device |
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| CN203032940U (en) * | 2012-11-24 | 2013-07-03 | 陈博 | Agricultural unmanned helicopter protective sleeve |
| CN104443418A (en) * | 2014-10-16 | 2015-03-25 | 李浩昌 | Cover or bag preventing wet fog rusting and corrosion of civil aviation berthed aircrafts or high-quality precision equipment |
| EP2868571A1 (en) * | 2013-11-05 | 2015-05-06 | Airbus Helicopters | Fuselage structure of a helicopter with a load carrying median floor interposed between a passenger area and an equipment area |
| CN206243494U (en) * | 2016-12-08 | 2017-06-13 | 玉环天润航空机械制造有限公司 | Airplane complete machine plain cotton fabric and Aircraft protection device |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201721616U (en) * | 2010-01-07 | 2011-01-26 | 哈尔滨飞机工业集团有限责任公司 | Helicopter cable-proof protector |
| CN203032940U (en) * | 2012-11-24 | 2013-07-03 | 陈博 | Agricultural unmanned helicopter protective sleeve |
| EP2868571A1 (en) * | 2013-11-05 | 2015-05-06 | Airbus Helicopters | Fuselage structure of a helicopter with a load carrying median floor interposed between a passenger area and an equipment area |
| CN104443418A (en) * | 2014-10-16 | 2015-03-25 | 李浩昌 | Cover or bag preventing wet fog rusting and corrosion of civil aviation berthed aircrafts or high-quality precision equipment |
| CN206243494U (en) * | 2016-12-08 | 2017-06-13 | 玉环天润航空机械制造有限公司 | Airplane complete machine plain cotton fabric and Aircraft protection device |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN107972880A (en) * | 2017-12-05 | 2018-05-01 | 长沙展朔轩兴信息科技有限公司 | Multi-rotor unmanned aerial vehicle protective device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106741990B (en) | 2018-11-20 |
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