CN106741990B - A kind of full machine sheet of helicopter and helicopter protective device - Google Patents
A kind of full machine sheet of helicopter and helicopter protective device Download PDFInfo
- Publication number
- CN106741990B CN106741990B CN201611232863.7A CN201611232863A CN106741990B CN 106741990 B CN106741990 B CN 106741990B CN 201611232863 A CN201611232863 A CN 201611232863A CN 106741990 B CN106741990 B CN 106741990B
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- Prior art keywords
- sheet
- main body
- cover main
- fuselage
- helicopter
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- 230000001681 protective effect Effects 0.000 title claims abstract description 10
- 239000004744 fabric Substances 0.000 claims description 183
- 230000000855 fungicidal effect Effects 0.000 claims description 16
- 206010049244 Ankyloglossia congenital Diseases 0.000 claims description 12
- 238000009413 insulation Methods 0.000 claims description 12
- 230000008901 benefit Effects 0.000 abstract description 6
- 238000004519 manufacturing process Methods 0.000 abstract description 5
- 238000005516 engineering process Methods 0.000 abstract description 4
- 230000002633 protecting effect Effects 0.000 abstract description 4
- 239000000463 material Substances 0.000 description 30
- 238000000034 method Methods 0.000 description 13
- 238000010586 diagram Methods 0.000 description 11
- 239000000428 dust Substances 0.000 description 10
- 239000003242 anti bacterial agent Substances 0.000 description 9
- 239000011248 coating agent Substances 0.000 description 9
- 238000000576 coating method Methods 0.000 description 9
- 238000007598 dipping method Methods 0.000 description 9
- 238000005507 spraying Methods 0.000 description 9
- 238000005253 cladding Methods 0.000 description 7
- 229920000742 Cotton Polymers 0.000 description 4
- 238000009434 installation Methods 0.000 description 4
- 239000000853 adhesive Substances 0.000 description 3
- 230000001070 adhesive effect Effects 0.000 description 3
- -1 go for a drive Substances 0.000 description 3
- 239000011505 plaster Substances 0.000 description 3
- 230000000007 visual effect Effects 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 230000008878 coupling Effects 0.000 description 2
- 238000010168 coupling process Methods 0.000 description 2
- 238000005859 coupling reaction Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 239000013500 performance material Substances 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 238000003860 storage 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 protective devices, 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 successively detachably connected 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 mask helicopter, weapon carrier of the weapon carrier sheet for helicopter described in detachable mask, rotor of the rotor sheet for helicopter described in detachable mask.For existing protection sheet, has convenient for the advantages that wearing/take off, storing, helicopter can be given and more in place, more fully protected, protecting effect greatly improves.
Description
Technical field
The invention belongs to aero-manufacturing technology fields, and in particular to a kind of full machine sheet of helicopter and helicopter protection dress
It sets.
Background technique
With the development of industrial or agricultural and science and technology, aircraft industry is in eruptive growth, is directed to aircraft for various purposes.By
In aircraft is outdoor park when, especially helicopter is easy the erosion 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 cockpit, cannot integrally protect to helicopter
Shield；And even for the protection plain cotton fabric of helicopter entirety, generally an entirety, in the mistake for being arranged or dismantling protection plain cotton fabric
Cheng Zhong since helicopter head is larger, thus more difficult wear/takes off, it is more difficult to store, secondly as the construction of helicopter is not advise
Then, it is thus impossible to give each component of helicopter personal protection, cause protecting effect bad or even certain positions can not obtain
To protection.
Summary of the invention
In consideration of it, the purpose of the present invention is to provide a kind of full machine sheet of helicopter and helicopter protective devices, with effective
Ground improves the above problem.
What the embodiment of the present invention was realized in：
The embodiment of the invention provides a kind of full machine sheets of helicopter, 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 mask helicopter, force of the weapon carrier sheet for helicopter described in detachable mask
Device hanger, rotor of the rotor sheet for helicopter described in detachable mask.
In preferred embodiments of the present invention, the rotor sheet includes：Multiple rotor cloth cover main bodies, each rotor
The first fixing piece for being fixed on the rotor cloth cover main body on the helicopter is provided in cloth cover main body.
In preferred embodiments of the present invention, the weapon carrier sheet includes：Multiple weapon carrier cloth cover main bodies, each
It is provided in the weapon carrier cloth cover main body for the weapon carrier cloth cover main body to be fixed on the helicopter
Second fixing piece.
In preferred embodiments of the present invention, the nosing sheet includes：It sees round the clock and retouches capstan head sheet, cockpit cloth
Cover and head sheet, the sight round the clock retouch capstan head sheet and include：It sees round the clock and retouches capstan head cloth cover main body and for seeing described round the clock
The third fixing piece that capstan head cloth cover main body is fixed on fuselage is retouched, the third fixing piece and described see round the clock retouch capstan head sheet master
Body connection；The head sheet includes：Head end cover main body and the 4th consolidating for head end cover main body to be fixed on head
Determine part, the head end cover main body is connect with the 4th fixing piece；The cockpit sheet includes：Cockpit cloth cover main body,
With overlapped the first overlap of leading portion sheet in the fuselage and for the cockpit cloth cover main body to be fixed on fuselage
5th fixing piece, first overlap and the 5th fixing piece are connect with the cockpit cloth cover main body.
In preferred embodiments of the present invention, leading portion sheet includes in the fuselage：Leading portion cloth cover main body and institute in fuselage
It states nosing sheet overlapped the second overlap and leading portion cloth cover main body in the fuselage is fixed on the helicopter
The 6th fixing piece；Second overlap and the 6th fixing piece are connect with leading portion cloth cover main body in the fuselage.
In preferred embodiments of the present invention, fuselage posterior segment sheet includes：Fuselage posterior segment cloth cover main body and institute
It states leading portion sheet in fuselage overlapped third overlap and the fuselage posterior segment cloth cover main body is fixed on the helicopter
On the 7th fixing piece；The third overlap and the 7th fixing piece are connect with the fuselage posterior segment cloth cover 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 cloth cover main bodies are provided in each empennage cloth cover main body for by the empennage sheet
Main body is fixed on the 8th fixing piece on empennage；The tail sheet includes：Tail cloth cover main body and fuselage posterior segment cloth
Cover overlapped the 4th overlap and the 9th fixing piece being fixed on the tail cloth cover main body on the helicopter；Described 4th
Overlap and the 9th fixing piece are connect with the tail cloth cover main body.
In preferred embodiments of the present invention, first fixing piece, second fixing piece, the third fixing piece,
4th fixing piece, the 5th fixing piece, the 6th fixing piece, the 7th fixing piece, the 8th fixing piece and
9th fixing piece is frenulum or pull stap, second overlap, the third overlap, the 4th overlap
Edge is provided with rubber tube.
In preferred embodiments of the present invention, described see round the clock retouches capstan head cloth cover main body, the cockpit cloth cover main body, institute
State head end cover main body, leading portion cloth cover main body, the posterior segment cloth cover main body, each empennage sheet master in the fuselage
Body, the tail cloth cover main body, each rotor cloth cover main body, each weapon carrier cloth cover main body are the double-deck knot
Structure, including：Outer layer with fungicidal properties and waterproof performance and the internal layer for having thermal insulation property and submissive performance.
The embodiment of the invention also provides a kind of helicopter protective devices, including：Controller alarm, is switched, is set to
Multiple sensors and the above-mentioned full machine sheet of helicopter on the outside of helicopter, the output end of each sensor with the control
The input terminal of device processed couples, and the switch is coupled with the power end of the controller, the output end of the controller and the report
The input terminal coupling of alert device.
The embodiment of the invention provides a kind of full machine sheet of helicopter and helicopter protective devices.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 pair
Helicopter implements comprehensive protection, and every section of sheet is designed according to the specification of helicopter, and there are only enough adjustment rulers
It is very little, it avoids because of sheet deformation (for example, sheet shrink) etc., and it is unable to reach the case where protection requires.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 greatly enhances the efficiency worn/taken off secondly, being also convenient for storing, thus reduce human and material resources, financial resources and when
Between, save cost；It on the other hand, can be to helicopter due to the sheet designed using the different parts for helicopter
Privileged site (for example, weapon carrier, rotor etc.) give and more in place, more fully protect, for using whole sheet, more
It is bonded helicopter, protecting effect greatly improves, improves the maintenance efficiency of helicopter, further save cost.
Other features and advantages of the present invention will be illustrated in subsequent specification, also, partly be become from specification
It is clear that being understood by implementing the embodiment of the present invention.The objectives and other advantages of the invention can be by written
Specifically noted structure is achieved and obtained in specification, claims and attached drawing.
Detailed description of the invention
It in order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, below will be to institute in embodiment
Attached drawing to be used is needed to be briefly described, it should be apparent that, the accompanying drawings in the following description is only some implementations of the invention
Example, for those of ordinary skill in the art, without creative efforts, can also obtain according to these attached drawings
Obtain other attached drawings.By the way that shown in attached drawing, above and other purpose of the invention, feature and advantage will be more clear.In whole
Identical appended drawing reference indicates identical part in attached drawing.Attached drawing, emphasis deliberately are not drawn by actual size equal proportion scaling
It is to show the gist of the present invention.
Fig. 1 shows signal when a kind of full machine sheet of helicopter provided in an embodiment of the present invention is set on helicopter
Figure.
Fig. 2 shows the structural schematic diagrams of the rotor cloth cover main body in rotor sheet provided in an embodiment of the present invention.
Fig. 3 shows the structural representation of the weapon on-hook cloth cover main body in weapon carrier sheet provided in an embodiment of the present invention
Figure.
Fig. 4 shows the first visual angle for scanning tower sheet round the clock in nosing sheet provided in an embodiment of the present invention
Structural schematic diagram.
Fig. 5 shows the second visual angle for scanning tower sheet round the clock in nosing sheet provided in an embodiment of the present invention
Structural schematic diagram.
Fig. 6 shows what the cockpit sheet in nosing sheet provided in an embodiment of the present invention was connected with head sheet
Structural schematic diagram.
Fig. 7 shows the structural schematic diagram of leading portion sheet in fuselage provided in an embodiment of the present invention.
Fig. 8 shows the structural schematic diagram of fuselage posterior segment provided in an embodiment of the present invention sheet.
Fig. 9 shows the structural schematic diagram of the empennage cloth cover main body in aft body sheet provided in an embodiment of the present invention.
Figure 10 shows the structural schematic diagram of the tail sheet in aft body sheet provided in an embodiment of the present invention.
Figure 11 shows the structural block diagram of the warning device in a kind of helicopter protective device provided in an embodiment of the present invention.
Icon：The full machine sheet of 10- helicopter；11- rotor sheet；111- rotor cloth cover main body；112- first is fixed
Part；13- weapon carrier sheet；131- weapon carrier cloth cover main body；The second fixing piece of 132-；21- nosing sheet；
210- sees retouch capstan head sheet round the clock；211- is seen round the clock retouches capstan head cloth cover main body；212- third fixing piece；213- head end
Cover；214- head end cover main body；The 4th fixing piece of 215-；216- cockpit sheet；217- cockpit cloth cover main body；
The first overlap of 218-；The 5th fixing piece of 219-；Leading portion sheet in 23- fuselage；Leading portion cloth cover main body in 231- fuselage；
The second overlap of 232-；The 6th fixing piece of 233-；234- size adjusting portion；25- fuselage posterior segment sheet；251- fuselage
Posterior segment cloth cover main body；252- third overlap；The 7th fixing piece of 253-；27- aft body sheet；271- empennage cloth
Cover；272- empennage cloth cover main body；The 8th fixing piece of 273-；274- tail sheet；275- tail cloth cover main body；276-
Four overlaps；The 9th fixing piece of 277-；30- warning device；40- sensor；41- controller；43- alarm；45- is opened
It closes.
Specific embodiment
In order to make the object, technical scheme and advantages of the embodiment of the invention clearer, below in conjunction with the embodiment of the present invention
In attached drawing, technical scheme in the embodiment of the invention is clearly and completely described, it is clear that described embodiment is
A part of the embodiment of the present invention, instead of all the embodiments.The present invention being usually described and illustrated herein in the accompanying drawings is implemented
The component of example can be arranged and be designed with a variety of different configurations.
Therefore, the detailed description of the embodiment of the present invention provided in the accompanying drawings is not intended to limit below claimed
The scope of the present invention, but be merely representative of selected embodiment of the invention.Based on the embodiments of the present invention, this field is common
Technical staff's every other embodiment obtained without creative efforts belongs to the model that the present invention protects
It encloses.
It should be noted that：Similar label and letter indicate similar terms in following attached drawing, therefore, once a certain Xiang Yi
It is defined in a attached drawing, does not then need that it is further defined and explained in subsequent attached drawing.
In the description of the present invention, it should be noted that the instruction such as term " on ", "lower", "left", "right", "inner", "outside"
Orientation or positional relationship be based on the orientation or positional relationship shown in the drawings or the invention product using when usually put
Orientation or positional relationship, be merely for convenience of description of the present invention and simplification of the description, rather than the device of indication or suggestion meaning
Or element must have a particular orientation, be constructed and operated in a specific orientation, therefore be not considered as limiting the invention.
In addition, term " first ", " second ", " third " etc. are only used for distinguishing description, it is not understood to indicate or imply relatively important
Property.
In the description of the present invention, it is also necessary to which explanation is unless specifically defined or limited otherwise, term " setting ",
" installation ", " connected ", " connection ", " coupling " shall be understood in a broad sense, for example, it may be being fixedly connected, be also possible to detachably connect
It connects, or is integrally connected；It can be mechanical connection, be also possible to be electrically connected；It can be directly connected, intermediate matchmaker can also be passed through
Jie is indirectly connected, and can be the connection inside two elements.It for the ordinary skill in the art, can be with concrete condition
Understand the concrete meaning of above-mentioned term in the present invention.
The embodiment of the invention provides a kind of full machine sheets 10 of helicopter, as shown in Figure 1.The full machine sheet 10 of the helicopter wraps
It includes：Rotor sheet 11, weapon carrier sheet 13 and fuselage sheet.Since 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 be given here by 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 mask helicopter.Due to the quantity of the rotor of different helicopters
Difference, such as the rotor quantity of light helicopter can be 2, the rotor quantity of Medium Helicopter can be 4 or 5, weight
The rotor quantity of type helicopter can be 6 or 8.In this present embodiment, as shown in Figure 2, it is preferable that the rotor sheet 11
Including：Multiple rotor cloth cover main bodies 111, each rotor cloth cover main body 111 are used for a piece of rotor of detachable mask helicopter.
In order to guarantee lifting airscrew from the intrusion of heavy rain, heavy snow, dust storm and hail, the rotor cloth cover main body 111
Should meet certain quality requirement, for example, waterproof performance, fungicidal properties, in terms of.In this present embodiment, preferably
Ground, the rotor cloth cover main body 111 use the cloth of double-layer structure, including：Outer layer material with fungicidal properties and waterproof performance
Expect and have the inner layer material of thermal insulation 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 in each rotor cloth cover main body 111 for by the rotor cloth cover main body 111
The first fixing piece 112 being fixed on helicopter.In this present embodiment, it is preferable that first fixing piece 112 can be frenulum
Or pull stap.Preferably, the quantity of first fixing piece 112 is multiple, and multiple first fixing pieces 112 are arranged at intervals at often
In a rotor cloth cover main body 111.
Wherein, to prevent rotor sheet 11 from going mouldy, the material for making rotor cloth cover main body 111 and the first fixing piece 112 can
To pass through mould proof processing.For example, can be used dipping, pad, antibacterial agent is applied on cloth by the methods of coating or spraying.
It should be understood that the rotor sheet 11 is also possible to an entirety, the entirety rotation for detachable mask helicopter
The wing.Therefore the rotor sheet 11 shown in the present embodiment includes the rotation of multiple a piece of rotors for detachable mask helicopter
The structure of wing cloth cover 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 mask helicopter.Due to the force of different helicopters
Device hanger quantity is different, such as the quantity of weapon carrier of certain helicopters can be 2 (each one of left and right), certain helicopters
Weapon carrier quantity can be 4 (each two of left and right), certain 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 cloth cover main bodies 131, each weapon are hung
Frame cloth cover main body 131 is used for a weapon carrier of detachable mask helicopter.
In order to guarantee helicopter weapon carrier from the intrusion of heavy rain, heavy snow, dust storm and hail, the weapon carrier sheet
Main body 131 should meet certain quality requirement, for example, waterproof performance, fungicidal properties, in terms of.In the present embodiment
In, it is preferable that the weapon carrier cloth cover main body 131 uses the cloth of double-layer structure, including：With fungicidal properties and waterproofness
The cladding material of energy and the inner layer material for having thermal insulation property and submissive performance, for example, outer layer is waterproof cloth, internal layer is velveteen
Cloth.
Wherein, as shown in figure 3, being provided in each weapon carrier cloth cover main body 131 for by the weapon carrier cloth
Cover main body 131 is fixed on the second fixing piece 132 on helicopter.In this present embodiment, it is preferable that second fixing piece 132
It can be frenulum or pull stap.Preferably, the quantity of second fixing piece 132 is multiple, between multiple second fixing pieces 132
Every being set in each weapon carrier cloth cover main body 131.
Wherein, to prevent weapon carrier sheet 13 from going mouldy, weapon carrier cloth cover main body 131 and the second fixing piece 132 are made
Material can pass through mould proof processing.For example, can be used dipping, pad, antibacterial agent is applied to cloth by the methods of coating or spraying
On material.
The fuselage sheet is used for the fuselage of detachable mask helicopter.In this 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 successively detachably connected.
The nosing sheet 21 is used for the leading portion of detachable mask fuselage, such as the positions such as cockpit and head.It is excellent
Selection of land, the nosing sheet 21 include：It sees round the clock and retouches capstan head sheet 210, cockpit sheet 216 and head sheet 213.
The sight round the clock retouches round the clock sight of the capstan head sheet 210 for detachable mask helicopter and retouches capstan head.In the present embodiment
In, please refer to Fig. 4 and Fig. 5, it is preferable that the sight round the clock retouches capstan head sheet 210 and includes：Described see round the clock retouches capstan head cloth cover main body
211 and for described see round the clock to be retouched the third fixing piece 212 that capstan head cloth cover main body 211 is fixed on fuselage, the third is solid
Determine part 212 and described see round the clock retouches the connection of capstan head cloth cover main body 211.
It is described to see round the clock in order to guarantee that seeing round the clock for helicopter retouches capstan head from the intrusion of heavy rain, heavy snow, dust storm and hail
Certain quality requirement should be met by retouching capstan head cloth cover main body 211, for example, waterproof performance, fungicidal properties, in terms of.
In this present embodiment, it is preferable that described see round the clock retouches the cloth that capstan head cloth cover main body 211 uses double-layer structure, including：With anti-
Mouldiness energy and the cladding material of waterproof performance and the inner layer material for having thermal insulation property and submissive performance, for example, outer layer is waterproof
Cloth, internal layer are panne velvet cloth.
Wherein, it sees to retouch round the clock and is provided with multiple third fixing pieces 212 in capstan head cloth cover main body 211.In this present embodiment, excellent
Selection of land, the third fixing piece 212 can be frenulum or pull stap.Preferably, multiple third fixing pieces 212 are arranged at intervals at
It sees and is retouched in capstan head cloth cover main body 211 round the clock.
Wherein, the mildew of capstan head sheet 210 is retouched to prevent from seeing round the clock, production is seen retouch capstan head cloth cover main body 211 and third round the clock
The material of fixing piece 212 can pass through mould proof processing.For example, can be used dipping, pad, the methods of coating or spraying are by antibacterial agent
It is applied on cloth.
Wherein, capstan head is retouched in the leading portion of helicopter due to seeing round the clock, it should be under when using seeing retouch capstan head sheet 210 round the clock
It is up inserted in, until turret part is all inserted in it by root, then is tightened with third fixing piece 212.Capstan head is retouched because seeing round the clock
It is equipped with transparent place, which can also protect equipment not frayed.
The head sheet 213 is used for the head of detachable mask helicopter.In this present embodiment, as shown in fig. 6, it is preferred that
Ground head sheet 213 includes：Head end cover main body 214 and the 4th consolidating for head end cover main body 214 to be fixed on head
Determine part 215, the head end cover main body 214 is connect with the 4th fixing piece 215.
In order to guarantee intrusion of the head from heavy rain, heavy snow, dust storm and hail of helicopter, the head end cover main body
214 and should meet certain quality requirement, for example, waterproof performance, fungicidal properties, in terms of.In the present embodiment
In, it is preferable that the head end cover main body 214 uses the cloth of double-layer structure, including：With fungicidal properties and waterproof performance
Cladding material and the inner layer material for having thermal insulation property and submissive performance, for example, outer layer is waterproof cloth, internal layer is panne velvet cloth.
Wherein, multiple 4th fixing pieces 215 are provided in head end cover main body 214.In this present embodiment, it is preferable that institute
Stating the 4th fixing piece 215 can be frenulum or pull stap.Preferably, multiple 4th fixing pieces 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 fixing piece 215 can
To pass through mould proof processing.For example, can be used dipping, pad, antibacterial agent is applied on cloth by the methods of coating or spraying.
The cockpit sheet 216 is used for the cockpit of detachable mask helicopter.In this present embodiment, as shown in fig. 6,
Preferably, the cockpit sheet 216 includes：Cockpit cloth cover main body 217, for leading portion sheet 23 in the fuselage, overlapped
First overlap 218 and for the cockpit cloth cover main body 217 to be fixed on the 5th fixing piece 219 on fuselage.Wherein, institute
It states the first overlap 218 and the 5th fixing piece 219 is connect with the cockpit cloth cover main body 217.
In this present embodiment, it is preferable that the cockpit cloth cover main body 217 and the first overlap 218 are all made of the double-deck knot
The cloth of structure, including：Cladding material with fungicidal properties and waterproof performance and the internal layer for having thermal insulation property and submissive performance
Material, for example, outer layer is waterproof cloth, internal layer is panne velvet cloth.
Wherein, multiple 5th fixing pieces 219 are provided in cockpit cloth cover main body 217.In this present embodiment, it is preferable that
5th fixing piece 219 can be frenulum or pull stap.Preferably, multiple 5th fixing pieces 219 are arranged at intervals at driving
In cabin cloth cover main body 217.
Wherein, it being made of due to fuselage sheet multiple isolated sheets, the lap-joint between different sheets may leak,
Thus be provided in cockpit cloth cover main body 217 for overlapped the first overlap 218 of leading portion sheet 23 in the fuselage.
Wherein, to prevent cockpit sheet 216 from going mouldy, production cockpit cloth cover main body 217, the first overlap 218 and the
The material of five fixing pieces 219 can pass through mould proof processing.For example, can be used dipping, pad, the methods of coating or spraying are by antibacterial
Agent is applied on cloth.
Leading portion sheet 23 is used for the middle leading portion of detachable mask fuselage in the fuselage.In this present embodiment, such as Fig. 7 institute
Show, it is preferable that leading portion sheet 23 includes in the fuselage：Leading portion cloth cover main body 231 and the nosing sheet 21 in fuselage
Overlapped the second overlap 232 and leading portion cloth cover main body 231 in the fuselage is fixed on the 6th fixing piece on helicopter
233, second overlap 232 and the 6th fixing piece 233 are connect with leading portion cloth cover main body 231 in the fuselage.
In this present embodiment, it is preferable that leading portion cloth cover main body 231 and the second overlap 232 are all made of double in the fuselage
The cloth of layer structure, including：Cladding material with fungicidal properties and waterproof performance and have thermal insulation property and submissive performance
Inner layer material, for example, outer layer is waterproof cloth, internal layer is panne velvet cloth.
Wherein, multiple 6th fixing pieces 233 are provided in fuselage in leading portion cloth cover main body 231.In this present embodiment, preferably
Ground, the 6th fixing piece 233 can be frenulum or pull stap.Preferably, multiple 6th fixing pieces 233 are arranged at intervals at machine
In body in leading portion cloth cover main body 231.
Wherein, it being made of due to fuselage sheet multiple isolated sheets, the lap-joint between different sheets may leak,
Thus be provided in leading portion cloth cover main body 231 in fuselage for the nosing sheet 21 overlapped the second overlap
232。
Wherein, in order to enable sheet is equably bonded with helicopter corresponding site, not pocket water, go for a drive, cloth shroud rim needs tight
Installation position is pasted, 232 edge of the second overlap is provided with rubber tube, to prevent invading for heavy rain, heavy snow, dust storm and hail
Enter.In addition, the method that sheet liner aviation balloon adhesive plaster also can be used.
Since helicopter cabin has certain radian variation at empennage, leading portion sheet 23 is far from the second overlap in fuselage
232 side is provided with size adjusting portion 234.Size adjusting portion 234 is frenulum, pull stap, zipper, velcro etc., for adjusting
Leading portion sheet 23 is close to the edge of fuselage posterior segment sheet 25 and the laminating degree of helicopter fuselage in complete machine body.
Wherein, to prevent leading portion sheet 23 in fuselage from going mouldy, leading portion cloth cover main body 231, the second overlap in fuselage are made
232 and the 6th the material of fixing piece 233 can pass through mould proof processing.For example, dipping can be used, pad, the side such as coating or spraying
Antibacterial agent is applied on cloth by method.
Fuselage posterior segment sheet 25 is used for the posterior segment of detachable mask fuselage.In this present embodiment, such as Fig. 8 institute
Show, it is preferable that fuselage posterior segment sheet 25 includes：Leading portion sheet in fuselage posterior segment cloth cover main body 251 and the fuselage
23 overlapped third overlaps 252 and the fuselage posterior segment cloth cover main body 251 is fixed on helicopter the 7th fixed
Part 253.Wherein, the third overlap 252 and the 7th fixing piece 253 with the fuselage posterior segment cloth cover main body 251
Connection.
In this present embodiment, it is preferable that the fuselage posterior segment cloth cover main body 251 and third overlap 252 are all made of double
The cloth of layer structure, including：Cladding material with fungicidal properties and waterproof performance and have thermal insulation property and submissive performance
Inner layer material, for example, outer layer is waterproof cloth, internal layer is panne velvet cloth.
Wherein, multiple 7th fixing pieces 253 are provided in fuselage posterior segment cloth cover main body 251.In this present embodiment, preferably
Ground, the 7th fixing piece 253 can be frenulum or pull stap.Preferably, multiple 7th fixing pieces 253 are arranged at intervals at machine
In body posterior segment cloth cover main body 251.
Wherein, it being made of due to fuselage sheet multiple isolated sheets, the lap-joint between different sheets may leak,
Thus be provided in fuselage posterior segment cloth cover main body 251 for overlapped the third overlap of leading portion sheet 23 in the fuselage
252。
Wherein, in order to enable sheet is equably bonded with helicopter corresponding site, not pocket water, go for a drive, cloth shroud rim needs tight
Installation position is pasted, 252 edge of third overlap is provided with rubber tube, to prevent invading for heavy rain, heavy snow, dust storm and hail
Enter.In addition, the method that sheet liner aviation balloon adhesive plaster also can be used.
Wherein, to prevent fuselage posterior segment sheet 25 from going mouldy, fuselage posterior segment cloth cover main body 251, third overlap are made
252 and the 7th the material of fixing piece 253 can pass through mould proof processing.For example, dipping can be used, pad, the side such as coating or spraying
Antibacterial agent is applied on cloth by method.
The aft body sheet 27 is used for the back segment of detachable mask fuselage, such as the positions such as empennage and tail.It is preferred that
Ground, the aft body sheet 27 include：Empennage sheet 271 and tail sheet 274.
The empennage sheet 271 is used for the empennage of detachable mask helicopter.In this present embodiment, it is preferable that the tail
Wing sheet 271 includes：Multiple empennage cloth cover main bodies 272, each empennage cloth cover main body 272 are used for the one of detachable mask helicopter
A empennage.
In order to guarantee empennage of helicopter from the intrusion of heavy rain, heavy snow, dust storm and hail, the empennage cloth cover main body 272
Should meet certain quality requirement, for example, waterproof performance, fungicidal properties, in terms of.In this present embodiment, preferably
Ground, the empennage cloth cover main body 272 use the cloth of double-layer structure, including：Outer layer material with fungicidal properties and waterproof performance
Expect and have the inner layer material of thermal insulation 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 in each empennage cloth cover main body 272 for by the empennage cloth cover main body 272
The 8th fixing piece 273 being fixed on helicopter.In this present embodiment, it is preferable that the 8th fixing piece 273 can be frenulum
Or pull stap.Preferably, the quantity of the 8th fixing piece 273 is multiple, and multiple 8th fixing pieces 273 are arranged at intervals at often
In a empennage cloth cover main body 272.
Wherein, to prevent empennage sheet 271 from going mouldy, the material for making empennage cloth cover main body 272 and the 8th fixing piece 273 can
To pass through mould proof processing.For example, can be used dipping, pad, antibacterial agent is applied on cloth by the methods of coating or spraying.
The tail sheet 274 is used for the tail of detachable mask helicopter.Preferably, as shown in Figure 10, the tail
Sheet 274 includes：Tail cloth cover main body 275, with overlapped the 4th overlap 276 of fuselage posterior segment sheet 25 and will be described
Tail cloth cover main body 275 is fixed on the 9th fixing piece 277 on helicopter.Wherein, the 4th overlap 276 and the described 9th
Fixing piece 277 is connect with the tail cloth cover main body 275.
In this present embodiment, it is preferable that the tail cloth cover main body 275 and the 4th overlap 276 are all made of double-layer structure
Cloth, including：Cladding material with fungicidal properties and waterproof performance and the internal layer material for having thermal insulation property and submissive performance
Material, for example, outer layer is waterproof cloth, internal layer is panne velvet cloth.
Wherein, multiple 9th fixing pieces 277 are provided in tail cloth cover main body 275.In this present embodiment, it is preferable that institute
Stating the 9th fixing piece 277 can be frenulum or pull stap.Preferably, multiple 9th fixing pieces 277 are arranged at intervals at tail cloth
In cover main body 275.
Wherein, it being made of due to fuselage sheet multiple isolated sheets, the lap-joint between different sheets may leak,
Thus be provided in tail cloth cover main body 275 for overlapped the 4th overlap 276 of fuselage posterior segment sheet 25.
Wherein, in order to enable sheet is equably bonded with helicopter corresponding site, not pocket water, go for a drive, cloth shroud rim needs tight
Installation position is pasted, 276 edge of the 4th overlap is provided with rubber tube, to prevent invading for heavy rain, heavy snow, dust storm and hail
Enter.In addition, the method that sheet liner aviation balloon adhesive plaster also can be used.
Wherein, to prevent tail sheet 274 from going mouldy, production tail sheet main body 275, the 4th overlap 276 and the 9th are solid
The material for determining part 277 can pass through mould proof processing.For example, can be used dipping, pad, antibacterial agent is applied in the methods of coating or spraying
It is added on cloth.
The embodiment of the invention also provides a kind of helicopter protective devices, including：Warning device 30 and above-mentioned helicopter
Full machine sheet 10, as shown in figure 11.Wherein, the structural block diagram of warning device 30 is illustrated only in Figure 11.
The warning device 30 includes：Controller 41, alarm 43, switch 45 and the multiple sensings being set on the outside of helicopter
Device 40.
When the complete not complete mask helicopter of machine sheet 10 of helicopter, exposed sensor 40 will be sent a signal to
The controller 41.Further, the output end of the sensor 40 is coupled with the input terminal of the controller 41.In this implementation
In example, the sensor 40 can be photosensitive sensor, for example, it may be photo resistance, infrared sensor etc..
The controller 41 is used to receive the signal that the sensor 40 is sent, and handles the signal, identifies
Just alarm 43 is controlled after the signal to alarm, and reminds staff to adjust the full machine sheet 10 of helicopter, so as to helicopter
Preferably protected.
Wherein, the controller 41 can be a kind of IC chip, the processing capacity 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), specific integrated circuit (Application Specific Integrated Circuit, ASIC), ready-made programmable gate
Array (Field Programmable Gate Array, FPGA) either other programmable logic device, discrete gate or crystal
Pipe logical device, discrete hardware components.General processor can be microprocessor or the processor is also possible to any routine
Processor etc..
The input terminal of the alarm 43 is coupled with the output end of the controller 41.The alarm 43 is used in failure work
Warning note is issued under condition, reminds staff to adjust the full machine sheet 10 of helicopter, preferably to be protected to helicopter.
Further, it when the controller 41 identifies the signal that sensor 40 is sent, just controls alarm 43 and sends warning note, it should
The mode of prompt can be auditory tone cues, be also possible to the combination etc. of signal lamp flash for prompting, or both.In the present embodiment
In, the alarm 43 can be combined aural and visual alarm, be also possible to buzzer, can also be warning lamp, or by buzzer and
The warning device etc. of warning lamp composition.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 and power supply connect
It connects, the other end of the switch 45 is connect with the power end of controller 41.Preferably, when switch 45 be closed when, controller 41 with
Conducting between power supply, controller 41 can work normally, and when switch 45 disconnects, the electricity between controller 41 and power supply is disconnected
It opens, controller 41 cannot work.
When not needing the full machine sheet 10 of mask helicopter, controller 41 can be controlled by switch 45 to work,
In order to avoid alarm 43 is constantly in alarm condition.
In conclusion the embodiment of the invention provides a kind of full machine sheet of helicopter and helicopter protective devices.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
The whole mode for being zero, can be bonded even closer with helicopter when in use, preferably protect to helicopter, reduce helicopter and exist
When open air is parked, the influence of wind and rain, hail, frost and snow to helicopter.On the other hand, the setting of muti-piece sheet, effectively prevents cloth
Cover is difficult to wear off, is difficult to the problem of folding storage when being an entirety, the efficiency worn/taken off is greatly enhanced, to subtract
Lack human and material resources, financial resources and time, saves cost.Meanwhile rotor sheet, weapon carrier sheet, nosing sheet,
Leading portion sheet, fuselage posterior segment sheet and aft body sheet are all made of the outer layer with fungicidal properties and waterproof performance in fuselage
Preferably protected with the double-layer structure of the internal layer for having thermal insulation property and submissive performance to helicopter, prevent in wet environment or
Sheet mildew etc. 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 has that structure is simple, protecting effect is good, makes
It is the advantages that with facilitating, being low in cost, easy to promote and utilize.
The foregoing is only a preferred embodiment of the present invention, is not intended to restrict the invention, for the skill of this field
For art personnel, the invention may be variously modified and varied.All within the spirits and principles of the present invention, made any to repair
Change, equivalent replacement, improvement etc., should all be included in the protection scope of the present invention.
Claims (10)
1. a kind of full machine sheet of helicopter, which is characterized 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 successively detachable 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 mask helicopter, the weapon carrier sheet is used for the weapon carrier of helicopter described in detachable mask,
Rotor of the rotor sheet for helicopter described in detachable mask.
2. the full machine sheet of helicopter according to claim 1, which is characterized in that the rotor sheet includes：Multiple rotors
Cloth cover main body is provided with for the rotor cloth cover main body to be fixed on the helicopter in each rotor cloth cover main body
On the first fixing piece.
3. the full machine sheet of helicopter according to claim 2, which is characterized in that the weapon carrier sheet includes：It is multiple
Weapon carrier cloth cover main body is provided in each weapon carrier cloth cover main body for by the weapon carrier cloth cover main body
The second fixing piece being fixed on the helicopter.
4. the full machine sheet of helicopter according to claim 3, which is characterized in that the nosing sheet includes：Round the clock
Capstan head sheet, cockpit sheet and head sheet are retouched in sight, and the sight round the clock retouches capstan head sheet and includes：It sees round the clock and retouches capstan head sheet master
Body and for described see round the clock to be retouched the third fixing piece that capstan head cloth cover main body is fixed on fuselage, the third fixing piece and institute
It states to see round the clock and retouches the connection of capstan head cloth cover main body；The head sheet includes：Head end cover main body and for by head end cover main body
The 4th fixing piece being fixed on head, the head end cover main body are connect with the 4th fixing piece；The cockpit sheet
Including：Cockpit cloth cover main body, with leading portion sheet overlapped the first overlap in the fuselage and for by the cockpit cloth
Cover main body is fixed on the 5th fixing piece on fuselage, first overlap and the 5th fixing piece with the cockpit cloth
Cover main body connection.
5. the full machine sheet of helicopter according to claim 4, which is characterized in that leading portion sheet includes in the fuselage：Machine
Leading portion cloth cover main body in body, with the nosing sheet overlapped the second overlap and by leading portion sheet master in the fuselage
Body is fixed on the 6th fixing piece on the helicopter；Second overlap and the 6th fixing piece are and in the fuselage
The connection of leading portion cloth cover main body.
6. the full machine sheet of helicopter according to claim 5, which is characterized in that fuselage posterior segment sheet includes：Machine
Body posterior segment cloth cover main body, with leading portion sheet overlapped third overlap in the fuselage and by fuselage posterior segment sheet
Main body is fixed on the 7th fixing piece on the helicopter；The third overlap and the 7th fixing piece with the fuselage
The connection of posterior segment cloth cover main body.
7. the full machine sheet of helicopter according to claim 6, which is characterized in that the aft body sheet includes：Empennage
Sheet and tail sheet, the empennage sheet include：Multiple empennage cloth cover main bodies are respectively provided in each empennage cloth cover main body
There is the 8th fixing piece for being fixed on the empennage cloth cover main body on empennage；The tail sheet includes：Tail sheet master
Body, with fuselage posterior segment sheet overlapped the 4th overlap and the tail cloth cover main body is fixed on the helicopter
The 9th fixing piece；4th overlap and the 9th fixing piece are connect with the tail cloth cover main body.
8. the full machine sheet of helicopter according to claim 7, which is characterized in that first fixing piece, described second are consolidated
Determine part, the third fixing piece, the 4th fixing piece, the 5th fixing piece, the 6th fixing piece, the 7th fixation
Part, the 8th fixing piece and the 9th fixing piece are frenulum or pull stap, and second overlap, the third are taken
It connects area, the 4th overlap edge and is provided with rubber tube.
9. the full machine sheet of helicopter according to claim 7, which is characterized in that it is described round the clock see retouch capstan head cloth cover main body,
The cockpit cloth cover main body, the head end cover main body, leading portion cloth cover main body, fuselage posterior segment sheet in the fuselage
Main body, each empennage cloth cover main body, the tail cloth cover main body, each rotor cloth cover main body, each weapon
Hanger cloth cover main body is double-layer structure, including：Outer layer with fungicidal properties and waterproof performance and has thermal insulation property and soft
The internal layer of pliable energy.
10. a kind of helicopter protective device, which is characterized in that including：Controller alarm, is switched, is set on the outside of helicopter
Multiple sensors and the full machine sheet of helicopter as described in any one of claims 1-9, the output of each sensor
End coupled with the input terminal of the controller, the switch is coupled with the power end of the controller, the controller it is defeated
Outlet is coupled with the input terminal 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 CN106741990A (en) | 2017-05-31 |
| CN106741990B true CN106741990B (en) | 2018-11-20 |
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| 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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Families Citing this family (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 |
Citations (5)
| 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 |
| 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 |
-
2016
- 2016-12-28 CN CN201611232863.7A patent/CN106741990B/en active Active
Patent Citations (5)
| 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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106741990A (en) | 2017-05-31 |
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