CN208813521U - Canard configuration airplane modular shelter coat - Google Patents
Canard configuration airplane modular shelter coat Download PDFInfo
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- CN208813521U CN208813521U CN201821331288.0U CN201821331288U CN208813521U CN 208813521 U CN208813521 U CN 208813521U CN 201821331288 U CN201821331288 U CN 201821331288U CN 208813521 U CN208813521 U CN 208813521U
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- module
- canard
- configuration airplane
- canard configuration
- fuselage
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Abstract
The utility model provides a kind of canard configuration airplane modular shelter coat, which includes: at least one of fuselage module, canard module, wing module, vertical tail module and propeller module；Wherein, fuselage module is used to be set in the fuselage of canard configuration airplane, canard module is used to be set in the canard of canard configuration airplane, wing module is used to be set in the wing of canard configuration airplane, vertical tail module is used to be set in the vertical tail of canard configuration airplane, and propeller module is used to be set in the propeller of canard configuration airplane；Wherein, canard module, wing module can be connect by the first connector with fuselage module；Vertical tail module can be connect by the second connector with wing module.Canard configuration airplane when the canard configuration airplane modular shelter coat can store parked outside or indoor long-time is protected.
Description
Technical field
The utility model belongs to aviation UAV field, more particularly, to a kind of canard configuration airplane modular shelter
Coat.
Background technique
For aircraft in outdoor parked and indoor long-term storage, body is exposed to outer be easy by sand and dust, sleet and rodent
The influence of animal causes unnecessary harm to body.Therefore, it needs to protect body during aircraft is parked, pass
The rain-proof cover of system can prevent rainwater and dust from directly falling in block upper surface to a certain extent, but can not be to body lower surface
Type protection, in inclement weather, rainwater and dust can contact body by cover opening, while traditional cover not can avoid
Rodent and insect enter body loss caused by internal unit from underpart.In addition to this, traditional cover is big
It is easy to be blown up under wind weather and fall off, body can not be protected in the presence of a harsh environment.
Canard configuration airplane progress when can be stored to parked outside or indoor long-time therefore, it is necessary to develop one kind
The canard configuration airplane modular shelter coat of protection.
Utility model content
The purpose of the utility model is to provide a kind of canard configuration airplane modular shelter coat, the canard configuration airplane moulds
Canard configuration airplane when block dress shield can store parked outside or indoor long-time is protected.
To achieve the goals above, the utility model provides a kind of canard configuration airplane modular shelter coat, the canard
Airplane modular shelter coat includes: fuselage module, canard module, wing module, vertical tail module and propeller mould
At least one of block；
Wherein, the fuselage module is used to be set in the fuselage of canard configuration airplane, and the canard module is for being arranged
On the canard of the canard configuration airplane, the wing module is used to be set in the wing of the canard configuration airplane, institute
Vertical tail module is stated for being set in the vertical tail of the canard configuration airplane, the propeller module is for being set in
On the propeller of the canard configuration airplane；
Wherein, the canard module, the wing module can be connect by the first connector with the fuselage module；Institute
Stating vertical tail module can be connect by the second connector with the wing module.
It preferably, further include weapon carrier module, the weapon carrier module is for being set in the canard configuration airplane
Weapon carrier on, the top of the weapon carrier module can be connect by hanger connecting piece with the wing module, described
The bottom of weapon carrier module is sewed with cinch cord.
It preferably, further include the frame module that rises and falls, the frame module that rises and falls is for being set in the undercarriage of canard configuration airplane
On, the undercarriage module top can be connect by rising and falling frame connector with the fuselage module, bottom and/or side setting
There is zipper.
It preferably, further include photoelectric nacelle module, the photoelectric nacelle module is for being set in the canard configuration airplane
Photoelectric nacelle on, the top of the photoelectric nacelle module can be connect by gondola connector with the fuselage module, described
Photoelectric nacelle module bottom is provided with cinch cord, is provided with flannelette napped fabric layer between the photoelectric nacelle module and the photoelectric nacelle.
It preferably, further include pitot protective module, the pitot protective module is for being set in the canard configuration
On the pitot of aircraft, anticollision buffer layer, the pitot are provided between the pitot protective module and the pitot
Protective module includes tip, and anti-collision alarm ribbon is provided at the tip.
Preferably, the fuselage module further includes overhauls window, and the overhauls window is provided with the top of the fuselage module
Portion and side, the edge of the overhauls window are provided with window connector.
Preferably, the bottom of the fuselage module is equipped with opening, and the opening passes through velcro or zipper seal.
Preferably, the wing module and the vertical tail module are respectively two.
Preferably, two wing modules are respectively arranged with red mark and green mark；Two vertical tail modules
It is respectively arranged with red mark and green mark.
Preferably, the fuselage module, the canard module, the wing module, the vertical tail module and described
Propeller module is prepared by nylon material.
The utility model has the beneficial effects that: passing through fuselage module, canard module, wing module, vertical tail module
And the setting of propeller module is set on canard configuration airplane corresponding position, is tightly connected by connector, and sand and dust, rain are prevented
Snow and rodent damage canard configuration airplane.
Other features and advantages of the utility model will then part of the detailed description can be specified.
Detailed description of the invention
The utility model illustrative embodiments are described in more detail in conjunction with the accompanying drawings, the utility model it is upper
It states and other purposes, feature and advantage will be apparent, wherein in the utility model illustrative embodiments, phase
Same reference label typically represents same parts.
Fig. 1 shows the main view of the canard configuration airplane modular shelter coat of one embodiment according to the present utility model
Figure.
Fig. 2 shows the side views of the canard configuration airplane modular shelter coat of one embodiment according to the present utility model
Figure.
Fig. 3 shows the vertical view of the canard configuration airplane modular shelter coat of one embodiment according to the present utility model
Figure.
Description of symbols
1, fuselage module；2, canard module；3, wing module；4, vertical tail module；5, weapon carrier module；6, it rises and falls
Frame module；7, photoelectric nacelle module；8, propeller module；9, pitot protective module.
Specific embodiment
Preferred embodiments of the present invention are described in more detail below.Although the following describe the utility model
Preferred embodiment, however, it is to be appreciated that may be realized in various forms the utility model without the implementation that should be illustrated here
Mode is limited.On the contrary, thesing embodiments are provided so that the utility model is more thorough and complete, and can be by this
The range of utility model is completely communicated to those skilled in the art.
The utility model provides a kind of canard configuration airplane modular shelter coat, the canard configuration airplane module chemoprevention
Protecting coat includes: at least one of fuselage module, canard module, wing module, vertical tail module and propeller module；
Wherein, the fuselage module is used to be set in the fuselage of canard configuration airplane, and the canard module is for being arranged
On the canard of the canard configuration airplane, the wing module is used to be set in the wing of the canard configuration airplane, institute
Vertical tail module is stated for being set in the vertical tail of the canard configuration airplane, the propeller module is for being set in
On the propeller of the canard configuration airplane；
Wherein, the canard module, the wing module can be connect by the first connector with the fuselage module；Institute
Stating vertical tail module can be connect by the second connector with the wing module.
Specifically, pass through the setting of fuselage module, canard module, wing module, vertical tail module and propeller module
It is set on canard configuration airplane corresponding position, is tightly connected by connector, prevent sand and dust, sleet and rodent to duck
Formula airplane damages.
Specifically, connector can be one of velcro or zipper, and adjacent block is connected by connector, form phase
To the dress shield of sealing, canard configuration airplane modular shelter coat is made to be suitable for bad weather, to canard configuration airplane into
Row omnibearing protection, protection effect is more preferably.
Specifically, on the one hand the dismounting of dress shield is convenient in modular design, on the other hand can be according to actual needs
To aircraft carry out integral protection or to each component of aircraft carry out it is separately protected, usage mode is more flexible.
It preferably, further include weapon carrier module, the weapon carrier module is for being set in the canard cloth
On the weapon carrier of office's aircraft, the top of the weapon carrier module can be connected by hanger connecting piece and the wing module
It connects, the bottom of the weapon carrier module is sewed with cinch cord.
It preferably, further include the frame module that rises and falls, the frame module that rises and falls is for being set in canard configuration airplane
On undercarriage, the undercarriage module top can be connect by rising and falling frame connector with the fuselage module, bottom and/or side
Face is provided with zipper.
Specifically, the frame module that rises and falls can carry out respectively enclosed guarantor to canard configuration airplane nose-gear and main landing gear
Shield, is fixed sealing using zipper.It is fixed with fuselage module junction using connector.
It preferably, further include photoelectric nacelle module, the photoelectric nacelle module is for being set in the canard cloth
On the photoelectric nacelle of office's aircraft, the top of the photoelectric nacelle module can be connected by gondola connector and the fuselage module
It connects, the photoelectric nacelle module bottom is provided with cinch cord, is provided between the photoelectric nacelle module and the photoelectric nacelle
Flannelette napped fabric layer.
Specifically, photoelectric nacelle module can carry out Global Macros to photoelectric nacelle, tightened, protected to root using drawstring
The flannelette napped fabric layer of shield module internal layer plays a protective role to gondola camera lens.
It preferably, further include pitot protective module, the pitot protective module is for being set in the duck
On the pitot of formula airplane, anticollision buffer layer is provided between the pitot protective module and the pitot, it is described
Pitot protective module includes tip, and anti-collision alarm ribbon is provided at the tip.
Specifically, pitot protective module can protect pitot, built-in anticollision buffer layer, and it is alert that tip hangs anticollision
Show ribbon.
Preferably, the fuselage module further includes overhauls window, and the overhauls window is provided with the fuselage mould
The top and side of block, the edge of the overhauls window are provided with window connector.
Specifically, overhauls window is arranged in fuselage roof and side maintenance position corresponding position in fuselage module, is convenient for engineering people
Member can be detected and be repaired to airborne equipment in the case where not dismantling fuselage module, and window edge can be carried out using velcro
Closing.
Preferably, the bottom of the fuselage module is equipped with opening, and the opening passes through velcro or zipper seal.
Preferably, the wing module and the vertical tail module are respectively two.
Preferably, two wing modules are respectively arranged with red mark and green mark；Two vertical ends
Wing module is respectively arranged with red mark and green mark.
Specifically, wing module can carry out Global Macros to wing, distinguish left and right using red green mark.Wing lower part is reserved
There are mooring ring window and weapon carrier window, window is closed using velcro, can expose mooring ring and weapon under wing after opening
Hanger interface.Wing body junction can be attached using velcro with fuselage.
Specifically, vertical tail module can carry out Global Macros to vertical tail, distinguish left and right using red green mark, utilize
Zipper is closed.Wing body junction can be attached using velcro with fuselage.
Preferably, the fuselage module, the canard module, the wing module, the vertical tail module
And the propeller module is prepared by nylon material.
It is highly preferred that nylon material is that military camouflage color nylon facing material plays certain sequestration.
Embodiment
Fig. 1 shows the main view of the canard configuration airplane modular shelter coat of one embodiment according to the present utility model
Figure.Fig. 2 shows the side views of the canard configuration airplane modular shelter coat of one embodiment according to the present utility model.Figure
3 show the top view of the canard configuration airplane modular shelter coat of one embodiment according to the present utility model.
As shown in Figure 1-Figure 3, which includes fuselage module 1, canard module 2, machine
Wing module 3, vertical tail module 4, propeller module 5, the frame module 6 that rises and falls, photoelectric nacelle module 7, pitot protective module 8,
Pitot protective module 9；
Wherein, fuselage module 1 is used to be set in the fuselage of canard configuration airplane, can be to fuselage Global Macros, under ventral
It is closed using velcro abutment joint.Overhauls window is arranged in fuselage roof and side maintenance position corresponding position in fuselage module,
Airborne equipment can be detected and be repaired in the case where being not to move out coat convenient for flight crew, window edge can utilize magic
The closing of exchange premium row.Fuselage module 1 and wing module 3, vertical tail module 4, rise and fall frame module 6 and the utilization of photoelectric nacelle module 7
Velcro is attached.
Wherein, canard module 2 is used to be set in the canard of the canard configuration airplane, and whole guarantor can be carried out to canard
Shield, wing body junction can be attached using velcro with fuselage.
Wherein, wing module 3 is used to be set in the wing of the canard configuration airplane, and whole guarantor can be carried out to wing
Shield distinguishes left and right using red green mark.Wing module 3 is reserved with mooring ring window and weapon carrier window, and window utilizes magic
Sealing is closed, and mooring ring and weapon carrier interface under wing can be exposed after opening.Wing body junction can using velcro and fuselage into
Row connection.
Wherein, vertical tail module 4 is used to be set in the vertical tail of the canard configuration airplane, can be to vertical tail
Global Macros are carried out, left and right is distinguished using red green mark, is closed using zipper.Wing body junction can utilize velcro and machine
Body is attached.
Wherein, weapon carrier module 5 is used to be set in the weapon carrier of the canard configuration airplane, can be to military under wing
Device and hanger are protected, and can be attached with wing module 1 using velcro, and tightened using cinch cord.
Wherein, the frame module 6 that rises and falls is used to be set in the undercarriage of canard configuration airplane, can rise and fall to nose-gear and master
Frame carries out enclosed protection respectively, and sealing is fixed using zipper.It is fixed with fuselage junction using velcro.
Wherein, photoelectric nacelle module 7 is used to be set in the photoelectric nacelle of the canard configuration airplane, can be to photoelectric nacelle
Global Macros are carried out, root is tightened using drawstring, protective module internal layer wraps up flannelette and plays protection work to gondola camera lens
With.
Wherein, propeller module 8 for be set on the propeller of the canard configuration airplane can it is whole to propeller into
Row protection, propeller blade part have anticollision buffer protection, and tip is identified equipped with anti-collision reflective.
Wherein, pitot protective module 9 is used to be set in the pitot of the canard configuration airplane, can to pitot into
Row protection, anticollision built in module buffer material, and tip hangs anti-collision alarm ribbon.
Each embodiment of the utility model is described above, above description is exemplary, and non-exclusive, and
And it is also not necessarily limited to disclosed each embodiment.Without departing from the scope and spirit of illustrated each embodiment, for
Many modifications and changes are obvious for those skilled in the art.
Claims (10)
1. a kind of canard configuration airplane modular shelter coat, which is characterized in that the canard configuration airplane modular shelter coat
It include: at least one of fuselage module, canard module, wing module, vertical tail module and propeller module；
Wherein, the fuselage module is used to be set in the fuselage of canard configuration airplane, and the canard module is for being set in institute
It states on the canard of canard configuration airplane, the wing module is used to be set in the wing of the canard configuration airplane, described to hang down
Straight tail module is used to be set in the vertical tail of the canard configuration airplane, and the propeller module is described for being set in
On the propeller of canard configuration airplane；
Wherein, the canard module, the wing module can be connect by the first connector with the fuselage module；It is described to hang down
Straight tail module can be connect by the second connector with the wing module.
2. canard configuration airplane modular shelter coat according to claim 1, which is characterized in that further include weapon carrier
Module, the weapon carrier module are used to be set in the weapon carrier of the canard configuration airplane, the weapon carrier module
Top can be connect by hanger connecting piece with the wing module, the bottom of the weapon carrier module is sewed with tightening
Rope.
3. canard configuration airplane modular shelter coat according to claim 1, which is characterized in that further include undercarriage mould
Block, the frame module that rises and falls can pass through for being set in the undercarriage of canard configuration airplane, the undercarriage module top
The frame connector that rises and falls is connect with the fuselage module, and bottom and/or side are provided with zipper.
4. canard configuration airplane modular shelter coat according to claim 1, which is characterized in that further include photoelectric nacelle
Module, the photoelectric nacelle module are used to be set in the photoelectric nacelle of the canard configuration airplane, the photoelectric nacelle module
Top can be connect by gondola connector with the fuselage module, the photoelectric nacelle module bottom is provided with cinch cord,
Flannelette napped fabric layer is provided between the photoelectric nacelle module and the photoelectric nacelle.
5. canard configuration airplane modular shelter coat according to claim 1, which is characterized in that further include that pitot is protected
Module is protected, the pitot protective module is used to be set in the pitot of the canard configuration airplane, the air speed protection of pipe
Anticollision buffer layer is provided between module and the pitot, the pitot protective module includes tip, is set at the tip
It is equipped with anti-collision alarm ribbon.
6. canard configuration airplane modular shelter coat according to claim 1, which is characterized in that the fuselage module is also
Including overhauls window, the overhauls window is provided with the top and side of the fuselage module, and the edge of the overhauls window is set
It is equipped with window connector.
7. canard configuration airplane modular shelter coat according to claim 1, which is characterized in that the fuselage module
Bottom is equipped with opening, and the opening passes through velcro or zipper seal.
8. canard configuration airplane modular shelter coat according to claim 1, which is characterized in that the wing module and
The vertical tail module is respectively two.
9. canard configuration airplane modular shelter coat according to claim 8, which is characterized in that two wing moulds
Block is respectively arranged with red mark and green mark；Two vertical tail modules are respectively arranged with red mark and green mark.
10. canard configuration airplane modular shelter coat according to claim 1, which is characterized in that the fuselage module,
The canard module, the wing module, the vertical tail module and the propeller module are prepared by nylon material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821331288.0U CN208813521U (en) | 2018-08-17 | 2018-08-17 | Canard configuration airplane modular shelter coat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821331288.0U CN208813521U (en) | 2018-08-17 | 2018-08-17 | Canard configuration airplane modular shelter coat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208813521U true CN208813521U (en) | 2019-05-03 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821331288.0U Active CN208813521U (en) | 2018-08-17 | 2018-08-17 | Canard configuration airplane modular shelter coat |
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| Country | Link |
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| CN (1) | CN208813521U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112429260A (en) * | 2020-09-21 | 2021-03-02 | 中国人民解放军空军南京航空四站装备修理厂 | Hail-suppression covering cloth for aircraft nose and aircraft body of fighter aircraft |
-
2018
- 2018-08-17 CN CN201821331288.0U patent/CN208813521U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112429260A (en) * | 2020-09-21 | 2021-03-02 | 中国人民解放军空军南京航空四站装备修理厂 | Hail-suppression covering cloth for aircraft nose and aircraft body of fighter aircraft |
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