CN209108609U - A kind of fixed-wing model plane structure based on carbon beam - Google Patents
A kind of fixed-wing model plane structure based on carbon beam Download PDFInfo
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- CN209108609U CN209108609U CN201821820450.5U CN201821820450U CN209108609U CN 209108609 U CN209108609 U CN 209108609U CN 201821820450 U CN201821820450 U CN 201821820450U CN 209108609 U CN209108609 U CN 209108609U
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- wing
- fixed
- aileron
- carbon beam
- gear
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- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 title claims abstract description 58
- 229910052799 carbon Inorganic materials 0.000 title claims abstract description 58
- 238000005183 dynamical system Methods 0.000 claims abstract description 7
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 10
- 239000006261 foam material Substances 0.000 claims description 3
- 238000009434 installation Methods 0.000 abstract description 16
- 238000004519 manufacturing process Methods 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 9
- 238000010276 construction Methods 0.000 description 5
- 230000035939 shock Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000001771 impaired effect Effects 0.000 description 2
- 239000003381 stabilizer Substances 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000003032 molecular docking Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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Abstract
The fixed-wing model plane structure based on carbon beam that the utility model relates to a kind of.The structure member of the model plane includes: fuselage, wing, empennage and aileron and elevator, to connect the hinge of aerofoil and rudder face, to auxiliary positioning and as the carbon beam of main load-carrying member, and the landing gear mechanism being made of deflectable nose-gear and fixed main landing gear.Its dynamical system includes motor and matched propeller, and the connecting plate by being glued to fuselage head is fixed.Each control surface deflection is controlled using steering engine.The combination of each component of the model plane is mainly interpolation and splicing, absorbs impact power by carbon beam when simple and efficient installation may be implemented, and landing, and impact resistance is stronger.Model plane undercarriage damaged probability can be effectively reduced in the utility model, reduces the production and use cost of aeromodelling airplane, and vast airplane hobbyist especially beginner is suitble to use.
Description
Technical field
The utility model relates to aeromodelling airplane technical fields, specifically, more particularly to a kind of fixed-wing based on carbon beam
Model plane structure.
Background technique
Manipulation model plane are more welcomed by the people in recent years as a kind of outdoor sports, but new hand is in manipulation model plane drop
During falling, easily make model plane especially undercarriage impaired in default of experience, and damage and be frequently experienced in undercarriage
With fuselage link position, there are two the main reason for causing this accident: a deficiency of elevation angle when being landing leads to above-mentioned connection
The failure by shear along fuselage axis direction has occurred in position；Cause above-mentioned link position vertical the other is the elevation angle is excessive when landing
It is greater than the maximum stress that airframe structure can bear at this in the shock loading of fuselage.Above-mentioned two situations are because by machine
The limitation of stature material, caused by leading to the shock proof scarce capacity in undercarriage junction.
Utility model content
According to technical problem set forth above, and provide a kind of fixed-wing boat that can effectively bear biggish shock loading
Mould construction.
The technological means that the utility model uses is as follows:
A kind of fixed-wing model plane structure based on carbon beam, comprising: removable group of fuselage being made of head, middle body and rear body
Main body, removable group of wing, the tailplane and dynamical system for being connected to rear body tail portion, the middle body and rear body horizontal direction are opened
Equipped with wing mounting groove, removable group of the wing is fixed on wherein by being glued, and the middle body and rear body pass through fuselage carbon beam
It is connected, the head and middle body are fixed by being glued, and removable group of the wing is symmetrical two panels, pass through wing carbon beam phase
Even, main landing gear is fixed on fuselage carbon beam by passing through the fixture of the fuselage carbon beam, the left and right edges of nose-gear pedestal
Open up with the matched groove of fuselage carbon beam shape, allow nose-gear to be connected to middle body bottom.
Further, the internal diameter of the fixture is matched with the outer diameter of the fuselage carbon beam, and the bottom of the fixture is equipped with spiral shell
Hole, main landing gear pass through the screw and clamp across its interconnecting piece.
Further, the nose-gear includes nose-gear main body, passes through connecting shaft and the nose-gear main body phase
The nose-gear pedestal between nose-gear rocker arm and nose-gear main body and nose-gear rocker arm even, will by pull rod
Nose-gear rocker arm is connected with the rocker arm of direction steering engine, and the rotation of nose-gear is controlled by direction steering engine.
Further, the dynamical system includes the motor and propeller for being set to the head front end, the spiral
Paddle is mounted in the shaft of motor, and the motor is fixed on connecting plate by being spirally connected, and the connecting plate is glued in described
Head front end.
Further, the wingtip rear of the removable group of wing has aileron by aileron hinge connection, sets on the aileron
There is aileron rudder angle, the aileron passes through the aileron steering engine control deflection being arranged on removable group of wing, sets on the aileron steering engine
There is aileron steering engine rocker arm, the aileron steering engine is connected with aileron rudder angle by aileron pull rod.
Further, the rear of the tailplane has elevator by elevator hinge connection, sets on the elevator
There is elevator rudder angle, the elevator passes through the elevator steering engine control deflection being arranged on tailplane, the elevator rudder
Machine is equipped with elevator steering engine rocker arm, and the elevator steering engine rocker arm is connected with elevator rudder angle by elevator pull rod.
Further, four angles of the middle body and rear body interface are nearby equipped with mounting hole, total depth and fuselage carbon
Pole length is equal, and four fuselage carbon beams are fixed in the mounting hole of middle body or rear body, is fixed by being glued；
Butt hole there are two being set on the interface of the removable group of wing of two panels, the length phase of total depth and wing carbon beam
Deng, two fuselage carbon beams are fixed in butt hole, pass through be glued fix.
Further, the fuselage, wing, aileron, tailplane are EPP foam material.
Compared with the prior art, the utility model has the advantage that
1, main landing gear is mounted on the carbon beam of the intensity with higher level, rigidity, so that the fixed-wing model plane exist
Stronger shock loading is able to bear when landing, to reduce the impaired probability of undercarriage；
2, the utility model relates to a kind of fixed-wing model plane, structure height modularization, remove fuselage, each aerofoil, preceding
It is general that all components fallen other than the connecting plate of frame pedestal, the fixture of main landing gear and motor could alternatively be commercially available model plane
Accessory greatly reduces production and application cost, and more vast airplane hobbyist is suitble to use.
The utility model can be widely popularized in aeromodelling airplane technical field based on the above reasons.
Detailed description of the invention
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is done simply to introduce, it should be apparent that, the accompanying drawings in the following description is
Some embodiments of the utility model, for those of ordinary skill in the art, in the premise of not making the creative labor property
Under, it is also possible to obtain other drawings based on these drawings.
Fig. 1 is the utility model model plane overall diagram.
Fig. 2 is the utility model model plane component disassembly diagram.
Fig. 3 is the utility model head scheme of installation.
Fig. 4 is middle body, rear body and main landing gear scheme of installation.
Fig. 5 is nose-gear scheme of installation.
Fig. 6 is wing scheme of installation.
Fig. 7 is aileron steering engine scheme of installation.
Fig. 8 is tailplane scheme of installation.
In figure: 1, propeller；2, motor；3, fuselage；31, head；32, middle body；33, rear body；4, tailplane；41,
Horizontal stabilizer；42, elevator；5, wing；6, aileron；7, main landing gear；71, main landing gear main body；72, fixture；8, preceding
Fall frame；81, nose-gear main body；82, connecting shaft；83, nose-gear rocker arm；9, fuselage carbon beam；10, connecting plate；11, preceding to rise and fall
Frame pedestal；12, gasket；13, direction steering engine；131, direction steering engine rocker arm；132, direction steering gear pull rod；14, aileron hinge；15,
Wing carbon beam；16, aileron steering engine；161, aileron steering engine rocker arm；162, aileron pull rod；163, aileron rudder angle；17, elevator rudder
Machine；171, elevator steering engine rocker arm；172, elevator pull rod；173, elevator rudder angle；18, elevator hinge；
Specific embodiment
It should be noted that in the absence of conflict, the feature in the embodiments of the present invention and embodiment can
To be combined with each other.The utility model will be described in detail below with reference to the accompanying drawings and embodiments.
It is practical new below in conjunction with this to keep the objectives, technical solutions, and advantages of the embodiments of the present invention clearer
Attached drawing in type embodiment, the technical scheme in the utility model embodiment is clearly and completely described, it is clear that is retouched
The embodiment stated is only the utility model a part of the embodiment, instead of all the embodiments.Below at least one example
The description only actually of property embodiment be it is illustrative, never as to the utility model and its application or any limit used
System.Based on the embodiments of the present invention, those of ordinary skill in the art are obtained without making creative work
The every other embodiment obtained, fall within the protection scope of the utility model.
It should be noted that term used herein above is merely to describe specific embodiment, and be not intended to restricted root
According to the illustrative embodiments of the utility model.As used herein, unless the context clearly indicates otherwise, otherwise singular
Form be also intended to include plural form, additionally, it should be understood that, when in the present specification use term "comprising" and/or
When " comprising ", existing characteristics, step, operation, device, component and/or their combination are indicated.
Unless specifically stated otherwise, positioned opposite, the digital table of the component and step that otherwise illustrate in these embodiments
Up to the unlimited the scope of the utility model processed of formula and numerical value.Simultaneously, it should be clear that for ease of description, each shown in attached drawing
The size of a part is not to draw according to actual proportionate relationship.Skill known for person of ordinary skill in the relevant
Art, method and apparatus may be not discussed in detail, but in the appropriate case, and the technology, method and apparatus should be considered as awarding
Weigh part of specification.In shown here and discussion all examples, example should be construed as merely by appointing to occurrence
Property, not as limitation.Therefore, the other examples of exemplary embodiment can have different values.It should also be noted that similar
Label and letter similar terms are indicated in following attached drawing, therefore, once be defined in a certain Xiang Yi attached drawing, then with
In attached drawing afterwards do not need that it is further discussed.
In the description of the present invention, it should be understood that the noun of locality such as " front, rear, top, and bottom, left and right ", " laterally,
Vertically, vertically, it is horizontal " and " pushing up, bottom " etc. indicated by orientation or positional relationship be normally based on orientation or position shown in the drawings
Relationship is set, is merely for convenience of describing the present invention and simplifying the description, in the absence of explanation to the contrary, these nouns of locality
Do not indicate that and imply that signified device or element must have a particular orientation or be constructed and operated in a specific orientation, because
This should not be understood as the limitation to scope of protection of the utility model: the noun of locality " inside and outside " refers to the wheel relative to each component itself
Wide is inside and outside.
For ease of description, spatially relative term can be used herein, as " ... on ", " ... top ",
" ... upper surface ", " above " etc., for describing such as a device shown in the figure or feature and other devices or spy
The spatial relation of sign.It should be understood that spatially relative term is intended to comprising the orientation in addition to device described in figure
Except different direction in use or operation.For example, being described as if the device in attached drawing is squeezed " in other devices
It will be positioned as " under other devices or construction after part or construction top " or the device of " on other devices or construction "
Side " or " under its device or construction ".Thus, exemplary term " ... top " may include " ... top " and
" in ... lower section " two kinds of orientation.The device can also be positioned with other different modes and (is rotated by 90 ° or in other orientation), and
And respective explanations are made to the opposite description in space used herein above.
In addition, it should be noted that, limiting components using the words such as " first ", " second ", it is only for be convenient for
Corresponding components are distinguished, do not have Stated otherwise such as, there is no particular meanings for above-mentioned word, therefore should not be understood as to this
The limitation of utility model protection range.
As shown in Figure 1, the utility model provides a kind of fixed-wing model plane structure based on carbon beam, comprising: by head 31,
The removable group of fuselage main body 3 that middle body 32 and rear body 33 form, the wing 5 that removable group of two-piece type are connected to rear 33 tail portion of body
Tailplane 4, dynamical system and fuselage carbon beam 9 and wing carbon beam 15 as connector and main load-carrying member；The middle body
32 and 33 horizontal direction of rear body offer wing mounting groove, removable group of the wing 5 is fixed on wherein by being glued, it is described in
Body 32 is connected with rear body 33 by fuselage carbon beam 9, and the head 31 is crossed to be glued and be fixed with middle body logical 32, removable group of the wing
5 be symmetrical two panels, is connected by wing carbon beam 15, and main landing gear 7 is fixed by the fixture 72 for passing through the fuselage carbon beam 9
On fuselage carbon beam 9, the left and right edges of nose-gear pedestal 81 open up with the matched groove of 9 shape of fuselage carbon beam so that
Nose-gear 8 can be connected to middle 32 bottom of body.
The internal diameter of the fixture 72 is matched with the outer diameter of the fuselage carbon beam 9, and the bottom of the fixture 72 is equipped with screw hole, main
Undercarriage 7 is fastened by the screw and fixture 72 for passing through its interconnecting piece.
Landing Gear System includes rotatable nose-gear 8 and fixed main landing gear 7；Before the nose-gear 8 includes
Rise and fall frame body 81, the nose-gear rocker arm 83 being connected by connecting shaft 82 with the nose-gear main body 81 and nose-gear master
The nose-gear pedestal 11 between body 81 and nose-gear rocker arm 83, before nose-gear main body 81 is mounted on by gasket 12
On undercarriage pedestal 11, nose-gear rocker arm 83 is connected with the rocker arm 131 of direction steering engine 13 by pull rod 132, passes through direction
The rotation of the control nose-gear 8 of steering engine 13.
The dynamical system includes the motor 2 and propeller 1 for being set to 31 front end of head, and the propeller 1 is pacified
In the shaft of motor 2, the motor 2 is fixed on connecting plate 10 by being spirally connected, and the connecting plate 10 is glued in institute
State 31 front end of head.
The wingtip rear of the removable group of wing 5 is connected with aileron 6 by aileron hinge 14, and the aileron 6 is equipped with pair
Wing rudder angle 163, the aileron 6 pass through the control deflection of aileron steering engine 16 being arranged on removable group of wing 5, the aileron steering engine 16
It is equipped with aileron steering engine rocker arm 161, the aileron steering engine 16 is connected with aileron rudder angle 163 by aileron pull rod 162.
The rear of the horizontal stabilizer 41 of the tailplane 4 is connected with elevator 42 by elevator hinge 18, described
Elevator 42 is equipped with elevator rudder angle 173, and the elevator 42 passes through the elevator steering engine 17 being arranged on tailplane 4 and control
System deflection, the elevator steering engine 17 are equipped with elevator steering engine rocker arm 171, the elevator steering engine rocker arm 171 and elevator rudder
Angle 173 is connected by elevator pull rod 172.
Four angles of 33 interface of the middle body 32 and rear body are nearby equipped with mounting hole, and total depth and fuselage carbon beam 9 are long
Spend equal, four fuselage carbon beams 9 are fixed in the mounting hole of middle body 32 or rear body 33, are passed through to be glued and be fixed；
Butt hole there are two being set on the interface of the removable group of wing 5 of two panels, the length of total depth and wing carbon beam 15
Spend equal, two fuselage carbon beams are fixed in butt hole, are passed through to be glued and be fixed.
Fuselage 3, wing 5, aileron 6, tailplane 4 are the common EPP foam material of model plane.
The utility model additionally provides a kind of installation method of fixed-wing model plane,
As shown in Fig. 2, the installation method of the fuselage 3 are as follows: nearby there is peace at four angles of 33 interface of middle body 32 and rear body
Hole, total depth and 9 equal length of fuselage carbon beam are filled, four fuselage carbon beams 9 are fixed on middle body 32 or rear body 33 during installation
Mounting hole in, interpolation docking can be carried out, interface is using being glued fitting.The interface of head 31 and middle body 32 is also by glue
Connect fitting.
As shown in figure 3, the fixed-wing model plane using motor 2 as a source of power, and propeller 1 is mounted on electronic
In the shaft of machine 2, high-speed rotating propeller 1 can provide tractive force to model plane, and model plane is made to travel forward.In order to make tractive force
Motor 2 is fixed on connecting plate 10 using the method being spirally connected on model plane, is then glued to connecting plate 10 by useful effect
On head 31.
As shown in figure 4, the main landing gear 7 includes main landing gear main body 71,72 two parts of fixture.Fixture 72 can pass through
Fuselage carbon beam 9, threaded hole is arranged at bottom, after fixture 72 is passed through fuselage carbon beam 9, makes the hole and fixture 72 in main landing gear main body 71
The threaded hole of bottom is aligned, and main landing gear main body 71, fixture 72 and fuselage carbon beam 9 can be fixed on one using screw
It rises.
As shown in figure 5, the 8 use direction steering engine 13 of nose-gear is controlled.Nose-gear 8 includes nose-gear master
Body 81, connecting shaft 82, nose-gear rocker arm 83, and be mounted on nose-gear pedestal 11 by gasket 12, nose-gear 8 can
It is just loaded between two fuselage carbon beams 9 of middle 32 bottom of body, to be fixed.Use direction steering gear pull rod 132 will before
Undercarriage rocker arm 83 is connected with the rocker arm 131 of direction steering engine 13, i.e., the rotation of controllable nose-gear 8.
As shown in fig. 6, the installation method of the wing 5 are as follows: wing 5 divides for symmetrical two panels, and there are two right on interface
Hole is connect, the length of wing carbon beam 15 and the total depth of butt hole are equal, and may be mounted at wherein, play positioning and enhancing structure
Effect.It is same to be fixed by being glued.There are wing mounting groove, overall length and machine along its length on middle body 32 and rear body 33
5 chord length of the wing is equal, and wing 5 to be mounted on fuselage, wing 5 is combined with fuselage 3 by being glued.To ensure wing when installation
5 about fuselage 3 middle face it is symmetrical.
As shown in fig. 7, the installation method of the aileron 6 are as follows: the deflection that aileron 6 is controlled using aileron steering engine 16, aileron rudder
Machine 16 is mounted on wing 5, and is equipped with aileron steering engine rocker arm 161, and the installation site of aileron steering engine 16 can make aileron rudder just
Machine rocker arm 161 is aligned with the aileron rudder angle 163 on aileron 6, and aileron steering engine rocker arm 161 and aileron rudder angle 163 use aileron pull rod
162 are connected, and aileron rudder angle 163 can be driven by the swing of aileron steering engine rocker arm 161, and then drive aileron movement.
As shown in figure 8, the installation method of the tailplane 4 are as follows: rear 33 tail portion of body is provided with horizontal tail mounting groove, can be by water
4 interpolation of the horizontal tail wing wherein, and is glued with rear body 33.Installation keeps tailplane 4 to be ensured symmetrical about the middle face of fuselage 3.Make
The deflection that elevator 42 is controlled with elevator steering engine 17, is installed in rear 33 tail portion of body.Elevator steering engine 17 is furnished with elevator
Steering engine rocker arm 171 is connected with elevator rudder angle 173 by elevator pull rod 172.The actuation principle of elevator 42 and 6 phase of aileron
Together.
Finally, it should be noted that the above various embodiments is only to illustrate the technical solution of the utility model, rather than it is limited
System；Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should
Understand: it is still possible to modify the technical solutions described in the foregoing embodiments, or to some or all of
Technical characteristic is equivalently replaced；And these are modified or replaceed, it does not separate the essence of the corresponding technical solution, and this is practical new
The range of each embodiment technical solution of type.
Claims (8)
1. a kind of fixed-wing model plane structure based on carbon beam characterized by comprising be made of head, middle body and rear body
Removable group of fuselage main body, removable group of wing, the tailplane and dynamical system for being connected to rear body tail portion, the middle body and rear body
Horizontal direction offers wing mounting groove, and removable group of the wing is fixed on wherein by being glued, and the middle body and rear body are logical
It crosses fuselage carbon beam to be connected, the head and middle body are fixed by being glued, and removable group of the wing is symmetrical two panels, are passed through
Wing carbon beam is connected, and main landing gear is fixed on fuselage carbon beam by passing through the fixture of the fuselage carbon beam, nose-gear pedestal
Left and right edges open up with the matched groove of fuselage carbon beam shape, allow nose-gear to be connected to middle body bottom.
2. the fixed-wing model plane structure according to claim 1 based on carbon beam, which is characterized in that the internal diameter of the fixture with
The outer diameter of the fuselage carbon beam matches, and the bottom of the fixture is equipped with screw hole, and main landing gear passes through the screw across its interconnecting piece
With clamp.
3. the fixed-wing model plane structure according to claim 1 based on carbon beam, which is characterized in that the nose-gear includes
Nose-gear main body, the nose-gear rocker arm being connected by connecting shaft with the nose-gear main body and nose-gear main body are with before
Nose-gear rocker arm is connected by the nose-gear pedestal between undercarriage rocker arm by pull rod with the rocker arm of direction steering engine,
The rotation of nose-gear is controlled by direction steering engine.
4. the fixed-wing model plane structure according to claim 1 based on carbon beam, which is characterized in that the dynamical system includes
It is set to the motor and propeller of the head front end, the propeller is mounted in the shaft of motor, the motor
It is fixed on connecting plate by being spirally connected, the connecting plate is glued in the head front end.
5. the fixed-wing model plane structure according to claim 1 based on carbon beam, which is characterized in that the removable group of wing
Wingtip rear has aileron by aileron hinge connection, and the aileron is equipped with aileron rudder angle, and the aileron is by being arranged removable
Aileron steering engine on group wing controls deflection, and the aileron steering engine is equipped with aileron steering engine rocker arm, the aileron steering engine and aileron
Rudder angle is connected by aileron pull rod.
6. the fixed-wing model plane structure according to claim 1 based on carbon beam, which is characterized in that after the tailplane
Edge has elevator by elevator hinge connection, and the elevator is equipped with elevator rudder angle, and the elevator is existed by setting
Elevator steering engine on tailplane controls deflection, and the elevator steering engine is equipped with elevator steering engine rocker arm, the elevator rudder
Machine rocker arm is connected with elevator rudder angle by elevator pull rod.
7. the fixed-wing model plane structure according to claim 1 based on carbon beam, which is characterized in that the middle body and rear body pair
Four angles of junction are nearby equipped with mounting hole, total depth and fuselage carbon beam equal length, and four fuselage carbon beams are fixed on middle body
Or it in the mounting hole of rear body, is fixed by being glued；
It is set on the interface of the removable group of wing of two panels there are two butt hole, the equal length of total depth and wing carbon beam,
Two fuselage carbon beams are fixed in butt hole, are fixed by being glued.
8. the fixed-wing model plane structure according to claim 1-7 based on carbon beam, which is characterized in that the machine
Body, wing, aileron, tailplane are EPP foam material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821820450.5U CN209108609U (en) | 2018-11-06 | 2018-11-06 | A kind of fixed-wing model plane structure based on carbon beam |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821820450.5U CN209108609U (en) | 2018-11-06 | 2018-11-06 | A kind of fixed-wing model plane structure based on carbon beam |
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| Publication Number | Publication Date |
|---|---|
| CN209108609U true CN209108609U (en) | 2019-07-16 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821820450.5U Active CN209108609U (en) | 2018-11-06 | 2018-11-06 | A kind of fixed-wing model plane structure based on carbon beam |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109157847A (en) * | 2018-11-06 | 2019-01-08 | 大连理工大学 | A kind of fixed-wing model plane structure and installation method based on carbon beam |
| CN110949654A (en) * | 2019-12-25 | 2020-04-03 | 彭振根 | Aircraft |
| IT202200002444A1 (en) * | 2022-02-10 | 2023-08-10 | Heimdall S R L | Drone |
-
2018
- 2018-11-06 CN CN201821820450.5U patent/CN209108609U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109157847A (en) * | 2018-11-06 | 2019-01-08 | 大连理工大学 | A kind of fixed-wing model plane structure and installation method based on carbon beam |
| CN109157847B (en) * | 2018-11-06 | 2023-11-24 | 大连理工大学 | Fixed wing aeromodelling structure based on carbon rod and installation method |
| CN110949654A (en) * | 2019-12-25 | 2020-04-03 | 彭振根 | Aircraft |
| IT202200002444A1 (en) * | 2022-02-10 | 2023-08-10 | Heimdall S R L | Drone |
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| GR01 | Patent grant |