CN105797392A - A foldable tilted aeromodel support component - Google Patents
A foldable tilted aeromodel support component Download PDFInfo
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- CN105797392A CN105797392A CN201410824825.5A CN201410824825A CN105797392A CN 105797392 A CN105797392 A CN 105797392A CN 201410824825 A CN201410824825 A CN 201410824825A CN 105797392 A CN105797392 A CN 105797392A
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- limited block
- plate
- hack lever
- external part
- pack
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Abstract
The invention provides a foldable tilted aeromodel support component comprising upper/lower support plates, support rods, support rod sleeves, folding/unfolding limiting blocks and a bottom support. The foldable tilted aeromodel support component is characterized in that the upper/lower support plates are identical in structure and are X-shaped; the upper/lower support plates are connected by supporting pillars to form a layered hollow structure; the support rod sleeves, the folding limiting blocks and the unfolding limiting blocks are arranged in the layered hollow structure; the two ends of each support rod are connected with the corresponding support rod sleeve and one motor installing plate; the folding/unfolding limiting blocks can be used for limiting the positions of folding and unfolding of the support rods; holes used for supporting or installing the support rods in the support rod sleeves and the folding/unfolding limiting blocks have an inclined structure with the axis and the horizontal plane forming an upward angle. The foldable tilted aeromodel support component is simple in structure, convenient to manufacture and maintain, foldable and long in service life, has the excellent flight performances such as low noise, small vibration amplitude and stable take-off and landing, and further improves the customer experience of aeromodel lovers.
Description
Technical field
The present invention relates to the construction applications of model airplane support, particularly relate to a kind of folding oblique formula model airplane carriage assembly.
Background technology
The kind of model airplane is a lot, and wherein most external styling is fixing not folding, need to take a lot of space, carries and stores all inconveniences.Also having to adopt is designed to folding by the part-structure (such as wing, propeller etc.) of model airplane, such as patent CN201410055618 and CN201220225932, just wing, Design of Propeller become folding respectively, this has saved space to a certain extent, but for X-type four axle model airplane structure, the support constituted because of fuselage and propeller bracket is taken up space at most, only wing, Design of Propeller are become folding, then save space DeGrain.
Simultaneously, number of patent application is 2014203834710 provide a kind of X-type four axle model airplane skeleton, there is folding convenient, space-saving feature, but its noise in flight and Oscillation Amplitude are bigger, also it is not sufficiently stable when taking off or land, have impact on its flying quality, compare existing most of model airplane aircraft, its service life is not obviously improved.
Summary of the invention
It is an object of the invention to propose a kind of have simple in construction, easily manufactured, keep in repair the model airplane carriage assembly of the feature such as convenient, collapsible, have that flight noise is low, Oscillation Amplitude is little, the high flying quality well of stability of rising and falling concurrently simultaneously, carry with when using, both redundant space it had been not take up, there is again longer service life, strengthen model airplane fan's customer experience.
For reaching above-mentioned purpose, embodiments of the invention adopt the following technical scheme that
A kind of collapsible tilting model airplane carriage assembly, by upper bracket plate, lower carriage plate, hack lever, hack lever set, pack up limited block, launch limited block, motor mounting plate, bottom bracket form, it is characterized in that: described upper bracket plate, the lower carriage structure that hardens is identical, all in X-shaped；Upper bracket plate is along length direction lateral symmetry, supporting plate in length direction stage casing is main support plate, Liang Ge corner in the length direction both sides along main support plate, be respectively equipped with one extend perpendicularly out end, one project in parallel out end, it is equipped with oblique angle external part at each end that extends perpendicularly out with parallel external part place, extends perpendicularly out end, project in parallel out end, oblique angle external part, main support plate are that one block of carbon fiber sectional material plate is machined forms；It is equipped with hack lever set installing hole in the described junction extending perpendicularly out the junction held with oblique angle external part, projecting in parallel out end and oblique angle external part, is separately installed with hack lever set；It is provided with expansion limited block installing hole in the outside of each oblique angle external part, is provided with the outside of parallel external part to pack up limited block installing hole at each end that extends perpendicularly out, and be separately installed with and launch limited block, pack up limited block；It is provided with some upper and lower plates connecting holes at the outer place of upper bracket plate, lower carriage plate, support column can be passed through upper bracket plate, lower carriage plate are connected in layer shape hollow structure；Described hack lever is tubular type section bar, and its one end is connected with hack lever set, and the other end is installed with motor mounting plate；Described hack lever set is overlapped body by hack lever, hack lever trepanning forms, described pack up limited block by packing up limited block body, pack up limited block hole and form, described expansion limited block by launch limited block body, launch limited block hole form, and the axis of hack lever trepanning, pack up limited block hole axis, launch limited block hole axis all horizontal by equal angular upwards, its angle is 1 °～15 °, it is preferable that 5 °；Described bottom bracket is frame-type, and fixing with lower carriage plate is connected.
Further, the collapsible tilting model airplane carriage assembly of described one, it is characterised in that: on described upper bracket plate and lower carriage plate, further respectively have different special-shaped hole slot.
Further, in order to reduce weight and improve the aesthetics of supporting plate, upper bracket plate, lower carriage plate are equipped with different special-shaped hole slot.
The collapsible tilting model airplane carriage assembly of one provided by the invention, have employed, the supporting plate that lower double-layer structure is identical is layer shape hollow structure by Stud connection, hack lever set, pack up limited block, launch limited block and be arranged in layer shape hollow structure, hack lever two ends respectively with hack lever set, motor mounting plate connects, pack up limited block, launch limited block and can the position packed up with launch of hack lever be carried out spacing respectively, the hack lever set wherein adopted, pack up limited block, launching the hole for supporting or install hack lever on limited block all adopts axis horizontal by the incline structure of upper angle, making hack lever is the structure of upward, carriage assembly structure is made to obtain optimization, stress between each supporting plate and cradling piece is balanced more, there is integrated flight performance well when flight.The present invention have simple in construction, easily manufactured, keep in repair the model airplane carriage assembly of the feature such as convenient, collapsible, have that flight noise is low, Oscillation Amplitude is little, the high flying quality well of stability of rising and falling concurrently simultaneously, carry with when using, both redundant space it had been not take up, there is again longer service life, strengthen model airplane fan's customer experience.
Accompanying drawing explanation
In order to be illustrated more clearly that the embodiment of the present invention or technical scheme of the prior art, the accompanying drawing used required in embodiment or description of the prior art will be briefly described below, apparently, accompanying drawing in the following describes is only some embodiments of the present invention, for those of ordinary skill in the art, under the premise not paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings.
Fig. 1 is the front view of upper bracket plate in the present invention；
Fig. 2 is the installation diagram top view (without bottom bracket) that in the present invention, hack lever is packed up in upper and lower supporting plate；
Fig. 3 is the installation diagram front view (without motor mounting plate) that in the present invention, hack lever launches in upper and lower supporting plate；
Fig. 4 is the assembling structural representation after removing upper bracket plate in the present invention；
Fig. 5 is the close-up schematic view of hack lever assembling structure in the present invention；
Fig. 6 is the partial enlargement front view of hack lever assembling structure in the present invention；
Fig. 7 is the structural representation of hack lever set in the present invention；
Fig. 8 is the front view of hack lever set in the present invention；
Fig. 9 is the structural representation packing up limited block in the present invention；
Figure 10 is the front view packing up limited block in the present invention；
Figure 11 is the structural representation launching limited block in the present invention；
In figure: 1 upper bracket plate；2 hack levers；3 hack lever sets；4 pack up limited block；5 launch limited block；6 motor mounting plates；7 bottom brackets；8 lower carriage plates；10 support columns；101 oblique angle external parts；102 launch limited block installing hole；103 hack lever set installing holes；104 extend perpendicularly out end；105 pack up limited block installing hole；106 main support plates；107 upper and lower plates connecting holes；108 project in parallel out end；109 special-shaped hole slots；30 hack lever set bodies；31 hack lever trepannings；40 pack up limited block body；41 pack up limited block hole；50 launch limited block body；51 launch limited block hole.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is clearly and completely described, it is clear that described embodiment is only a part of embodiment of the present invention, rather than whole embodiments.Based on the embodiment in the present invention, the every other embodiment that those of ordinary skill in the art obtain under not making creative work premise, broadly fall into the scope of protection of the invention.
The collapsible tilting model airplane carriage assembly of one that the embodiment of the present invention proposes, as shown in Figure 1 to 11, by upper bracket plate 1, lower carriage plate 8, hack lever 2, hack lever set 3, pack up limited block 4, launch limited block 5, motor mounting plate, bottom bracket 7 form, it is characterized in that: described upper bracket plate 1, lower carriage plate 8 structure are identical, all in X-shaped；Upper bracket plate 1 is along length direction lateral symmetry, supporting plate in length direction stage casing is main support plate 106, Liang Ge corner in the length direction both sides along main support plate 106, it is respectively equipped with one to extend perpendicularly out 104, one, end and project in parallel out end 108,104 it is equipped with oblique angle external part 101 with parallel external part 108 place at each end that extends perpendicularly out, extends perpendicularly out end 104, project in parallel out end 108, oblique angle external part 101, main support plate 106 are that one block of carbon fiber sectional material plate is machined forms；In the described junction extending perpendicularly out end 104 and oblique angle external part 101, project in parallel out and hold the junction of 108 and oblique angle external part 101 to be equipped with hack lever set installing hole 103, be separately installed with hack lever set 3；It is provided with expansion limited block installing hole 102 in the outside of each oblique angle external part 101, is provided with the outside of parallel external part 108 to pack up limited block installing hole 105 at each end 104 that extends perpendicularly out, and be separately installed with expansion limited block 5, pack up limited block 4；It is provided with some upper and lower plates connecting holes 107 at the outer place of upper bracket plate 1, lower carriage plate 8, support column 10 can be passed through upper bracket plate 1, lower carriage plate 8 are connected in layer shape hollow structure；Described hack lever 2 is tubular type section bar, and its one end is overlapped 3 with hack lever and is connected, and the other end is installed with motor mounting plate 6；Described hack lever set 3 is overlapped body 30 by hack lever, hack lever trepanning 31 forms, described pack up limited block 4 by packing up limited block body 40, pack up limited block hole 41 and form, described expansion limited block 5 is made up of expansion limited block body 50, expansion limited block hole 51, and the axis of hack lever trepanning 31, pack up limited block hole 41 axis, launch limited block hole 51 axis all horizontal by equal angular upwards, its angle is 1 °～15 °, it is preferable that 5 °；Described bottom bracket 7 is in frame-type, and fixing with lower carriage plate 8 is connected.
Further, in order to alleviate weight and improve the aesthetics of supporting plate, upper bracket plate 1, lower carriage plate 8 are equipped with different special-shaped hole slot 109.
The above; being only the specific embodiment of the present invention, but protection scope of the present invention is not limited thereto, any those familiar with the art is in the technical scope that the invention discloses; change can be readily occurred in or replace, all should be encompassed within protection scope of the present invention.Therefore, protection scope of the present invention should be as the criterion with described scope of the claims.
Claims (3)
1. a collapsible tilting model airplane carriage assembly, by upper bracket plate (1), lower carriage plate (8), hack lever (2), hack lever set (3), pack up limited block (4), launch limited block (5), motor mounting plate (6), bottom bracket (7) form, it is characterized in that: described upper bracket plate (1), lower carriage plate (8) structure are identical, all in X-shaped；Upper bracket plate (1) is along length direction lateral symmetry, supporting plate in length direction stage casing is main support plate (106), Liang Ge corner in the length direction both sides along main support plate (106), be respectively equipped with one extend perpendicularly out end (104), one project in parallel out end (108), it is equipped with oblique angle external part (101) at each end (104) that extends perpendicularly out with parallel external part (108) place, extends perpendicularly out end (104), project in parallel out end (108), oblique angle external part (101), main support plate (106) are that one block of carbon fiber sectional material plate is machined forms；The junction that extends perpendicularly out end (104) and oblique angle external part (101) described, project in parallel out the junction of end (108) and oblique angle external part (101) and be equipped with hack lever and overlap installing hole (103), be separately installed with hack lever set (3)；Expansion limited block installing hole (102) it is provided with in the outside at each oblique angle external part (101), it is provided with the outside of parallel external part (108) packs up limited block installing hole (105) at each end (104) that extends perpendicularly out, and be separately installed with expansion limited block (5), pack up limited block (4)；It is provided with some upper and lower plates connecting holes (107) at the outer place of upper bracket plate (1), lower carriage plate (8), support column (10) can be passed through upper bracket plate (1), lower carriage plate (8) are connected in layer shape hollow structure；Described hack lever (2) is tubular type section bar, and its one end is connected with hack lever set (3), and the other end is installed with motor mounting plate (6)；Described hack lever set (3) is overlapped body (30) by hack lever, hack lever trepanning (31) forms, described pack up limited block (4) by packing up limited block body (40), pack up limited block hole (41) and form, described expansion limited block (5) is made up of expansion limited block body (50), expansion limited block hole (51), and the axis of hack lever trepanning (31), pack up limited block hole (41) axis, launch limited block hole (51) axis all horizontal by equal angular upwards, its angle is 1 °～15 °；Described bottom bracket (7) is in frame-type, and fixing with lower carriage plate (8) is connected.
2. the collapsible tilting model airplane carriage assembly of one according to claim 1, it is characterised in that: on described upper bracket plate (1) and lower carriage plate (8), further respectively have different special-shaped hole slot (109).
3. the collapsible tilting model airplane carriage assembly of one according to claim 1, it is characterised in that: it is all 5 ° horizontal by angle upwards at the axis of described hack lever trepanning (31), the axis packing up limited block hole (41), the axis that launches limited block hole (51).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410824825.5A CN105797392A (en) | 2014-12-27 | 2014-12-27 | A foldable tilted aeromodel support component |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410824825.5A CN105797392A (en) | 2014-12-27 | 2014-12-27 | A foldable tilted aeromodel support component |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105797392A true CN105797392A (en) | 2016-07-27 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410824825.5A Pending CN105797392A (en) | 2014-12-27 | 2014-12-27 | A foldable tilted aeromodel support component |
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| CN (1) | CN105797392A (en) |
Citations (10)
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|---|---|---|---|---|
| EP1502851A1 (en) * | 2002-04-16 | 2005-02-02 | Obschestvo s Ogranichennoi Otvetstvennostyu Midera-k | Aerodynamic lifting-thrusting propulsion device |
| CN201959566U (en) * | 2011-01-20 | 2011-09-07 | 杭州中天模型有限公司 | Wing for three-way fixed wing airplane |
| CN202244078U (en) * | 2011-07-29 | 2012-05-30 | 深圳市大疆创新科技有限公司 | Multi-rotary-wing unmanned aircraft |
| CN202526910U (en) * | 2012-05-04 | 2012-11-14 | 黑龙江科技学院 | Multi-shaft general flying vehicle frame |
| CN202605730U (en) * | 2012-05-02 | 2012-12-19 | 田瑜 | Multi-rotor aircraft |
| CN103359283A (en) * | 2013-06-29 | 2013-10-23 | 天津大学 | High-reliability unmanned aerial vehicle with tilt rotors |
| CN203461110U (en) * | 2013-09-10 | 2014-03-05 | 姜学海 | Irregularly-folded three-point landing type multi-axis unmanned aerial vehicle |
| CN203528812U (en) * | 2013-09-06 | 2014-04-09 | 天津云友科技有限公司 | Foldable four-rotor aircraft |
| CN203954686U (en) * | 2014-07-12 | 2014-11-26 | 张向东 | A kind of X-type four axle model airplane skeleton and install bins thereof |
| CN204319767U (en) * | 2014-12-27 | 2015-05-13 | 张向东 | A kind of collapsible tilting model airplane bracket component |
-
2014
- 2014-12-27 CN CN201410824825.5A patent/CN105797392A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1502851A1 (en) * | 2002-04-16 | 2005-02-02 | Obschestvo s Ogranichennoi Otvetstvennostyu Midera-k | Aerodynamic lifting-thrusting propulsion device |
| CN201959566U (en) * | 2011-01-20 | 2011-09-07 | 杭州中天模型有限公司 | Wing for three-way fixed wing airplane |
| CN202244078U (en) * | 2011-07-29 | 2012-05-30 | 深圳市大疆创新科技有限公司 | Multi-rotary-wing unmanned aircraft |
| CN202605730U (en) * | 2012-05-02 | 2012-12-19 | 田瑜 | Multi-rotor aircraft |
| CN202526910U (en) * | 2012-05-04 | 2012-11-14 | 黑龙江科技学院 | Multi-shaft general flying vehicle frame |
| CN103359283A (en) * | 2013-06-29 | 2013-10-23 | 天津大学 | High-reliability unmanned aerial vehicle with tilt rotors |
| CN203528812U (en) * | 2013-09-06 | 2014-04-09 | 天津云友科技有限公司 | Foldable four-rotor aircraft |
| CN203461110U (en) * | 2013-09-10 | 2014-03-05 | 姜学海 | Irregularly-folded three-point landing type multi-axis unmanned aerial vehicle |
| CN203954686U (en) * | 2014-07-12 | 2014-11-26 | 张向东 | A kind of X-type four axle model airplane skeleton and install bins thereof |
| CN204319767U (en) * | 2014-12-27 | 2015-05-13 | 张向东 | A kind of collapsible tilting model airplane bracket component |
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Application publication date: 20160727 |