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A foldable tilted aeromodel support component

A tilting, aviation technology, applied in entertainment, toys, toy airplanes, etc., can solve problems such as not significantly improved service life, unstable take-off or landing, and inconspicuous space-saving effect, and achieve good comprehensive flight performance and structure The effect of simplicity and high landing stability

Inactive Publication Date: 2016-07-27
张向东
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] There are many types of aviation models, most of which are fixed and cannot be folded, which takes up a lot of space and is inconvenient to carry and store
There are also designs to fold some of the structures of the aviation model (such as wings and propellers, etc.), such as patents CN201410055618 and CN201220225932, which respectively design the wings and propellers to be foldable, which saves space to a certain extent, but For the X-type four-axis aviation model structure, because the bracket composed of the fuselage and the propeller bracket occupies the most space, the space-saving effect is not obvious if only the wings and propellers are designed to be foldable
[0003] At the same time, the patent application No. 2014203834710 provides an X-type four-axis aviation model skeleton, which has the characteristics of convenient folding and space saving, but its noise and vibration amplitude are relatively large during flight, and it is not stable enough during take-off or landing, which affects its Flight performance, compared with most existing aircraft model aircraft, its service life has not been significantly improved

Method used

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  • A foldable tilted aeromodel support component
  • A foldable tilted aeromodel support component
  • A foldable tilted aeromodel support component

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Embodiment Construction

[0023] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0024] A foldable and tiltable model aircraft bracket assembly proposed by the embodiment of the present invention, such as Figure 1 to Figure 11 As shown, it consists of an upper bracket plate 1, a lower bracket plate 8, a frame rod 2, a frame rod cover 3, a retracted limit block 4, an unfolded limit block 5, a motor mounting plate, and a bottom bracket 7. It is characterized in that: The structure of the upper support plate 1 and the lower support plate 8 is exa...

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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 [0001] The invention relates to the structural field of aircraft model brackets, in particular to a foldable tilt-up type aircraft model bracket assembly. Background technique [0002] There are many types of aviation models, most of which are fixed and cannot be folded, which takes up a lot of space and is inconvenient to carry and store. There are also designs to fold some of the structures of the aviation model (such as wings and propellers, etc.), such as patents CN201410055618 and CN201220225932, which respectively design the wings and propellers to be foldable, which saves space to a certain extent, but For the X-type four-axis aviation model structure, because the frame composed of the fuselage and the propeller bracket occupies the most space, the space-saving effect is not obvious if the wings and propeller are only designed to be foldable. [0003] At the same time, the patent application No. 2014203834710 provides an X-type four-axis aviation mode...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): A63H27/18A63H27/24
Inventor 李立蔚张向东
Owner 张向东
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