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Deformation machine frame and aircraft

A technology of aircraft and frame, applied in the field of aircraft, can solve the problems of inconvenient carrying and transportation of the rotor, and achieve the effect of easy carrying and transportation, small size and convenient folding

Inactive Publication Date: 2018-09-04
SZ DJI TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the rotor protruding out of the fuselage is not easy to carry and transport

Method used

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  • Deformation machine frame and aircraft
  • Deformation machine frame and aircraft
  • Deformation machine frame and aircraft

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Embodiment Construction

[0026] Embodiments of the present invention will be further described below in conjunction with the accompanying drawings. The same or similar reference numerals in the drawings represent the same or similar elements or elements having the same or similar functions throughout.

[0027] In addition, the embodiments of the present invention described below in conjunction with the accompanying drawings are exemplary, and are only used to explain the embodiments of the present invention, and should not be construed as limiting the present invention.

[0028] In the present invention, unless otherwise clearly specified and limited, the first feature may be in direct contact with the first feature or the first and second feature may be in direct contact with the second feature through an intermediary. touch. Moreover, "above", "above" and "above" the first feature on the second feature may mean that the first feature is directly above or obliquely above the second feature, or simpl...

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PUM

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Abstract

The invention discloses a deformation machine frame (100) of an aircraft (10) and the aircraft(10). The deformation machine frame (10) comprises a center frame (12) and two arm assemblies(14). The twoarm assemblies are respectively arranged on the two sides of the center frame (12) and is rotationally connected with the center frame (12) so as to enable the deformation machine frame (10) can be switched between an extended state and a folded state. Each arm assembly (14) comprises a deformation rod (142) and a cross rod (144), wherein the deformation rod (142) comprises a first end (1422) rotatably connected to the central frame (12), and a second end (1424) connected to the cross bar (144), and the height of the second end (1424) is greater than the height of the first end (1422). In theextended state, the second ends (1424) of the two arm assemblies are respectively away from the center frame (12). In a folded state, the deformation rods (142) of the two arm assemblies (14) are laminated above the center frame (12).

Description

technical field [0001] The invention relates to the field of aircraft, in particular to a deformation frame of the aircraft and the aircraft. Background technique [0002] Unmanned aerial vehicles usually need to operate in different places and be transported over long distances. However, the rotor extending out of the fuselage is not easy to carry and transport. Contents of the invention [0003] Embodiments of the present invention provide a deformable frame of an aircraft and the aircraft. [0004] A deformation frame of an aircraft according to an embodiment of the present invention includes: [0005] center frame; and [0006] Two machine arm assemblies, the two machine arm assemblies are respectively arranged on both sides of the center frame, and are rotatably connected with the center frame, so that the deformation frame can be switched between an extended state and a folded state ; [0007] Wherein, the arm assembly includes a deformation rod and a cross bar,...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/30
CPCB64U10/14B64U30/293B64U80/00B64U2101/30B64U20/50B64U50/19
Inventor 梁贵彬
Owner SZ DJI TECH CO LTD