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Multi-axis aircraft
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A multi-axis aircraft and frame technology, applied in the field of aircraft, can solve the problems that objects cannot be transported and objects cannot be fixed on it
Active Publication Date: 2019-04-16
HARBIN UNIV
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But the utility model cannot transport objects, cannot fix objects on it
Method used
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specific Embodiment approach 1
[0032] Combine below Figure 1-12 To illustrate this embodiment, the present invention relates to an aircraft, more specifically a multi-axis aircraft, including a main frame body 1, a power assembly 2, an adjustment mechanism 3, a support structure 4 and a power supply assembly 5, the main body of the present invention The lower end of the frame body 1 can not only place objects of different sizes, but also hold objects of different sizes, and the upper end of the support structure 4 in the present invention can place objects, which is convenient for the multi-axis aircraft to transport objects.
[0033] There are four power assemblies 2, and the four power assemblies 2 are respectively fixedly connected to the front, rear, left, and right ends of the main frame body 1, and the front, rear, left, and right ends of the lower end of the adjustment mechanism 3 are hingedly connected to the main frame body 1, and the supporting structure The lower end of 4 is fixedly connected to...
specific Embodiment approach 2
[0034] Combine below Figure 1-12 To illustrate this embodiment, the main frame body 1 includes a middle square plate 1-1, a hinge seat 1-2, a sliding sleeve 1-3, a wire slot 1-4, an arm bar 1-5, a splint 1-6 and a bottom The supporting plate 1-7, the four ends of the front, rear, left, and right of the middle square plate 1-1 are fixedly connected with the arm bars 1-5, and the four arm bars 1-5 are all provided with the wire grooves 1-4, and the four wire grooves 1-4 extends to the middle square plate 1-1 and intersects, the four arm bars 1-5 are slidably connected with sliding sleeves 1-3, and the upper ends of the four sliding sleeves 1-3 are fixedly connected with hinged seats 1- 2. The lower ends of the four sliding sleeves 1-3 are fixedly connected with splints 1-6, and the inner sides of the lower ends of the four splints 1-6 are fixedly connected with bottom supporting plates 1-7. The four sliding sleeves 1-3 can slide along the four arm bars 1-5 respectively, thereb...
specific Embodiment approach 3
[0035] Combine below Figure 1-12To illustrate this embodiment, the main frame body 1 further includes rubber sheets 1-8, and the inner sides of the four bottom brackets 1-7 are all bonded and connected with rubber sheets 1-8. When objects are clamped between the two opposite bottom pallets 1-7, the rubber sheet 1-8 can play an anti-slip effect.
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Abstract
The invention relates to an aircraft, in particular to a multi-axis aircraft. The multi-axis aircraft comprises a main frame body, four power assemblies, a regulating mechanism, a supporting structureand a power assembly. The lower end of the main frame body can contain objects of different sizes and can clamp objects of different sizes, the upper end of the supporting structure can contain objects, and the multi-axis aircraft can convey the objects. The four power assemblies are fixedly connected to the left, right, front and back ends, the front, back, left and right ends of the lower end of the regulating mechanism are hinged to the main frame body, the lower end of the supporting structure is fixedly connected to the main frame body, the regulating mechanism is fixedly connected to the middle end of the supporting structure, and the power assembly is fixedly connected to the supporting structure.
Description
technical field [0001] The invention relates to an aircraft, more specifically a multi-axis aircraft. Background technique [0002] The application number is CN201620123725.4 for a turbojet multi-axis aircraft. This utility model discloses a turbojet multi-axis aircraft, which includes a multi-axis aircraft frame platform, multiple support arms, and multiple multi-axis aircraft power devices. and the control platform; the control platform is arranged on the upper end surface of the multi-axis aircraft frame platform, and the control system and the battery used by the electric turbojet or the fuel used by the fuel jet turbine are installed on the control platform; one end of the multiple support arms is respectively connected to multiple The multi-axis aircraft rack platform is connected, and multiple support arms are distributed around the multi-axis aircraft rack platform; the multiple multi-axis aircraft power devices are respectively arranged on the other ends of the mult...
Claims
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Application Information
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