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US 10,766,599 B2Granted
Aircraft and outer shell therefor
AssigneePowerVision Robot Inc.
InventorsWeifeng Zheng, Hui Han, Yi Zheng, Buwei Wei, Guozhi Zeng
Life of this patent
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Abstract
An aircraft and an outer shell therefor. The aircraft includes an outer shell; and main body components, accommodated in the outer shell. The outer shell includes: an inner cavity, the inner cavity being provided with a space for at least accommodating the main body components of the aircraft; an outer surface, the outer surface enclosing the inner cavity.
Claims17
An aircraft, comprising:
- an outer shell;
- and
- main body components, accommodated in the outer shell;
- wherein the outer shell comprises an inner cavity and an outer surface, the outer surface forms a first opening for a mechanical arm of the aircraft to expand and retract relative to the outer shell, and the main body components comprise a first installation mechanism that is located at the first opening and allows variation of the angle of the mechanical arm relative to a gravity center axis of the aircraft;
- wherein the mechanical arm comprises:
- an arm main body, the arm main body being installed on the first installation mechanism and being capable of being at least partially accommodated in the first opening when the mechanical arm is retracted;
- and
- an arm cover, the arm cover being installed on a side of the arm main body and being capable of at least partially covering the first opening when the mechanical arm is retracted.
5 more elements
An outer shell of an aircraft, the outer shell comprising:
- an inner cavity, the inner cavity having a space for at least accommodating main body components of the aircraft;
- and
- an outer surface, the outer surface enclosing the inner cavity;
- wherein the outer surface forms a first opening for a mechanical arm of the aircraft to expand and retract relative to the outer shell, and the main body components comprise a first installation mechanism that is located at the first opening and allows variation of the angle of the mechanical arm relative to a gravity center axis of the aircraft;
- wherein the mechanical arm comprises:
- an arm main body, the arm main body being installed on the first installation mechanism and being capable of being at least partially accommodated in the first opening when the mechanical arm is retracted;
- and
- an arm cover, the arm cover being installed on a side of the arm main body and being capable of at least partially covering the first opening when the mechanical arm is retracted.
5 more elements
Dependencies are inferred from the claim text.