Aircraft system
First Claim
Patent Images
1. An aircraft system, comprising an aircraft apparatus comprising an image capturing device and a remote control, wherein:
- the remote control comprises a display, a first communication circuit adapted for transmitting aircraft control signals to the aircraft apparatus, and a second communication circuit adapted for receiving image signals of the image capturing device;
the display is adapted for displaying the image signals;
the aircraft apparatus comprises a gimbal, an aircraft unit is connected with the image capturing device through the gimbal;
the gimbal is connected with the aircraft unit through a gimbal connector;
the gimbal connector comprises a connecting body;
two buckling parts respectively outwardly extend from a front side and a rear side of the connecting body, so as to buckle with the gimbal for limiting the movement of the gimbal in the vertical direction and the front and rear directions;
an upper shock absorption plate is disposed between the gimbal connector and the gimbal;
two buckling components, respectively corresponding to the two buckling parts, are disposed at a top surface of the upper shock absorption plate;
the two buckling components are respectively buckled with the two buckling parts;
a position where the top surface of the upper shock absorption plate is close to the two buckling components has two channels, each of the two buckling components has an L-shaped cross section;
the two channels are respectively located under the two buckling components;
two first limit parts respectively outwardly extend from a front side and a rear side at a right end portion of the connecting body, and are respectively against a right end portion of the two buckling components;
the connecting body has an accommodating groove at a left end portion thereof;
a second limit part is disposed at a left end face of the accommodating groove, is located in the accommodating groove, and is against the left end face of the upper shock absorption plate.
0 Assignments
0 Petitions
Accused Products
Abstract
An aircraft system (1) includes an aircraft apparatus (31) including an image capturing device (33) and a remote control (32). The remote control (32) includes a display (321), a first communication circuit (322) adapted for transmitting aircraft control signals to the aircraft apparatus (31), and a second communication circuit (323) adapted for receiving image signals of the image capturing device. The display (321) is adapted for displaying the image signals.
-
Citations
16 Claims
-
1. An aircraft system, comprising an aircraft apparatus comprising an image capturing device and a remote control, wherein:
-
the remote control comprises a display, a first communication circuit adapted for transmitting aircraft control signals to the aircraft apparatus, and a second communication circuit adapted for receiving image signals of the image capturing device;
the display is adapted for displaying the image signals;the aircraft apparatus comprises a gimbal, an aircraft unit is connected with the image capturing device through the gimbal; the gimbal is connected with the aircraft unit through a gimbal connector;
the gimbal connector comprises a connecting body;
two buckling parts respectively outwardly extend from a front side and a rear side of the connecting body, so as to buckle with the gimbal for limiting the movement of the gimbal in the vertical direction and the front and rear directions;an upper shock absorption plate is disposed between the gimbal connector and the gimbal;
two buckling components, respectively corresponding to the two buckling parts, are disposed at a top surface of the upper shock absorption plate;
the two buckling components are respectively buckled with the two buckling parts;a position where the top surface of the upper shock absorption plate is close to the two buckling components has two channels, each of the two buckling components has an L-shaped cross section;
the two channels are respectively located under the two buckling components;
two first limit parts respectively outwardly extend from a front side and a rear side at a right end portion of the connecting body, and are respectively against a right end portion of the two buckling components;
the connecting body has an accommodating groove at a left end portion thereof;
a second limit part is disposed at a left end face of the accommodating groove, is located in the accommodating groove, and is against the left end face of the upper shock absorption plate. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16)
-
Specification