一种整机旋翼测试装置及其飞行仿真训练模拟器
By designing a flight simulation training simulator that includes a test bench and a rotor power kit, the problems of low efficiency and low accuracy in rotor power kit testing have been solved, enabling efficient rotor power kit testing and training.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- CETC SPECIAL MISSION AIRCRAFT SYST ENG
- Filing Date
- 2025-06-24
- Publication Date
- 2026-07-17
AI Technical Summary
In existing technologies, rotor power kits require repeated disassembly and reassembly when tested on drones, which cannot simulate real-world operating conditions, resulting in low testing efficiency and low accuracy.
Design a flight simulation training simulator, including a test bench and a detachable rotor power unit. The test bench is equipped with a power battery, a navigation flight controller and a remote control receiver. It can simulate the real-world operating conditions of the rotor power unit on a drone and control the rotation speed and tilt angle of the rotor power unit through the navigation flight controller to achieve flight and hovering functions.
It enables efficient testing of UAV rotor power systems, improves testing accuracy, and can be used for training and hovering exercises to simulate real-world operating conditions.
Smart Images
Figure CN224519418U_ABST
Abstract
Claims
1. A flight simulation training simulator, characterized in that, include: The stand (1) has installation areas at all four corners; Four rotor power units (2) are detachably and correspondingly installed in the four installation areas; The support (3) is located in the middle of the platform (1). The support (3) is equipped with a power battery (5), a navigation flight controller (6) and a remote control receiver (7). The power battery (5) is electrically connected to the four rotor power units (2), the navigation flight controller (6) and the remote control receiver (7). The navigation flight controller (6) is communicatively connected to the remote control receiver (7) and the four rotor power units (2).
2. The flight simulation training simulator of claim 1, wherein, The platform (1) includes two longitudinal beams (11) and two transverse beams (12). A first gap is provided between the two longitudinal beams (11) in the transverse direction, and each of the transverse beams (12) is located in the first gap and its two ends are respectively provided on the two longitudinal beams (11). A second gap is provided between the two crossbeams (12) along the longitudinal direction. Each of the longitudinal beams (11) has two installation areas located on both sides of the second gap. The support (3) is provided between the middle parts of the two crossbeams (12).
3. The flight simulation training simulator of claim 2, wherein, Each of the installation areas is provided with a longitudinally adjustable main mounting base (21), and the rotor power kit (2) is mounted on the main mounting base (21).
4. The flight simulation training simulator of claim 3, wherein, Each of the beams (12) is adjustable at both ends along the longitudinal direction to adjust the longitudinal length of the installation area.
5. The flight simulation training simulator of claim 4, wherein, Each rotor power unit (2) includes a rotor ESC (22), a rotor motor (23), and a rotor propeller (24). The rotor ESC (22) and the rotor motor (23) are both located on the main mounting base (21), and the rotor motor (23) is connected to the rotor propeller (24) on its rotation axis. The rotor ESC (22) is communicatively connected to the navigation flight controller (6) and the rotor motor (23).
6. The flight simulation training simulator of any one of claims 2 to 5, wherein, The support (3) is also provided with an optical fiber inertial navigation system (8), which is communicatively connected to the navigation flight control system (6).
7. The flight simulation training simulator of claim 6, wherein, The support (3) is a hollow box, the top of which is detachably mounted on the two crossbeams (12), and the hollow box has a side opening on one and / or both sides along the transverse direction.
8. The flight simulation training simulator of claim 7, wherein, The top of the hollow box is provided with a top opening, and the top opening of the hollow box is provided with opposite connecting plates (10) on both sides along the horizontal direction. Each of the crossbeams (12) is adjustablely provided on the connecting plate (10) along the longitudinal direction.
9. The flight simulation training simulator of claim 8, wherein, The top opening cover of the hollow box is provided with a support plate (4), and the support plate (4) is provided on both sides of the longitudinal direction on the two crossbeams (12) and is adjustable in the longitudinal direction. The navigation flight controller (6), the remote control receiver (7), the fiber optic inertial navigation system (8), and the power battery (5) are all located inside the hollow box, or the navigation flight controller (6), the remote control receiver (7), and the fiber optic inertial navigation system (8) are located inside the hollow box, and the power battery (5) is located outside the hollow box and is located on the support plate (4).
10. An entire-rotor test apparatus characterized by comprising: It includes a test component set and a flight simulation training simulator as described in any one of claims 1 to 9.