A propeller hub device with flapping restraint radial hinge shaft and helicopter with same
A hinge shaft and propeller hub technology, which is applied in the field of helicopters, can solve the problems of reliability, flight control and flexibility, strict requirements on the material of the rotor hub device, complex weight, etc., and achieve compact structure, good damping effect, and improved The effect of overall stiffness
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0027] refer to figure 1 and figure 2 , figure 1 It shows a schematic structural view of a three-blade propeller hub device with swinging restraint radial hinge shaft according to Embodiment 1 of the present invention, figure 2 It shows a schematic structural view of a four-bladed propeller hub device with a swing-constrained radial hinge shaft according to Embodiment 1 of the present invention, as shown in figure 1 and figure 2 As shown, a propeller hub device with a swinging restraint radial hinge shaft includes: a central body 7;
[0028] A plurality of waving hinge shafts 4 are uniformly integrated in the radial direction on the central body 7, and a bearing 5 is assembled on each of the waving hinge shafts 4, and a propeller hub 3 is assembled on each of the bearings 5, and each of the A paddle 1 is installed at the lower end of the propeller hub 3;
[0029] Wherein, when the swing hinge shaft 4 rotates around the central body 7 , it drives the propeller hub 3 and...
Embodiment 2
[0039] A helicopter, including the propeller hub device provided in Embodiment 1 of the present invention with a swing-constrained radial hinge shaft.
[0040] According to the helicopter provided by the present invention, a plurality of swinging hinge shafts 4 are evenly integrated in the radial direction on the central body 7, and the propeller hub 3 is set on the swinging hinge shafts 4 to directly rotate to realize the swinging of the blade 1, directly The associated parts are only the central body 7 fixed on the rotor shaft 8, the swinging hinge shaft 4, the propeller hub 3 and the paddle 1 set on the propeller hub 3. Since there are fewer parts and the turning point is the smallest, the overall rigidity can be improved. Thereby improving the effect of the natural frequency of the blade 1; at the same time, the viscoelastic waving damper 6 is built into the center body 7, without a separate outer chain structure, the structure is compact, the damping effect is good, the numb...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 


