Light pressure driven nano engine and driving method thereof
A kind of engine and nanotechnology, applied in the field of nanometers, can solve the problems of harsh conditions for the development of nanoengines, difficult control of the reaction process of chemical substances, etc.
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0049] This embodiment provides a figure 1 The photopressure-driven nano-engine of the shown structure comprises a hollow fuselage 1 in the shape of a spheroid; and two wings fixed on the fuselage 1, the two wings have the same size, including a The wing frame 2 and the aluminized PET film 3 covered on the wing frame 2; both wings are perpendicular to the long axis of the fuselage 1 and are located on the short axis section of the fuselage 1.
[0050] In this embodiment, the material of the fuselage 1 is SiO 2 The nanomaterial has a thickness of 30nm; the major axis radius of the fuselage 1 is 120nm, the minor axis radius is 80nm, and the oblateness α is about 0.33.
[0051] In the present embodiment, the shape of the wing frame 2 is fan-shaped, the radius of the fan is 500nm, and the central angle of the fan is 100°; the wing frame 2 is made of TiO 2 surrounded by nanotubes, TiO 2 The nanotubes have a radius of 10 nm.
[0052] In this embodiment, the thickness of the alum...
Embodiment 2
[0062] This embodiment provides a figure 1 The photopressure-driven nano-engine of the shown structure comprises a hollow fuselage 1 in the shape of a spheroid; and two wings fixed on the fuselage 1, the two wings have the same size, including a The wing frame 2 and the aluminized PET film 3 covered on the wing frame 2; both wings are perpendicular to the long axis of the fuselage 1 and are located on the short axis section of the fuselage 1.
[0063] In this embodiment, the material of the fuselage 1 is SiO 2 The nanomaterial has a thickness of 30nm; the major axis radius of the fuselage 1 is 120nm, the minor axis radius is 80nm, and the oblateness α is about 0.33.
[0064] In the present embodiment, the shape of the wing frame 2 is fan-shaped, the radius of the fan is 600nm, and the central angle of the fan is 120°; the wing frame 2 is made of TiO 2 surrounded by nanotubes, TiO 2 The nanotubes have a radius of 10 nm.
[0065] In this embodiment, the thickness of the alum...
Embodiment 3
[0075] This embodiment provides a figure 1 The photopressure-driven nano-engine of the shown structure comprises a hollow fuselage 1 in the shape of a spheroid; and two wings fixed on the fuselage 1, the two wings have the same size, including a The wing frame 2 and the aluminized PET film 3 covered on the wing frame 2; both wings are perpendicular to the long axis of the fuselage 1 and are located on the short axis section of the fuselage 1.
[0076] In this embodiment, the material of the fuselage 1 is SiO 2 The nanomaterial has a thickness of 30nm; the major axis radius of the fuselage 1 is 120nm, the minor axis radius is 80nm, and the oblateness α is about 0.33.
[0077] In the present embodiment, the shape of the wing frame 2 is fan-shaped, the radius of the fan is 500nm, and the central angle of the fan is 100°; the wing frame 2 is made of TiO 2 surrounded by nanotubes, TiO 2 The nanotubes have a radius of 10 nm.
[0078] In this embodiment, the thickness of the alum...
PUM
| Property | Measurement | Unit |
|---|---|---|
| Radius | aaaaa | aaaaa |
| Central angle | aaaaa | aaaaa |
| Thickness | aaaaa | aaaaa |
Abstract
Description
Claims
Application Information
Login to View More 


