Flying car
A flying car and body technology, applied in the field of flying cars, can solve problems such as structural fatigue, and achieve the effect of less energy consumption and long range
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0022] Example one: such as figure 1 , 2 , 3 and 4, the integrated propulsion pneumatic system is a ducted fan system. The ducted fan system includes duct 9, fan 10, horizontal support stabilizer 13, horizontally supports flaperon 14 at the rear edge of stabilizer 13, vertical The stabilizer 15 is supported, and the rudder 16 at the rear edge of the stabilizer 15 is supported vertically.
[0023] This embodiment is a conventional ducted fan system. The duct 9 has a symmetrical airfoil profile. The fan 10 is a coaxial fan. The horizontal support stabilizer 13 and the vertical support stabilizer 15 cross to support the motor driving the fan 10. When the duct fan is in a horizontal attitude, it can generate direct lift to make the flying car take off vertically. When the duct fan system is in a vertical attitude with a small angle of attack, the airfoil composed of stabilizer 13 and flaperon 14 and duct 9 can be supported horizontally. The lift is generated, and the fan 10 can gener...
Embodiment 2
[0025] Embodiment two: such as Figure 5 , 6 , 7 and 8, the integrated propulsion aerodynamic system is a ducted wing system. The ducted wing system includes ducted wing 23, fan 10, flaperon 24 at the upper rear edge of ducted wing, support wing, and support wing The middle flap 28 at the trailing edge, the lower flap 27 at the lower rear edge of the ducted wing, the upper rudder 25 at the upper rear edge of the ducted wing 23, the lower rudder 26 at the lower rear edge of the ducted wing 23, at the fan At the back of 10, on the upper part of the duct wing 23, there is a slit through the duct wing 23.
[0026] The upper part, lower part, and support wing of the ducted wing 23 in this embodiment are all asymmetrical airfoils, and the fan 10 is a coaxial fan, and the slipstream generated has no slipstream torsion, which can provide good support for the support wing and ducted wing. The upper and lower parts of 23 are boosted by power, and the slipstream of the fan 10 can also pass ...
PUM
Abstract
Description
Claims
Application Information
- R&D Engineer
- R&D Manager
- IP Professional
- Industry Leading Data Capabilities
- Powerful AI technology
- Patent DNA Extraction
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.
© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com