Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Single aircraft

A single-person aircraft and aircraft technology, applied in the field of aircraft, can solve the problems of not being able to take into account vertical take-off and landing and high-speed flight, and achieve the effect of mutual conversion and smoothness

Inactive Publication Date: 2010-12-29
龙川
View PDF0 Cites 21 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] To sum up, the shortcomings of the existing single-person aircraft technology are: the inability to take into account both vertical take-off and landing and high-speed flight

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Single aircraft
  • Single aircraft
  • Single aircraft

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0032] Embodiment one, see appendix figure 1 , 2 , 3, 4, 5, and 6, the single-person aircraft of ordinary conventional layout, including cockpit, ducted fan propulsion system, ducted short wing 19, wing 4A, horizontal stabilizer and vertical stabilizer, is characterized in that: The cockpit is located in the middle of the aircraft. The base of the cockpit is the cabin body 1. The front of the cabin body 1 has a hatch 2, and the head is a hatch cover 3. When the aircraft takes off and lands vertically, the aircraft is in a vertical upward posture, and the driver stands in the cockpit accordingly. , when the aircraft is flying horizontally, the aircraft as a whole is in a horizontal forward attitude, and the driver is prone in the cockpit accordingly; Clutch 28, speed reducer 27, the rectifying plate 10 of supporting duct, wherein the axis of the fan shaft 26 of fan 9 is parallel with the longitudinal axis of aircraft, from the top view, the connecting line between the axes of ...

Embodiment 2

[0036] Embodiment two, see appendix Figure 7 , 8 and the single aircraft of the X-tail conventional layout in 9, comprising cockpit, ducted fan propulsion system, ducted short wing 19, wing 4A and X-tail, it is characterized in that: described cockpit is positioned at the middle part of aircraft, cockpit The basis of this is the cabin body 1, the cabin body 1 has a hatch door 2 on the front, and a hatch cover 3 on the head. For the horizontal forward posture, the driver is correspondingly lying prone in the cockpit; the ducted fan propulsion system is located at both sides of the cockpit, and the ducted fan propulsion system includes an engine 29 located in the engine compartment 7, a clutch 28, a speed reducer 27, The rectifier 10 supporting the duct, the fan 9 located in the duct 8, wherein the axis of the fan shaft 26 of the fan 9 is parallel to the longitudinal axis of the aircraft, and the connection between the axes of the two fan shafts 26 is seen from the plan view. ...

Embodiment 3

[0040] Embodiment three, see appendix Figure 10 , 11 12 and 13, the canard-type single-person aircraft of the layout comprises a cockpit, a ducted fan propulsion system, a ducted short wing 19, a wing 4B, a canard 39 and a vertical empennage, and it is characterized in that: the cockpit is located in the aircraft In the middle part, the basis of the cockpit is the cabin body 1, the front of the cabin body 1 has a hatch door 2, and the head is a hatch cover 3. When the aircraft takes off and lands vertically, the aircraft as a whole is in a vertical upward posture, and the driver stands in the cockpit accordingly, and the aircraft is horizontal. When flying, the aircraft is in a horizontal forward attitude as a whole, and the driver is lying prone in the cockpit accordingly; the ducted fan propulsion system is located at both sides of the cockpit, and the ducted fan propulsion system includes an engine 29 positioned in the engine compartment 7, a clutch 28, Speed ​​reducer 27...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention relates to a single aircraft. The single aircraft comprises a control cabin, a bypass fan propulsion system, bypass stub wings, airfoils, empennages or canards, wherein the base of the control cabin is a capsule; the front side of the capsule is provided with a capsule door, and the head of the capsule is provided with a capsule cover; the whole aircraft is vertically upward when vertically taking off and landing, and a pilot correspondingly stands in the control cabin; the whole aircraft is horizontally forward when horizontally flying, and the pilot correspondingly lies flat on the stomach in the control cabin; the bypass fan propulsion system is arranged on both sides of the control cabin through the bypass stub wings; the bypass fan propulsion system comprises an engine positioned inside an engine cabin, a clutch, a speed reducer, a supporting bypass commutator segment and a fan positioned in a bypass; the engine drives the fan to rotate so as to generate power; and the airfoils, horizontal empennages or X-shaped empennages control the transformation of vertical taking off and landing and horizontal flying. Because of the structure, the single aircraft realizes the vertical taking off and landing and high-speed flying and can stably transform between a vertical state and a horizontal state.

Description

technical field [0001] The invention relates to an aircraft, in particular to a single-person aircraft capable of vertical take-off and landing and high-speed flight. Background technique [0002] There are many types of single-person aircraft in the prior art, such as the single-person aircraft SOLOTREK-XFV developed by American Michael Mohill. This aircraft is driven by a piston engine to generate lift and pull the aircraft to take off. Without wings, the engine drives the ducted fan to generate lift during the entire flight, with slow speed, short range, and short battery life. The single-person aircraft "flying power wing" developed by the Swiss Yves Rossi is composed of a pair of foldable wings and 4 turbojet engines fixed under the wings. The driver fixes the "flying power wing" on the back , jump from the plane that is flying at high altitude, unfold and fold the wings and start the turbojet engine jet flight, and finally open the parachute to land. Although the "fly...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Applications(China)
IPC IPC(8): B64C29/00B64C1/00B64C3/00
Inventor 龙川
Owner 龙川
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products

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