Dish-shaped aircraft

A dish-shaped aircraft and a dish-shaped technology, applied in the field of aircraft, can solve the problems of scattered distribution of components, insufficient lift change domain, large thrust, etc., and achieve the effects of improving balance controllability, improving stealth ability, and increasing suction capacity.

Inactive Publication Date: 2017-07-28
XIHUA UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Defect 1: There is a lot of wasted space under the dish-shaped skirt, and various components are scattered at the concave side of the dish-shaped skirt, without packaging and integration, forming an independent cabin, thus failing to form the functions of floating and diving on the water surface
[0005] Defect 2: The existing technology is to install ailerons on the edge of the dish-shaped skirt or use a gate device in the middle of the dish-shaped skirt to change the lift of the corresponding side, which has low efficiency and ins...

Method used

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Examples

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Embodiment Construction

[0028] The following embodiments will further illustrate a dish-shaped aircraft of the present invention in conjunction with the accompanying drawings

[0029] see figure 2 , a dish-shaped aircraft, comprising a power system (1), a dish-shaped skirt wing (2), and a dish-shaped diving cabin (3).

[0030] see image 3 , A power system (1) of a dish-shaped aircraft, comprising a rectifier tube (11), a coaxial dual rotor system (12), and a bracket (13), wherein the coaxial dual rotor system (12) comprises an engine, a gearbox, a differential Speeder, coaxial reverse propeller.

[0031] The inner wall of the above-mentioned rectifier tube (11) is a cylindrical tubular shape, the axis of which coincides with the central axis of the aircraft, and the propeller is wrapped inside the tube body. (2) Leave a distance for the fluid to flow out; the inlet (111) and the outlet (113) of the rectifier tube (11) are both trumpet-shaped, the shape of the rectifier tube (11) is bracelet-shap...

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PUM

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Abstract

The invention discloses a dish-shaped aircraft, relates to the technical field of aircraft, and provides an aircraft with increased functions of floating and diving on the water surface of the aircraft, high controllability, strong stealth capability and high thrust utilization. The auxiliary devices of the aircraft are packaged and integrated to form a saucer-shaped diving cabin with controllable airtightness. The saucer-shaped diving cabin is placed on the concave side of the saucer-shaped skirt wing to realize the floating and diving of the aircraft; The louver system is lower than three sets, and the louver system forms an annular array with the central axis of the dish-shaped skirt wing as the axis, thereby improving the controllability; the rectifier tube of the power system adopts the design of anti-radar detection and wind gathering.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a dish-shaped aircraft, more specifically, the invention relates to a dish-shaped aircraft with functions of floating and diving on the water surface, easy attitude control, stealth and improved thrust design. Background technique [0002] There are two schemes to use the Coanda effect (or Coanda effect) to make a dish-shaped aircraft. One is the British engineer Geoff Hatton's scheme, which uses a single-rotor fan structure at the top of the umbrella shell to provide downwash airflow. , use the Coanda effect (or Coanda effect) to generate lift, place a deflector at a specific angle on the outer surface of the shell to offset the torsional force, and evenly arrange four ailerons on the edge of the umbrella shell to achieve the balance of the aircraft and Flight direction control. Another solution is to replace the single-rotor fan in his solution with a coaxial dual-rotor fan b...

Claims

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Application Information

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IPC IPC(8): B64C39/06B64C35/02B64C17/00
CPCB64C39/06B64C17/00B64C35/006B64C35/008B64C39/001
Inventor 不公告发明人
Owner XIHUA UNIV
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