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Wing full-motion airplane without rudder surface

A technology without rudder surfaces and wings, which is applied to aircraft parts, aircraft controls, aircraft transmissions, etc., can solve the problems of reduced aircraft performance, complex mechanism, and low cost performance, and achieve good stability and rotation

Inactive Publication Date: 2012-08-15
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At this stage, there are few types of fixed-wing aircraft that can solve short-distance take-off and landing, and the cost is high. Other aircraft that can take off and land vertically are complex in structure and heavy in weight. Some equipment added to achieve vertical take-off and landing reduces the performance of the aircraft. The price is too low

Method used

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  • Wing full-motion airplane without rudder surface
  • Wing full-motion airplane without rudder surface
  • Wing full-motion airplane without rudder surface

Examples

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Embodiment

[0023] The non-rudder wing all-moving aircraft of the present embodiment is as Figure 1~8 As shown, it includes a wing, a power system and a fuselage. The wing is connected to the fuselage through a rotating shaft mechanism, and the power system is located in the fuselage, and a drive mechanism connected to the power system is provided on the fuselage. The driving mechanism is connected with the leading edge of the wing.

[0024] The main beam web of the wing is provided with a shaft sleeve, which is fixedly connected to the wing, and a circular shaft is fixed at the corresponding position of the wing main beam on the fuselage, and the shaft diameter forms a gap with the inner diameter of the sleeve. Cooperate.

[0025] The fuselage and empennage are integrated.

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Abstract

The invention relates to a wing full-motion airplane without a rudder surface. The wing full-motion airplane comprises wings, a power system and a fuselage, wherein the wings are connected with the fuselage through rotating shaft mechanisms, the power system is positioned in the fuselage, and a driving mechanism connected with the power system is arranged on the fuselage, and connected with leading edges of the wings. The wing full-motion airplane without the rudder surface not only can realize various attitude control of the airplane by wing full-motion, but also can realize short take-off and landing, and is large in fuselage space.

Description

technical field [0001] The invention relates to a full-motion aircraft without rudder surfaces and wings, and belongs to the technical field of short take-off and landing aircraft and aviation vehicle design. Background technique [0002] At present, with the strengthening of our country's national defense, the aircraft carrier has become a necessary military strike force, and the development of the aircraft carrier will inevitably require corresponding carrier-based aircraft technology. Due to the limited distance between the decks of aircraft carriers, carrier-based aircraft are required to take off and land at short distances. At this stage, there are few types of fixed-wing aircraft that can solve short-distance take-off and landing, and the cost is high. Other aircraft that can take off and land vertically are complex in structure and heavy in weight. Some equipment added to achieve vertical take-off and landing reduces the performance of the aircraft. The price / perfor...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C9/00B64C13/30
Inventor 孙文杜晓松李凤鸣张立丰
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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