CN102632991A

CN102632991A - Wing full-motion airplane without rudder surface

Info

Publication number: CN102632991A
Application number: CN2012100833158A
Authority: CN
Inventors: 孙文; 杜晓松; 李凤鸣; 张立丰
Original assignee: Nanjing University of Aeronautics and Astronautics
Current assignee: Nanjing University of Aeronautics and Astronautics
Priority date: 2012-03-27
Filing date: 2012-03-27
Publication date: 2012-08-15

Abstract

The invention relates to a full-motion aircraft without rudder surfaces, including wings, a power system and a fuselage. There is a drive mechanism connected to the power system, which drive mechanism is connected to the leading edge of the wing. The full-motion aircraft without rudder surfaces and wings of the present invention can not only realize the control of various attitudes of the aircraft by the full motion of the wings, but also can take off and land at a short distance and have a large fuselage space.

Description

The moving full aircraft of no rudder face wing

Technical field

The present invention relates to the moving full aircraft of a kind of no rudder face wing, belong to short field aircraft and aviation aircraft design field.

Background technology

At present, along with the enhancing of China's national defense strength, the military attack strength that aircraft carrier has necessitated, and the development of aircraft carrier certainly will require corresponding carrier-borne aircraft technology.Because the aircraft-carrier-deck distance is limited, so require the carrier-borne aircraft STOL.It is less that present stage solves the fixed wing aircraft type of STOL, and cost is high, but the other VTOL aircraft has reduced the performance of aircraft because its mechanism is complicated, and weight is excessive for realizing some equipment that VTOL increases, and cost performance is low excessively.

Summary of the invention

The present invention is directed to the deficiency of the problems referred to above, propose a kind of can STOL, the fuselage space is big and the moving full aircraft of no rudder face wing that moved each attitude control that realizes aircraft by wing entirely.

The present invention is that the technical scheme that solves the problems of the technologies described above proposition is: the moving full aircraft of a kind of no rudder face wing; It is characterized in that: comprise wing, power system and fuselage; Said wing is connected with fuselage through rotating shaft mechanism; And power system is positioned at fuselage, and on fuselage, is provided with the driver train that is connected with power system, and said driver train is connected with the leading edge of a wing.

Preferred again: the girder web of said wing is provided with a rotating shaft axle sleeve, and this axle sleeve and wing are affixed, and the wing girder correspondence position on the said fuselage is fixed with a circular shaft, and this diameter of axle and sleeve diameter form free-running fit.

Further: said fuselage and empennage are an integral body.

Again further: also comprise the wing drive system, this wing drive system realizes that through controlling and driving mechanism wing rotates around the axis.

Preferred more again: said rotating shaft axle sleeve is the square-outside and round-inside type.

During use; The wing drive system realizes that through controlling and driving mechanism wing rotates around the axis; Just; Realize the pitch control of aircraft when realizing that through wing drive system controlling and driving mechanism wing rotates synchronously, realize the turning and the lift-over of aircraft when realizing that through wing drive system controlling and driving mechanism wing is differential.Specifically be that when driver train made two wings differential to the leading edge of a wing application of force, aircraft can be realized turning or lift-over.When driver train rotated two wings to the leading edge of a wing application of force synchronously, aircraft can be realized pitch control, promptly worked as two wings and increased the angle of attack synchronously, and aircraft comes back, and realizes climbing; When two wings reduced the angle of attack synchronously, aircraft was bowed, and realized diving.

The moving full aircraft of no rudder face wing of the present invention; Compare prior art; Has following beneficial effect: be connected with fuselage through rotating shaft mechanism because wing is stated in employing; Therefore driver train and leading edge of a wing bonded assembly are pressed design plan, can STOL, the fuselage space is big and moved each attitude control that realizes aircraft entirely by wing; Select for use rotating shaft axle sleeve and circular shaft to cooperate the rotating shaft mechanism that forms more to help the rotation of wing simultaneously; Adopt the wing drive system, make driver train realize that more easily wing rotates around the axis; The rotating shaft axle sleeve is made as the square-outside and round-inside type, makes that the stability of rotating shaft mechanism and rotation are better.

Description of drawings

Fig. 1: no rudder face wing is the profile three-view diagram of moving aircraft entirely;

Fig. 2: no rudder face wing is the structural representation of moving aircraft entirely;

Fig. 3 is Fig. 2 bottom bracket axle structural representation;

Fig. 4 is a wing pivot structure scheme drawing among Fig. 2;

Fig. 5 is Fig. 2 wing difference structure scheme drawing;

Fig. 6 is the synchronous rotational structure scheme drawing of Fig. 2 wing;

Fig. 7 is the maximum positive incidence structural representation of Fig. 2 starboard wing;

Fig. 8 is Fig. 2 port wing maximum negative angle of attack structural representation;

Fig. 9 is Fig. 2 tail structure scheme drawing;

Wherein: 1-fuselage, 2-wing, 3-empennage, the rotating shaft of 4-wing, 5-driver train, 6-rotating shaft axle sleeve.

The specific embodiment

Accompanying drawing discloses the structural representation of a preferred embodiment of the invention without limitation, below will combine accompanying drawing that technical scheme of the present invention at length is described.

Embodiment

The moving full aircraft of the no rudder face wing of present embodiment is shown in Fig. 1 ~ 8; Comprise wing, power system and fuselage; Said wing is connected with fuselage through rotating shaft mechanism; And power system is positioned at fuselage, and on fuselage, is provided with the driver train that is connected with power system, and said driver train is connected with the leading edge of a wing.

The girder web of said wing is provided with a rotating shaft axle sleeve, and this axle sleeve and wing are affixed, and the wing girder correspondence position on the said fuselage is fixed with a circular shaft, and this diameter of axle and sleeve diameter form free-running fit.

Said fuselage and empennage are an integral body.

Also comprise the wing drive system, this wing drive system realizes that through controlling and driving mechanism wing rotates around the axis.

Said rotating shaft axle sleeve is the square-outside and round-inside type.

Combine the preferred specific embodiment of the described the present invention of accompanying drawing only to be used to explain embodiment of the present invention above; Rather than as restriction to aforementioned goal of the invention and accompanying claims content and scope; Every foundation technical spirit of the present invention all still belongs to the present invention's technology and rights protection category to any simple modification, equivalent variations and modification that above embodiment did.

Claims

1. a full motion aircraft without rudder surface wing, is characterized in that: comprise wing, power system and fuselage, described wing is connected with fuselage by rotating shaft mechanism, and power system is positioned at fuselage, and in machine The body is provided with a drive mechanism connected with the power system, and the drive mechanism is connected with the leading edge of the wing.

2. The full-motion aircraft without rudder surfaces and wings according to claim 1, wherein the driving mechanism is a linkage mechanism.

3. according to claim 2 described non-rudder wing all-motion aircraft, it is characterized in that: the main girder web of described wing is provided with a rotating shaft bushing, and this bushing is fixedly connected with wing, and on described fuselage A circular shaft is fixed at the corresponding position of the main beam of the wing, and the shaft diameter forms a clearance fit with the inner diameter of the shaft sleeve.

4. The full-motion aircraft without rudder surfaces and wings according to claim 3, wherein the fuselage and empennage are integrated.

5. The full-motion aircraft without rudder surfaces according to claim 4, characterized in that: it also includes a wing drive system, and the wing drive system realizes the rotation of the wings around the axis of rotation by controlling the drive mechanism.

6. The all-motion aircraft without rudder surfaces and wings according to claim 5, characterized in that: the shaft sleeve is square on the outside and circular on the inside.