CN112249298A

CN112249298A - Efficient ground effect wing ship elevator counterweight device

Info

Publication number: CN112249298A
Application number: CN202011079003.0A
Authority: CN
Inventors: 周还潮; 甘武奎; 李云龙
Original assignee: Zhengzhou Neptune Industry Co ltd
Current assignee: ZHENGZHOU HAIWANG MICRO MIST Co.,Ltd.
Priority date: 2020-10-10
Filing date: 2020-10-10
Publication date: 2021-01-22
Anticipated expiration: 2040-10-10
Also published as: CN112249298B

Abstract

The invention relates to the field of WIG craft, in particular to a high-efficiency WIG craft elevator counterweight device; the problem that the elevator of the original wing ship in the prior art is not balanced and can generate a downward inclination effect under the action of the gravity of the elevator is solved; the device comprises a horizontal stabilizer, an elevator and a steering shaft, and is characterized in that the steering shaft is fixedly arranged on both sides of the elevator, a counterweight for maintaining the gravity center of a counterweight device is arranged in the middle of the steering shaft, and a balance block is arranged at the far elevator end of the steering shaft; the invention can provide downward torque through the balance weight, thereby balancing the weight of the elevator, and the balance weight with the mass center in the steering shaft can adjust the whole mass center of the breeding system to be close to the steering shaft, thereby being convenient for the system to keep balance.

Description

Efficient ground effect wing ship elevator counterweight device

Technical Field

The invention relates to the field of WIG craft, in particular to a high-efficiency WIG craft elevator counterweight device.

Background

WIG craft utilizes the ground effect principle to make a vessel. The WIG craft can be divided into two types, namely an hydrofoil craft and an air wing craft, wherein the hydrofoil craft consists of a hull for providing buoyancy and a horizontal stabilizing surface with a certain aspect ratio. The surface effect is generated by the influence of the surface on the airflow when the horizontal stabilizer moves close to the surface, so that the lift-drag ratio of the horizontal stabilizer is increased, the propelling power can be reduced, and the sailing away from the ground can be kept.

The elevators of the small WIG craft are the "control surfaces" that control the lifting of the WIG craft. The horizontal tail wing of the WIG craft can be manipulated, and the pitching motion of the WIG craft is mainly controlled. The elevator is movable up or down about the elevator rotation axis. The elevator of the original wing ship is not balanced, and can generate a declination effect under the action of the gravity of the elevator. And the downdip force is not on the elevator rotating shaft, so that the bolt of the elevator rotating shaft is loosened after a long time, and further the elevator is loosened. Due to the long-term stress of the elevator, the elevator control system is stressed for a long time, and the elevator control system is adversely affected.

Practical contents

The invention provides an efficient counterweight device for an elevator of a ground effect wing ship, which solves the problems that the elevator of the original wing ship in the prior art is not balanced and can generate a downward inclination effect under the action of the gravity of the elevator.

The technical scheme of the invention is realized as follows: the invention discloses an efficient ground effect wing ship elevator counterweight device which comprises a horizontal stabilizing surface, an elevator and a steering shaft, wherein the steering shaft is fixedly arranged on two sides of the elevator, a counterweight for maintaining the gravity center of the counterweight device is arranged in the middle of the steering shaft, and a counterweight is arranged at the far end of the steering shaft, far away from the elevator.

Furthermore, the balance weight is a shot connected to the middle part of the rotary rudder shaft through a connecting rod.

Furthermore, the counterweight is a disk-shaped weight with the center of the circle in the axial projection of the rotary rudder shaft.

Further, the counterweight is a regular polygon weight with a mass center in the axial projection of the steering shaft.

Furthermore, the outer side of the horizontal stabilizer is provided with an outer wing capable of rotating along with the balance block, the outer wing comprises a front wing and a rear wing, the middle part of the rear wing is rotatably connected with the horizontal stabilizer through a steering shaft, the far rear end of the front wing is rotatably connected with the horizontal stabilizer, a limiting rod is arranged in the rear wing, and a sliding rod rotatably connected with the limiting rod is arranged in the front wing.

Further, the limiting rod can slide in the rear wing.

Furthermore, the far rudder shaft side of the elevator is of a hollow structure

The efficient ground effect wing ship elevator counterweight device disclosed by the invention has the following beneficial effects:

1. the invention can provide downward torque through the balance weight, thereby balancing the weight of the elevator, and the balance weight with the mass center in the steering shaft can adjust the whole mass center of the breeding system to be close to the steering shaft, thereby being convenient for the system to keep balance.

2. The invention belongs to the field of ground effect wing ships, and the flight height is lower, so that no matter the time of the elevator moving upwards or downwards is shorter, the horizontal flight attitude is kept to advance most of the time, when the elevator deflects, the balance block can drive the front wing and the rear wing to deflect, and at the moment, the rear wing of the front wing can be stressed in the direction opposite to the deflection direction of the balance block, and the auxiliary effect can be played when the elevator returns; or when the elevator or the steering shaft is loosened, the negative feedback rectification function can be realized, and the flight safety is ensured to a certain extent.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.

FIG. 1 is a top cross-sectional view of a horizontal stabilizer of the efficient WIG craft elevator counterweight apparatus of the present invention;

fig. 2 is a side sectional view of the horizontal stabilizer of the efficient WIG craft elevator counterweight of the present invention.

In the figure: 1 horizontal stabilizer, 2 elevators, 31 steering shafts, 32 balancing weights, 33 connecting rods, 34 balancing weights, 41 rear wings, 42 front wings and 43 limiting rods.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Example 1

Referring to fig. 1, when the direction of the elevator is consistent with the horizontal stabilizing plane, the balance block provides a torque which is opposite to the direction of the elevator and is close to the direction of the elevator, so that the loosening of a bolt of the elevator caused by the dead weight of the elevator on the steering shaft can be greatly avoided; when the elevator needs to deflect, the balance block can continuously counteract the moment caused by the gravity of the elevator, so that the elevator can deflect under smaller force, and the sensitivity of the elevator is effectively improved; when the deflection is finished and the elevator needs to keep the deflection position, the elevator far away from the steering shaft is of a hollow structure, and the steering shaft is provided with the circular balancing weight with the mass center falling on the steering shaft, so that the mass center of the balancing weight device can be effectively controlled on the steering shaft, and the situation that the elevator and the balancing weight return to the horizontal position due to the weight of the elevator and the balancing weight can be avoided.

Referring to fig. 2, when the elevator deflects upward, the link and the counterweight will deflect downward, and at the same time, the rear wing will be driven to deflect downward, at this time, the limiting rod capable of sliding inside the rear wing and the sliding rod inside the front wing will be pulled to slide out, the front wing will also deflect, at this time, the surface of the rear wing of the front wing forms a pressure that will point to the original position, so that the function of quickly returning to the right position can be realized after the elevator finely adjusts the direction.

Example 2

Referring to fig. 1, when the direction of the elevator is consistent with the horizontal stabilizer, the balance weight provides a torque which is opposite to the direction of the elevator and is close to the direction of the elevator, so that the bolt of the steering shaft can be greatly prevented from loosening due to the dead weight of the elevator; when the elevator needs to deflect, the balance block can continuously counteract the moment caused by the gravity of the elevator, so that the elevator can deflect under smaller force, and the sensitivity of the elevator is effectively improved; when the deflection is finished and the elevator needs to keep the deflection position, the elevator far away from the steering shaft is of a hollow structure, and the steering shaft is provided with the regular hexagonal counterweight block with the mass center falling on the steering shaft, so that the gravity center of the counterweight device can be effectively controlled on the steering shaft, and the situation that the elevator and the counterweight return to the horizontal position due to the weight of the elevator and the counterweight can be avoided.

Example 3

Referring to fig. 1, when the direction of the elevator is consistent with the horizontal stabilizer, the balance weight provides a torque which is opposite to the direction of the elevator and is close to the direction of the elevator, so that the bolt of the steering shaft can be greatly prevented from loosening due to the dead weight of the elevator; when the elevator needs to deflect, the balance block can continuously counteract the moment caused by the gravity of the elevator, so that the elevator can deflect under smaller force, and the sensitivity of the elevator is effectively improved; when the deflection is finished and the elevator needs to keep the deflection position, the side of the elevator far away from the steering shaft is of a hollow structure, and the steering shaft is provided with the regular octagonal balancing weight with the mass center falling on the steering shaft, so that the gravity center of the balancing weight device can be effectively controlled on the steering shaft, and the situation that the elevator and the balancing weight return to the horizontal position due to the weight of the elevator and the balancing weight can be avoided.

The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents, improvements and the like that fall within the spirit and principle of the present invention are intended to be included therein.

Claims

1. an efficient ground-effect wing ship elevator counterweight device, comprising a horizontal stabilizer, an elevator and a rudder shaft, it is characterized in that, both sides of the elevator are fixedly provided with a rudder shaft, and the middle of the rudder shaft is provided with a rudder shaft. There is a counterweight to maintain the center of gravity of the counterweight device, and a balance block is provided at the far end of the rudder shaft far from the elevator.

2 . The efficient elevator counterweight device for a ground effect ship according to claim 1 , wherein the balance weight is a lead ball connected to the middle of the rudder shaft through a connecting rod. 3 .

3 . The efficient elevator counterweight device for a ground effect ship according to claim 2 , wherein the counterweight is a pie-shaped weight with a center of the circle in the axial projection of the rudder shaft. 4 .

4 . The efficient elevator counterweight device for a ground effect ship according to claim 2 , wherein the counterweight is a regular polygonal weight whose center of mass is in the axial projection of the rudder shaft. 5 .

5 . The efficient elevator counterweight device for a ground-effect ship according to any one of claims 3 and 4, characterized in that, an outer wing that can rotate with the balance block is provided on the outside of the horizontal stabilizer, and the outer wing comprises Front wing and rear wing, the middle part of the rear wing is rotatably connected to the horizontal stabilizer through the rudder shaft, the far rear wing end of the front wing is rotatably connected to the horizontal stabilizer, and a limit rod is arranged in the rear wing, so The front wing is provided with a sliding rod rotatably connected with the limit rod.

6 . The efficient elevator counterweight device for a ground effect ship according to claim 5 , wherein the limit rod can slide in the rear wing. 7 .

7 . The efficient elevator counterweight device for a ground-effect wing craft according to claim 1 , wherein the elevator remote-rotating rudder shaft side is a hollow structure. 8 .