Pulley type structure high lift device for dual-arc sliding rail

A technology of increasing lift device and double circular arc, which is applied in the field of aeronautical structure, can solve the problems of complex track shape, easy to get stuck, complicated processing, etc., and achieve the effect of compact structure, large retreat and small fairing area

Inactive Publication Date: 2011-07-06
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

But since there is only one radius, it is equivalent to Figure three In the mechanism, the dimensions of the AB and CF rods are determined, and they can only guide the flaps to reach the two positions accurately
[0009] Non-arc slide rails are generally straight line + arc slide rails. The radius of this slide rail is variable, so the flaps can reach the required three positions, but due to the complex shape of the track, it is easy to get stuck
[0010] The helical slide rail can well realize the spatial guidance of each position, but its processing is complicated and the cost is high, so it is only used by a few models

Method used

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  • Pulley type structure high lift device for dual-arc sliding rail
  • Pulley type structure high lift device for dual-arc sliding rail
  • Pulley type structure high lift device for dual-arc sliding rail

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Embodiment Construction

[0028] The present invention will be further described in detail in conjunction with the accompanying drawings and implementation examples.

[0029] A sliding rail pulley type structure increasing device with double circular arc sliding rails of the present invention is guided by the sliding rails, and the flaps can move to the three positions required by the aerodynamic force without getting stuck, such as Figure 4 As shown, the device includes a double-arc slide rail 1, a pulley 2, a bracket 3 and a flap 4.

[0030] Double arc slide rail 1 such as Figure 5 As shown, it includes a connecting piece 100, a first circular arc slide rail segment 101, a straight segment slide rail segment 102, a second circular arc slide rail segment 103 and a slide rail groove 104. The connecting piece 100 is used for the double arc slide rail 1 and The wings of the aircraft are connected, and the connecting piece 100, the first arc slide rail section 101, the straight section slide rail secti...

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Abstract

The invention discloses a pulley type structure high lift device for a dual-arc sliding rail, which comprises a dual-arc sliding rail, a pulley, a bracket and a flap, wherein the bracket is connected below the flap and connected with the pulley, the pulley is positioned in a sliding rail groove in the dual-arc sliding rail to ensure that the dual-arc sliding rail can slide on the pulley; the dual-arc sliding rail comprises a connecting member, a first arc sliding rail section, a straight line sliding rail section, a second arc sliding rail section and a sliding rail groove; the connecting member is used for connecting the dual-arc sliding rail with the wings of an airplane; the connecting member, the first arc sliding rail section, the straight line sliding rail section and the second arcsliding rail section are sequentially connected to form the dual-arc sliding rail, the sliding rail groove is arranged at the middle of the sliding rail; and the straight line sliding rail section isused for smoothly transiting the first arc sliding rail section and the second arc sliding rail section. The position of the flap is determined by the sliding rail, larger recession quantity and deflection angle can be realized in limited space compared with other mechanisms, and the lift drag ratio of the airplane during taking off and landing is increased.

Description

technical field [0001] The invention belongs to the field of aeronautical structures, and in particular relates to a sliding rail pulley structure increasing device with double circular arc sliding rails. Background technique [0002] Flaps are commonly used in various aircrafts. They can increase the lift of the aircraft in a short time, and are mainly used in the process of aircraft take-off and landing and special emergency situations. The multi-slotted Fuller flap retreats significantly while the flap rudder deflects, increasing the overall camber and wing area of ​​the wing, and improving the condition of the boundary layer through the airflow through the slits, thus increasing the lift increment. Compared with other types of flaps, its height-increasing effect has great advantages, and has been applied in many large and medium-sized transport aircraft abroad, and foreign countries have imposed strict technical blockades on my country in this field. In China, due to th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C3/38
Inventor 田云刘沛清舒培屈秋林周志杰
Owner BEIHANG UNIV
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