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Submerged folding wing synchronous lateral unfolding locking mechanism and unfolding locking method thereof

A locking mechanism and folding wing technology, applied in the aerospace field, can solve the problems of large influence of fluid, reduce the flight stability of missiles, affect the unfolding and locking process, etc., and achieve the effect of ensuring aerodynamic performance, reliable locking, and simple and compact structure.

Pending Publication Date: 2019-09-13
ZHEJIANG SCI-TECH UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Most of the wing surface folding and unfolding locking mechanisms currently used are exposed outside the projectile body in the folded state, and the overall aerodynamic performance of the missile will be affected to a certain extent in the folded state, reducing the flight stability of the missile; The folding and unfolding mechanism exposed outside the projectile body is greatly affected by the fluid during the folding and unfolding process, which directly affects the unfolding and locking process

Method used

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  • Submerged folding wing synchronous lateral unfolding locking mechanism and unfolding locking method thereof
  • Submerged folding wing synchronous lateral unfolding locking mechanism and unfolding locking method thereof
  • Submerged folding wing synchronous lateral unfolding locking mechanism and unfolding locking method thereof

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Embodiment Construction

[0019] The present invention will be further described below in conjunction with the accompanying drawings and embodiments.

[0020] Such as figure 1 , figure 2 , image 3 and Figure 6 As shown, the submerged folding wing synchronously expands the locking mechanism laterally, including a frame 1, a folding wing 2, a spring locking mechanism 3, a positioning block 4, a motor 5, a locking slider 6, a pin shaft 7, a screw rod 8, Torsion spring fixture 9, torsion spring 10, nut block 11, shaft coupling 12, spring 13 and spring pin 14; The output shaft of motor 5 is fixedly connected with screw mandrel 8 by shaft coupling 12; The base of motor 5 and frame 1 is fixed; the screw rod 8 and the frame 1 constitute a rotating pair, and the axial direction of the screw rod 8 is perpendicular to the platform surface of the frame 1; the nut block 11 and the screw rod 8 constitute a screw pair, and are connected with the locking slider 6 by screws ; The locking slider 6 is provided wit...

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Abstract

The invention discloses a submerged folding wing synchronous lateral unfolding locking mechanism and an unfolding locking method thereof. Existing airfoil folding and unfolding locking mechanisms areexposed outside projectiles in the folded state, the overall aerodynamic performance of missiles is affected in the folded state, and the folding and unfolding process is greatly affected by fluid. The mechanism of the invention comprises a machine frame, folding wings, a spring locking mechanism, a positioning block, a motor, a locking sliding block, a pin shaft, a screw rod, a torsional spring fixing member, a torsional spring, a nut block, a coupling, a spring and a spring pin. The N folding wings are synchronously unlocked by moving the locking sliding block in the axial direction of the screw rod; and the unlocked folding wings are unfolded under the action of the torsional spring, and are locked by the spring locking mechanism after being unfolded in position. The mechanism is storedin a projectile in the folded state, submerged folding of the missile wings is achieved, the aerodynamic performance of the missile is effectively ensured, and the lateral dimension of the missile isreduced.

Description

technical field [0001] The invention belongs to the technical field of aerospace and aviation, and relates to a missile folding wing unfolding and locking mechanism, in particular to a submerged folding wing synchronous lateral unfolding and locking mechanism and an unfolding and locking method thereof. Background technique [0002] Folding wings can reduce the radial size of the missile body, reduce the volume of the launching device, facilitate storage, transportation and launching in the launch box or launch tube, increase the carrying capacity of vehicles or ships, and improve the combat capability of weapons and equipment. The function of the folding wing unfolding locking mechanism is to make the wing surface fold before launching, and automatically unfold and lock reliably under the action of driving force after launching. Most of the wing surface folding and unfolding locking mechanisms currently used are exposed outside the projectile body in the folded state, and t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B10/14
CPCF42B10/14
Inventor 胡明李健高云高兴文吴梅赵德明杨景
Owner ZHEJIANG SCI-TECH UNIV
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