A modified missile pylon for fixed-wing aircraft model

A fixed-wing and missile technology, applied in transportation and packaging, military equipment configuration, aircraft parts, etc., can solve the problems of zero versatility, high cost, missile falling, etc., and achieves firm grip, low cost, disassembly and assembly. handy effect

Active Publication Date: 2017-03-22
启东市机关液化气有限责任公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Then when modifying the design of the pylons for missiles and smoke pipes, the existing pylons are either too complicated and expensive, or too simple, and are prone to problems such as missiles falling off when the aircraft is maneuvering under overload; and now the pylons are only designed for stand-alone aircraft The design has almost zero versatility, which is not good for the development of aircraft model business

Method used

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  • A modified missile pylon for fixed-wing aircraft model
  • A modified missile pylon for fixed-wing aircraft model
  • A modified missile pylon for fixed-wing aircraft model

Examples

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Embodiment Construction

[0013] Such as Figure 1 to Figure 5 As shown, a modified missile pylon for a fixed-wing aircraft model includes modified missile 1, fixing bolt 2, pylon shell 3, electronic pulse igniter 4, glow tube 5, fuse 6, driving steering gear 7, steering gear shaking The arm 8, the slider 9, the first link 10, the second link 11, the claw link 12, the hexagon nut 13, the movable claw 14, the pin 15, the small spring 16, are characterized in that: the drive The steering gear 7 is fixedly installed in the mounting seat inside the pylon shell 3, the steering gear rocker arm 8 is fixedly installed on the output shaft of the driving steering gear 7, and the rectangular box of the slider 9 is slidably mounted on the steering gear rocker arm 8. , The protruding shaft of the slider 9 is rolling mounted in the upper shaft hole of the first connecting rod 10, and the upper shaft hole ends of the two second connecting rods 11 are connected to the lower shaft hole of the first connecting rod 10 thr...

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Abstract

The invention discloses a hanging rack used for modified missiles of a fixed wing model airplane. The hanging rack mainly comprises an installation frame assembly, a missile fixing jaw assembly, a connection rod drive mechanism and an electronic pulse ignition mechanism. The hanging rack is suitable for the usage of a large turbine spray / electric fixed wing simulation machine; the mechanisms are simple and effective in design; the simulation of real missile fixing components can be achieved in form, and holding is stable when an aircraft flies. The usage of the model modified missiles with different calibers in a certain range can be achieved through an elastic movable jaw mechanism; immediate ignition can be achieved through the electronic ignition mechanism, and effective launch of the modified missiles is archived, so that a foundation is laid for the model airplane to achieve wonderful fight performances and smoke writing performances.

Description

Technical field [0001] The invention provides a pylon for modified missiles, in particular a pylon for modified missiles of fixed-wing aircraft models, and belongs to the technical field of pylons for modified missiles of aircraft models. Background technique [0002] At the 2015 World Turbojet Airplane Exchange Conference, a variety of real aircraft models were dazzling. The wonderful flight performances, simulated missile launch performances and smoke pulling performances of the model airplanes at the opening and closing ceremonies made the audience clapped and praised. Then, when modifying the design of the pylons of the missiles and the smoke pipes, the existing ones are either too complicated and expensive to build, or too simple, which are prone to problems such as the missile falling when the aircraft is maneuvering under overload; and the current pylon design is only for single aircraft. Design, versatility is almost zero, which is detrimental to the development of model...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D7/04
Inventor 邢永安
Owner 启东市机关液化气有限责任公司
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