Composite 27-hole magazine applied to aviation
The invention relates to a composite 27-hole magazine applied to aviation. An existing aviation magazine is generally prepared through slotting machine processing of an aluminum alloy forge blank andis subject to defects in too many complicated processes, a high weight and high cost, easy occurrence...
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| creator | YANG MANWEI ZHANG ZHENXING YU DALONG HE WENWEN YOU QIUMEI WANG JINWEI HU XINJIAN WANG HAIYUN JIAO ZIWEN XUE JING |
| description | The invention relates to a composite 27-hole magazine applied to aviation. An existing aviation magazine is generally prepared through slotting machine processing of an aluminum alloy forge blank andis subject to defects in too many complicated processes, a high weight and high cost, easy occurrence of local deformation of parts and the like. Aiming at the defects, the invention provides the composite 27-hole magazine applied to aviation. A square box shaped structure with an interval grid frame which is prepared through layering design of a carbon fiber composite material and overall solidification and shaping is used. The magazine comprises a top plate, a magazine rectangular hole, an installation hole, a front enclosing groove cavity, a front enclosing plate, a baseplate, a lateral trapezoid groove cavity, side plates, a lateral rectangular groove cavity and the like. A carbon fiber pre-preg is paved by layers according to design through use of a mold; and direct layering on the professional shaping mold, |
| format | Patent |
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An existing aviation magazine is generally prepared through slotting machine processing of an aluminum alloy forge blank andis subject to defects in too many complicated processes, a high weight and high cost, easy occurrence of local deformation of parts and the like. Aiming at the defects, the invention provides the composite 27-hole magazine applied to aviation. A square box shaped structure with an interval grid frame which is prepared through layering design of a carbon fiber composite material and overall solidification and shaping is used. The magazine comprises a top plate, a magazine rectangular hole, an installation hole, a front enclosing groove cavity, a front enclosing plate, a baseplate, a lateral trapezoid groove cavity, side plates, a lateral rectangular groove cavity and the like. 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An existing aviation magazine is generally prepared through slotting machine processing of an aluminum alloy forge blank andis subject to defects in too many complicated processes, a high weight and high cost, easy occurrence of local deformation of parts and the like. Aiming at the defects, the invention provides the composite 27-hole magazine applied to aviation. A square box shaped structure with an interval grid frame which is prepared through layering design of a carbon fiber composite material and overall solidification and shaping is used. The magazine comprises a top plate, a magazine rectangular hole, an installation hole, a front enclosing groove cavity, a front enclosing plate, a baseplate, a lateral trapezoid groove cavity, side plates, a lateral rectangular groove cavity and the like. 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| language | chi ; eng |
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| subjects | BLASTING FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS ANDORDNANCE, e.g. CANNONS HEATING LIGHTING MECHANICAL ENGINEERING MOUNTINGS FOR SMALLARMS OR ORDNANCE WEAPONS |
| title | Composite 27-hole magazine applied to aviation |
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