Method for increasing combustion efficiency of boron powder

A technology of combustion efficiency and boron powder, which is applied in the field of improving the combustion efficiency of solid fuel boron powder used in missiles, can solve the problems of reducing boron content in propellants, reducing fuel combustion efficiency, and increasing fuel "dead weight" to achieve stable quality and high performance. Reliable, easy-to-operate results
CN101759508AInactive Publication Date: 2010-06-30TONGJI UNIV

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
TONGJI UNIV
Publication Date
2010-06-30
Estimated Expiration
Not applicable · inactive patent
Patent Text Reader

Abstract

The invention relates to a method for increasing the combustion efficiency of boron powder. The method comprises the following steps: firstly, weighing fluororubber and acetone by the mass ratio thereof being 1:(1-200); then, dissolving the fluororubber in the acetone to obtain fluororubber solution; next, adding boron powder to the fluororubber solution by the mass ratio between the boron powder and the fluororubber being 1:(0.01-0.5); stirring at 20 to 70 DEG C; and drying the obtained product at 20 to 100 DEG C for 1h to 20h after the acetone is fully evaporated to obtain the boron powder coated with fluororubber. The method of the invention has the advantages of simple process and convenient operation; the boron powder as a solid fuel prepared by the method of the invention has the advantages of stable quality and reliable performance; and the method can effectively increase the combustion efficiency of boron powder.
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Description

technical field

[0001] The invention relates to a method for improving the combustion efficiency of boron powder. Specifically, it is a method to improve the combustion efficiency of boron powder, a solid fuel used in missiles. Background technique

[0002] Tactical missiles are important weapons necessary for modern national defense, and their range, maneuverability, and supersonic travel performance depend on the solid fuel energy of the missile motor and propellant. Boron has long been the preferred solid fuel for missiles due to its high mass and volumetric energy density. However, boron oxide produced by boron combustion has the characteristics of low melting point and high boiling point. After boron oxide is generated, it will wrap on the surface of boron to prevent further reaction between air and boron, thus greatly reducing the combustion efficiency of boron.

[0003] At present, researchers mainly use inorganic and organic substances to coat boron powder to impro...

Claims

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