
基本信息:
- 专利标题: 一种连续型固体微推进器
- 专利标题(英):Continuous solid micro thruster
- 申请号:CN201710233857.1 申请日:2017-04-11
- 公开(公告)号:CN106968836A 公开(公告)日:2017-07-21
- 发明人: 李国中 , 赵海龙 , 马增帅 , 栗夫园 , 李平
- 申请人: 北京机械设备研究所
- 申请人地址: 北京市海淀区永定路50号
- 专利权人: 北京机械设备研究所
- 当前专利权人: 北京机械设备研究所
- 当前专利权人地址: 北京市海淀区永定路50号
- 代理机构: 北京天达知识产权代理事务所
- 代理人: 王涛; 王一
- 主分类号: F02K9/24
- IPC分类号: F02K9/24 ; F02K9/32
The invention provides a continuous solid micro thruster. The continuous solid micro thruster comprises an encapsulation conduit (1), a curved conduit (2), a plurality of micro propulsion units (3), a spray pipe (4), a supplemental unit and a propulsion unit. The encapsulation conduit (1) is of cuboid shell structure, a hollow cavity (8) is formed in the encapsulation conduit (1), the top of the encapsulation conduit (1) is sealed, the bottom of the encapsulation conduit (1) is opened, and a trough groove (7) penetrating through both sides wall is formed in the bottom of the encapsulation conduit (1); the spray pipe (4) is installed on the encapsulation conduit (1) in a butt joint mode; the micro propulsion units (3) are located in the hollow cavity (8) of the encapsulation conduit (1), the supplemental unit is arranged on the top of the encapsulation conduit (1), and the supplemental unit is compressible; the curved conduit (2) and the propulsion unit are correspondingly arranged on the two sides of the trough groove (7) of the encapsulation conduit (1). According to the continuous solid micro thruster, the single-point repeated propelling function can be achieved, the reaction is rapid, the thrust is large and reliability is high.
公开/授权文献:
- CN106968836B 一种连续型固体微推进器 公开/授权日:2018-04-20
IPC结构图谱:
F | 机械工程;照明;加热;武器;爆破 |
--F02 | 燃烧发动机;热气或燃烧生成物的发动机装置 |
----F02K | 喷气推进装置 |
------F02K9/00 | 火箭发动机装置,即带有燃料及其氧化剂的发动机;其控制 |
--------F02K9/08 | .使用固体推进剂 |
----------F02K9/24 | ..用固体推进剂对火箭发动机的装载;专门适用于固体推进剂药柱工作的方法或装置 |