Connection sealing structure for nozzle assembly of solid rocket engine
An engine nozzle, solid rocket technology, applied in rocket engine devices, machines/engines, mechanical equipment, etc., can solve the problems of temperature shock resistance, limited structure space, high impact, high connection strength, simple processing technology, The effect of high connection reliability
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0016] figure 1 Among them, the present invention includes a nozzle housing 1, a sealant 2 for sealing the connection gap, a retaining ring 3 for connection and fixing, and a nozzle expansion section 4 for limiting the throat liner and converting energy. The stop ring 3 is placed in the concave annular installation groove and the limit groove corresponding to the nozzle expansion section 4, the sealant 2 is basically evenly applied on the corresponding surface of the nozzle expansion section 4, and then the stop ring 3 and The corresponding thread of the nozzle housing 1 enables the nozzle expansion section 4 to be firmly connected to the rear section of the nozzle housing 1, and enables the sealant 2 applied on the nozzle expansion section 4 to be evenly distributed on the corresponding curved surface , to fill up the corresponding curved surfaces of the nozzle housing 1 and the nozzle expansion section 4 that need to be sealed. During the installation and docking process of...
PUM
Abstract
Description
Claims
Application Information
- R&D Engineer
- R&D Manager
- IP Professional
- Industry Leading Data Capabilities
- Powerful AI technology
- Patent DNA Extraction
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.
© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com