Aero-engine ignition control system with monitoring device
An aero-engine and ignition control technology, which is applied in the direction of machines/engines, rocket engine devices, jet propulsion devices, etc., can solve problems such as increasing the probability of misfire, and achieve the effects of simple structure, improved reliability, and high device stability
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0013] In order to better understand the aero-engine ignition control system with a monitoring device according to the solution of the present invention, a preferred embodiment of the aero-engine ignition control system with a monitoring device of the present invention will be further elaborated below in conjunction with the accompanying drawings.
[0014] Such as figure 1 As shown, the aero-engine ignition control system with monitoring device provided by the present invention includes a first channel A and a second channel B provided in the electronic controller of the engine, and the first channel A and the second channel B are controlled and connected respectively. The connected first ignition relay a and the second ignition relay b realize the ignition power supply control to the ignition nozzle, and the aircraft engine interface control unit is also provided with a first backup ignition relay c and a second backup ignition relay d, wherein, The first channel A and the se...
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