Double-cavity fuel system suitable for diving flight of unmanned aerial vehicle and design method thereof
A fuel system and unmanned aerial vehicle technology, which is applied in the direction of unmanned aircraft, aircraft, fuel tanks of power plants, etc., can solve the problem of not being able to meet the normal fuel supply, achieve reliable fuel supply, and avoid yaw effects
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0056] The fuel system proposed in this embodiment that can adapt to the UAV's dive flight includes a soft fuel tank 1 , an oil pump 2 , an exhaust solenoid valve 3 , a one-way valve 4 and an oil-gas separator 5 . Wherein: the outlet of the soft oil tank communicates with the oil inlet at the upper end of the oil-gas separator through a pipeline; an oil pump 2 is connected to the pipeline. The oil outlet 9 at the lower end of the oil-gas separator is externally connected to the oil inlet of the engine through a pipeline; a check valve 4 is connected to the pipeline. The exhaust port 10 located at the upper end of the oil-gas separator communicates with the outside atmosphere through a pipeline; an exhaust solenoid valve 3 is connected to the pipeline.
[0057] The soft oil tank 1, the oil pump 2, the exhaust solenoid valve 3 and the one-way valve 4 are all prior art.
[0058] The oil-air separator 5 includes an oil-air separator 6 and a liquid level sensor 7 . The oil-gas 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