High-speed high-temperature efficient fuel pump for aerospace
A technology for aerospace and fuel pumps, applied in pumps, pump components, rotary piston pumps, etc., can solve problems such as increased contact stress of gears, loss of liquid heating power, and inability to discharge to the outlet, and achieves improved meshing transmission efficiency, The effect of reducing volumetric efficiency loss and suppressing flow pulsation
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0028] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.
[0029] In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer" etc. The indicated orientation or positional relationship is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the referred device or element must have a specific orientation, or in a specific orientation. construction and operation, and therefore cannot be constru...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 


