Boundary compression engine
An engine and interface technology, applied in engine components, combustion engines, machines/engines, etc., can solve problems such as limiting the practical application value of engines, increasing engine manufacturing costs, and complex engine structures, and improving thermal power conversion efficiency and manufacturing costs. Low, the effect of improving load response characteristics
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0045] Such as figure 1 The interface compression engine shown includes a working medium envelope space 1, a piston 2, an intake valve 3 and an exhaust valve 4, and the working medium envelope space 1 includes at least the piston cylinder liner matching area 5, the combustion area 6 and the high-pressure gas compressor In the three areas of zone 7, a high-pressure gas inlet 8 is provided on the outer wall of the high-pressure gas compression zone 7, and the high-pressure gas inlet 8 is connected with the high-pressure gas source 10 through the compressed gas control valve 9, and the pressure of the high-pressure gas in the high-pressure gas source 10 is greater than that of the engine. The pressure of the fresh air in the enveloping space 1 of the working medium when inflation is completed. The high-pressure gas source 10 is set as a sealed high-pressure gas storage tank 1000, and the compressed gas control valve 9 is controlled so that the compressed gas control valve 9 is op...
Embodiment 2
[0048] Such as figure 2 The interface compression engine shown differs from Embodiment 1 in that the high-pressure gas in the high-pressure gas source 10 is engine exhaust. Fuel nozzles 13 are provided on the combustion zone 6 . The combustion zone 6 is far away from the piston 2, and the high-pressure gas compression zone 7 is located between the combustion zone 6 and the matching zone 5 of the piston and cylinder liner.
[0049] In this embodiment, the fresh air inhaled during the suction stroke is fresh air. Similarly, since the sum of the volumes of the combustion zone 6 and the high-pressure gas pressure zone 7 is set relatively large relative to the ratio of the piston cylinder liner matching zone 5, if only the compression of the piston 2 is used in the compression stroke, even when the piston 2 is at the upper stop At this point, the compressed fresh air cannot reach the pressure required for the ensuing combustible mixture to start explosive combustion. In order t...
Embodiment 3
[0051] Such as image 3 The difference between the shown interface compression engine and Embodiment 2 is that the pressure of the high-pressure gas in the high-pressure gas source 10 is greater than the pressure required to compress the fresh charge in the working medium envelope space 1 to the compression ratio set by the engine. The high-pressure gas in the high-pressure gas source 10 is the working medium of the engine. The intake valve 3 communicates with the pressurized fresh air source 12 through the control valve 90 . The combustion zone 6 is close to the piston 2, and the combustion zone 6 is located between the gas pressure zone 7 and the piston cylinder liner matching zone 5.
[0052] Since the intake valve 3 communicates with the fresh charge source 12 through the control valve 90, the intake and compression strokes can be omitted. At the end of the exhaust stroke, the intake valve 3 and the control valve 90 are opened, and the fresh air in the fresh charge source...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More - R&D
- Intellectual Property
- Life Sciences
- Materials
- Tech Scout
- Unparalleled Data Quality
- Higher Quality Content
- 60% Fewer Hallucinations
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.
© 2025 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com
