View source for 18132167. ROTOR ASSEMBLY WITH COOLING CHANNELS SEPARATED BY RIBS FOR A ROTARY ENGINE simplified abstract (Pratt & Whitney Canada Corp.)

=ROTOR ASSEMBLY WITH COOLING CHANNELS SEPARATED BY RIBS FOR A ROTARY ENGINE=


==Organization Name==

[[:Category:Pratt & Whitney Canada Corp.|Pratt & Whitney Canada Corp.]]


[[Category:Pratt & Whitney Canada Corp.]]

==Inventor(s)==

[[:Category:Jérémie Barberger of Montreal (CA)|Jérémie Barberger of Montreal (CA)]][[Category:Jérémie Barberger of Montreal (CA)]]

[[:Category:Michel Bousquet of Longueuil (CA)|Michel Bousquet of Longueuil (CA)]][[Category:Michel Bousquet of Longueuil (CA)]]

==ROTOR ASSEMBLY WITH COOLING CHANNELS SEPARATED BY RIBS FOR A ROTARY ENGINE - A simplified explanation of the abstract==


This abstract first appeared for US patent application 18132167 titled 'ROTOR ASSEMBLY WITH COOLING CHANNELS SEPARATED BY RIBS FOR A ROTARY ENGINE

The abstract describes a rotor housing for an aircraft rotary engine, consisting of a side housing body and a rail. The side housing body has a fluid cooling passage and a plurality of ribs, with the rail disposed at the ribs to form fluid cooling channels.

* The rotor housing includes a side housing body and a rail.
* The side housing body forms a fluid cooling passage and a plurality of ribs.
* The ribs are coincident with the fluid cooling passage and extend into it.
* The rail is disposed at the ribs to form fluid cooling channels.
* The fluid cooling channels are connected in fluid communication with the fluid cooling passage.

Potential Applications:
- Aircraft rotary engines
- Aerospace industry
- Cooling systems for high-performance engines

Problems Solved:
- Efficient cooling of rotary engines
- Improved heat dissipation
- Enhanced engine performance and longevity

Benefits:
- Increased engine efficiency
- Reduced risk of overheating
- Extended engine lifespan

Commercial Applications:
Title: Advanced Cooling Systems for Aircraft Rotary Engines
This technology can be utilized in the aerospace industry to enhance the performance and reliability of aircraft rotary engines. It can also be applied in other high-performance engine systems that require efficient cooling solutions.

Questions about the technology:
1. How does the rotor housing improve the cooling efficiency of aircraft rotary engines?
2. What are the potential cost savings associated with using this innovative cooling system?

Frequently Updated Research:
Stay updated on the latest advancements in aircraft engine cooling technology to ensure optimal performance and reliability in aerospace applications.


==Original Abstract Submitted==

A rotor housing for an aircraft rotary engine includes a side housing body and a rail. The side housing body extends along an axis between and to an inner side and an outer side. The side housing body forms a fluid cooling passage and a plurality of ribs. The fluid cooling passage extends about the axis at the inner side. The plurality of ribs are coincident with and extend into the fluid cooling passage. The plurality of ribs are distributed about the fluid cooling passage as an array of ribs. The rail is disposed at the plurality of ribs. The rail extends about the fluid cooling passage. The side housing body and the rail form a plurality of fluid cooling channels connected in fluid communication with the fluid cooling passage.



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