Side wall for rotary engine housing
US-11333068-B1 · May 17, 2022 · US
US12196154B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12196154-B2 |
| Application number | US-202318326102-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 31, 2023 |
| Priority date | May 31, 2023 |
| Publication date | Jan 14, 2025 |
| Grant date | Jan 14, 2025 |
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A housing assembly for a rotary engine, has: a rotor housing having an inner face facing a rotor cavity, a first side and a second side opposite to the first side; a first side housing secured to the first side, and a second side housing secured to the second side, the rotor cavity bounded axially between the first side housing and the second side housing; and a seal received within a groove at an interface between the rotor housing and the first side housing, the groove located outwardly of the inner face and overlapping a peripheral section of the first side housing, the seal having: an elastomeric member compressed between the peripheral section and the rotor housing; and a metallic member disposed inwardly of the elastomeric member, the metallic member in contact with both of the peripheral section of the first side housing and the rotor housing.
Opening claim text (preview).
The invention claimed is: 1. A housing assembly for a rotary internal combustion engine, comprising: a rotor housing extending around an axis, the rotor housing having an inner face facing a rotor cavity, a first side and a second side opposite to the first side; a first side housing secured to the first side of the rotor housing, and a second side housing secured to the second side of the rotor housing, the rotor cavity bounded axially between the first side housing and the second side housing, the first side housing including a side wall secured to the rotor housing and a side plate, a peripheral section of the side plate disposed between the side wall and the rotor housing; and a seal received within a groove at an interface between the rotor housing and the first side housing, the groove annularly extending around the axis, located outwardly of the inner face of the rotor housing, and overlapping a peripheral section of the first side housing, the seal having: an elastomeric member compressed between the peripheral section of the first side housing and the rotor housing; and a metallic member disposed inwardly of the elastomeric member relative to the axis, the metallic member in contact with both of the peripheral section of the first side housing and the rotor housing, a stiffness of the metallic member is such that a pressure force generated by the metallic member on the side plate is at most 150 pounds by inch of length of the metallic member when the rotary internal combustion engine is non-operating. 2. The housing assembly of claim 1 , wherein a gap is defined between the rotor housing and the peripheral section of the side plate, the groove communicating with the rotor cavity through the gap. 3. The housing assembly of claim 1 , wherein a cross-section of the metallic member includes at least two crests and a valley located between the at least two crests, the metallic member being compressible in a direction parallel to the axis. 4. The housing assembly of claim 3 , wherein a cross-section of the metallic member has an E-shape. 5. The housing assembly of claim 1 , wherein the pressure force is at least 25 pounds by inch. 6. The housing assembly of claim 1 , wherein the metallic member is made of a material having a melting point above a temperature of combustion gases inside the rotor cavity. 7. The housing assembly of claim 1 , comprising a coolant circuit within the rotor housing, the first side housing, and the second side housing, the seal fluidly separating the coolant circuit from the rotor cavity. 8. A rotary internal combustion engine comprising: a rotor; a rotor housing extending around an axis, the rotor housing having an inner face facing a rotor cavity containing the rotor, a first side and a second side opposite to the first side; a first side housing secured to the first side of the rotor housing, a second side housing secured to the second side of the rotor housing, the rotor located axially between the first side housing and the second side housing, and circumscribed by the rotor housing, the first side housing including a side wall secured to the rotor housing and a side plate, a peripheral section of the side plate disposed between the side wall and the rotor housing; and a seal received within a groove at an interface between the first side housing and the rotor housing, the groove annularly extending around the axis, located outwardly of the inner face of the rotor housing, and overlapping a peripheral section of the first side housing, the seal having: an elastomeric member compressed between the peripheral section of the first side housing and the rotor housing; and a metallic member in contact with both of the peripheral section of the first side housing and the rotor housing, the metallic member located radially between the inner face of the rotor housing and the elastomeric member, the metallic member configured for generating a pressure force on the side plate is at most 150 pounds by inch of length of the metallic member when the rotary internal combustion engine is non-operating. 9. The rotary internal combustion engine of claim 8 , wherein a gap is defined between the rotor housing and the peripheral section of the side plate, the groove communicating with the rotor cavity through the gap. 10. The rotary internal combustion engine of claim 8 , wherein a cross-section of the metallic member includes at least two crests and a valley located between the at least two crests, the metallic member being compressible in a direction parallel to the axis. 11. The rotary internal combustion engine of claim 8 , wherein a cross-section of the metallic member has an E-shape. 12. The rotary internal combustion engine of claim 8 , wherein the pressure force is at least 25 pounds by inch. 13. The rotary internal combustion engine of claim 8 , wherein the metallic member is made of a material having a melting point above a temperature of combustion gases inside the rotor cavity. 14. The rotary internal combustion engine of claim 8 , comprising a coolant circuit within the rotor housing, the first side housing, and the second side housing, the seal fluidly separating the coolant circuit from the rotor cavity. 15. A method of sealing a rotary internal combustion engine having a rotor cavity bounded by a rotor housing and a side housing, the method comprising: mitigating leakage of combustion gases out of the rotor cavity with an elastomeric member at an interface between the rotor housing and a side plate mounted to a side wall of the side housing; and protecting the elastomeric member from the combustion gases while permitting thermal growth of the side plate relative to the side wall with a metallic member disposed between the elastomeric member and the rotor cavity, the metallic member configured for generating a pressure force on the side plate of at most 150 pounds by inch of length of the metallic member when the rotary internal combustion engine is non-operating. 16. The method of claim 15 , wherein the protecting of the elastomeric member from the combustion gases with the metallic member includes compressing an E-seal between the rotor housing and the side housing, a cross-sectional area of the E-seal having a “E” shape.
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