Apex and face seals with rotary internal combustion engine

Patent metadata

Field	Value
Publication number	US-9850758-B2
Application number	US-201514606182-A
Country	US
Kind code	B2
Filing date	Jan 27, 2015
Priority date	Jul 28, 2011
Publication date	Dec 26, 2017
Grant date	Dec 26, 2017

Abstract

A rotor for a rotary internal combustion engine with a first face seal biased axially outwardly away from the first end face has opposed curled ends abutting a first end seal of a respective one of the adjacent apex portions, and a second face seal biased axially outwardly away from the second end face has opposed curled ends abutting a second end seal of a respective one of the adjacent apex portions. A rotary internal combustion engine and a method of sealing chambers of a Wankel engine are also discussed.

First claim

The invention claimed is:

1. A rotor for a rotary internal combustion engine comprising:
a body having first and second axially spaced apart end faces, and a peripheral face extending between the end faces and defining at least three circumferentially spaced apex portions, the first and second end faces each having a groove defined therein between each of the apex portions and each adjacent one of the apex portions, the grooves of the first and second end faces being disposed adjacent to and radially inwardly of the peripheral face of the rotor;
at each of the apex portions:
an apex seal protruding radially from the peripheral face of the body and being biased radially away therefrom, and
first and second end seals received in a corresponding recess defined in the first and second end face, respectively, the first end seal protruding axially from the first end face and being biased axially outwardly away therefrom, and the second end seal protruding axially from the second end face and being biased axially outwardly away therefrom, the apex seal having ends received in a radial slot defined in the first and second end seals;

a first face seal located in each groove of the first end face and extending between adjacent ones of the apex portions, each first face seal being biased axially outwardly away from the first end face, each first face seal having opposed curled ends each abutting the first end seal of a respective one of the adjacent apex portions; and
a second face seal located in each groove of the second end face and extending between adjacent ones of the apex portions, each second face seal being biased axially outwardly away from the second end face, each second face seal having opposed curled ends each abutting the second end seal of a respective one of the adjacent apex portions.

2. The rotor as defined in claim 1 , wherein for each of the apex portions, the apex seal includes first and second apex seal elements protruding radially from the peripheral face of the body and being biased radially away therefrom, the first apex seal element protruding axially from the first end face and biased axially outwardly away therefrom, the second apex seal element protruding axially from the second end face and biased axially outwardly away therefrom.

3. The rotor as defined in claim 1 , wherein the curled ends of the first and second face seals are curved radially outwardly.

4. The rotor as defined in claim 1 , wherein each of the curled ends abuts the respective end seal without contact between an extremity of the curled end and the respective one of the end seals.

5. The rotor as defined in claim 1 , wherein the apex seals are made of ceramic and the face seals are made of metal.

6. The rotor as defined in claim 1 , wherein the at least three circumferentially spaced apex portions include only three apex portions.

7. A rotary internal combustion engine comprising:
a stator body having an internal cavity defined by axially spaced apart end walls and an inner surface extending between the end walls, the cavity having an epitrochoid shape defining at least two lobes;
a rotor body having two axially spaced apart end faces each extending in proximity of a respective one of the end walls of the stator body, and a peripheral face extending between the end faces and defining a number of circumferentially spaced apex portions which is one more than a number of the lobes of the cavity, the rotor body being engaged to an eccentric shaft to rotate within the cavity with each of the apex portions remaining in proximity of the inner surface of the cavity;
at each of the apex portions:
an apex seal protruding radially from the peripheral face of the body and being radially biased against the inner surface of the cavity, and
first and second end seals received in a corresponding recess defined in the first and second end face, respectively, the first end seal being axially biased against the first end wall, and the second end seal being axially biased against the second end wall, the apex seal having ends received in a radial slot defined in the first and second end seals;

a first face seal extending from each of the apex portions to each adjacent one of the apex portions, each first face seal extending from the first end face adjacent to and radially inwardly of the peripheral face of the rotor and being axially biased against the first end wall, each first face seal having opposed curled ends each abutting the first end seal of a respective one of the apex portions; and
a second face seal extending from each of the apex portions to each adjacent one of the apex portions, each second face seal extending from the second end face adjacent to and radially inwardly of the peripheral face of the rotor and being axially biased against the second end wall, each second face seal having opposed curled ends each abutting the second end seal of a respective one of the apex portions.

8. The engine as defined in claim 7 , wherein for each of the apex portions, the apex seal includes first and second apex seal elements protruding radially from the peripheral face of the rotor body, the first and second apex seal elements being radially biased against the inner surface of the cavity, the first apex seal element being axially biased against the first end wall, and the second apex seal element being axially biased against the second end wall.

9. The engine as defined in claim 7 , wherein the curled ends of the first and second face seals are curved radially outwardly.

10. The engine as defined in claim 7 , wherein each of the curled ends abuts the respective end seal without contact between an extremity of the curled end and the respective one of the end seals.

11. The engine as defined in claim 7 , wherein the apex seals are made of ceramic and the face seals are made of metal.

12. The engine as defined in claim 7 , wherein the number of the circumferentially spaced apex portions is 3 and the number of the lobes of the cavity is 2.

13. A method of sealing chambers of a Wankel engine defined between a rotor cavity and a rotor thereof, the cavity having axially spaced apart first and second end walls and a peripheral wall extending between the end walls, and the rotor having two axially spaced apart first and second end faces and a peripheral face extending between the end faces and defining circumferentially spaced apex portions, the method comprising:
at each one of the apex portions, radially pushing at least a portion of an apex seal against the peripheral wall;
between each adjacent ones of the apex portions, axially pushing a first face seal extending from the first end face against the first end wall;
between each adjacent ones of the apex portions, axially pushing a second face seal extending from the second end face against the second end wall;
at each one of the apex portions, axially pushing a first end seal having a first slot receiving a first end of the apex seal and extending from the first end face against the first end wall, abutting a curled end of an adjacent one of the first face seals with the first end seal, and abutting a curled end of another adjacent one of the first face seals with the first end seal; and
at each one of the apex portions, axially pushing a second end seal having a second slot receiving a second end of the apex seal and extending from the second end face against the second end wall, abutting a curled end of an adjacent one of the second face seals with the end seal, and abutting a curled end of another adjacent one of the second face seals with the second end seal.

Assignees

• Pratt & Whitney Canada

Inventors

• Gekht Eugene
• Thomassin Jean
• Bolduc Sebastien
• Gagnon-Martin David

Classifications

• F01C21/08

  Rotary pistons (reciprocating pistons in general F16J) · CPC title

• F16J15/545

  submitted to unbalanced pressure in circumference; seals for oscillating actuator · CPC title

• F01C19/10

  Sealings for working fluids between radially and axially movable parts · CPC title

• F01C1/22 Primary

  of internal-axis type with equidirectional movement of co-operating members at the points of engagement, or with one of the co-operating members being stationary, the inner member having more teeth or tooth- equivalents than the outer member · CPC title

• F01C19/08

  Axially-movable sealings for working fluids · CPC title