Isochoric heat addition engines and methods

1. A method of adjustably reducing by a percentage in power output of an internal combustion rotary engine, the internal combustion rotary engine comprising:

a housing having an intake port, a recess that forms a part of a combustion chamber, and an exhaust port, wherein the intake port and the exhaust port are adjacent to one another within the housing and located so that both the intake and exhaust ports are closer to the combustion chamber on one side of the housing than another side;

a fuel injector configured to inject fuel into the recess, the fuel injector mounted in the housing;

a rotor having a lobe, the rotor being rotatably mounted in the housing and coupled to a shaft;

two gates, each gate movably mounted with respect to the housing on opposing sides of the recess, so that each gate is engaged at least periodically with the rotor, wherein during engagement of at least one of the two gates with the rotor a volume is maintained between a surface of the at least one gate, the rotor, and the housing, the volume undergoing changes in accordance with the cycle during rotation of the rotor; and

a controller configured to control the fuel injector,

the method comprising:

reducing the volume from a first quantity to a second quantity in a compression phase of the cycle so as to compress air disposed therein;

holding the volume constant at the second quantity after the compression phase and during a combustion phase of the cycle by engaging the two gates against the rotor so as to form the combustion chamber;

injecting fuel into the combustion chamber by the fuel injector, wherein reduction in volume of air during the compression phase of the cycle in combination with the introduction of fuel are sufficient to cause spontaneous combustion of the fuel;

controlling the fuel injector to inject the same amount of fuel each time fuel is injected or to withhold introduction of fuel during a percentage of cycles, so that fuel is introduced only over a sufficient number of cycles per unit of time in order to produce a reduction by the percentage, in the power output of the engine; and

increasing the volume of gases in an expansion phase of the cycle to a third quantity that is larger than the first quantity, by disengaging one of the two gates from contact with the rotor and the other one of the two gates remains engaged with the rotor until a completion of the expansion phase, while expanding gases from combustion apply a torque to the rotor relative to the housing so as to cause the rotor, and therefore the shaft, to rotate,

wherein the intake port and the exhaust port are located within the housing so that angular displacement, of the rotor lobe in operation of the engine in the compression phase of the cycle, between a first position when the rotor lobe is close to the intake port and a second position when the rotor lobe is close to the recess so as to form the combustion chamber is substantially less than angular displacement of the rotor lobe in operation of the engine in the expansion phase of the cycle, between the second position and a third position when the rotor lobe is close to the exhaust port, and

for each cycle that withholds the introduction of fuel, supplying heat by heat transfer from (i) walls of the engine directly, (ii) a heat exchanger, or both, during a phase of such cycle when combustion would occur if introduction of fuel had not been withheld and during the expansion phase of such cycle.

2. An internal combustion rotary engine comprising:

a. a housing having an intake port, a recess that forms a part of a combustion chamber during a combustion phase of a cycle of the engine, a fuel injector mounted therein and configured to inject fuel into the recess, and an exhaust port, wherein the intake port and the exhaust port are adjacent to one another within the housing and located so that both the intake and exhaust ports are closer to the combustion chamber on one side of the housing than another side;

b. a rotor having a lobe, the rotor being rotatably mounted in the housing and coupled to a shaft;

c. two gates, each gate movably mounted with respect to the housing on opposing sides of the recess, so that each gate is engaged at least periodically with the rotor, wherein during engagement of at least one of the two gates with the rotor a volume is maintained between a surface of the at least one gate, the rotor, and the housing, the volume undergoing changes in accordance with the cycle during rotation of the rotor; and

d. a controller configured to control the fuel injector,

wherein:

in a compression phase of the cycle, the volume is reduced from a first quantity to a second quantity so as to compress air disposed therein,

in the combustion phase of the cycle, the two gates are configured to engage against the rotor such that the volume is held constant at the second quantity after compression and during combustion, so as to form the combustion chamber, and fuel is introduced into the combustion chamber by the fuel injector, wherein reduction in volume of air during the compression phase of the cycle in combination with the introduction of fuel are sufficient to cause spontaneous combustion of the fuel,

in an expansion phase of the cycle, one of the two gates is configured to disengage from contact with the rotor such that the volume of gases from combustion is increased to a third quantity that is larger than the first quantity, while expanding gases from combustion apply a torque to the rotor relative to the housing so as to cause the rotor, and therefore the shaft, to rotate, and the other one of the two gates is configured to remain engaged with the rotor until the completion of the expansion phase of the cycle, and

the intake port and the exhaust port are located within the housing so that angular displacement, of the rotor lobe in operation of the engine in the compression phase of the cycle, between a first position when the rotor lobe is close to the intake port and a second position when the rotor lobe is close to the recess so as to form the combustion chamber is substantially less than angular displacement of the rotor lobe in operation of the engine in the expansion phase of the cycle, between the second position and a third position when the rotor lobe is close to the exhaust port.

3. An internal combustion rotary engine according to claim 1 , wherein the gates are slidably mounted with respect to the housing.

4. An internal combustion rotary engine according to claim 1 , wherein the gates are pivotally mounted with respect to the housing.

5. An internal combustion rotary engine according to claim 4 , wherein the pivotally mounted gates form an external wall of the housing.

6. An internal combustion rotary engine according to claim 1 , further comprising two cams coupled to the gates, the cams rotated by a drive system synchronized with the rotation of the rotor.

7. An internal combustion rotary engine of claim 1 , further comprising:

a seal assembly that seals the rotor in relation to the housing, the rotor having an edge and a face, the seal assembly comprising:

a groove formed in the face of the rotor, proximate to the edge and having a radially inward wall and a radially outward wall, the groove having a bevel located in the radially outward wall; and

a sealing strip disposed in the groove and having, in contact with the groove, a conformal surface;

wherein the strip is engaged in frictional contact against the housing, the housing presenting to the sealing strip a substantially flat surface, the frictional contact tending to cause the strip to rotate slightly with respect to the rotor and to move slightly axially in a direction out of the groove, so as to reduce any gap between the strip and the housing and so as to increase sealing between the rotor and the housing.

8. An internal combustion rotary engine of claim 1 , wherein the engine is configured to operate as an internal combustion engine of the homogenous charge compression ignition type, causing combustion of a fuel-air mixture when a state of the mixture is transformed from subcritical to critical, the engine further comprising:

a catalytic surface carried on a mechanical substrate, the surface being normally concealed from the mixture; and

a trigger for initiating combustion by causing the catalytic surface to be exposed to the mixture when the mixture is placed under minimum volume conditions.

9. An internal combustion rotary engine of claim 8 , wherein the catalytic surface is placed directly on the rotor of the engine, and configured in such a manner that it is exposed each time the rotor reaches a specific angular extent in the cycle.

10. An internal combustion rotary engine of claim 8 , wherein the catalytic surface is placed in a location of the housing of the engine, and configured in such a manner that it is exposed each time the rotor reaches a specific angular extent in the cycle.

11. An internal combustion rotary engine according to claim 1 , further comprising a separator gate between the intake port and the exhaust port, the separator gate movably mounted with respect to the housing and configured to engage with the rotor.