Abstract: A seal assembly between first and second passages of an engine block and a gear box assembly of a reciprocating engine. The seal assembly includes a conduit having a first end portion disposed inside of the first fluid passage and a second end portion disposed outside of the first fluid passage in fluid communication with the second passage of the gear box assembly. The seal assembly includes a collar disposed about the second end portion of the conduit, and a radial sealing interface disposed between an outer conduit surface of the conduit and an inner collar surface of the collar, wherein the radial sealing interface supports a first radial seal. The seal assembly includes an axial sealing interface disposed between an axial face of the collar and an opposing axial face of the gear box assembly, wherein the axial sealing interface supports a face seal.

Abstract: A seal assembly between first and second passages of an engine block and a gear box assembly of a reciprocating engine. The seal assembly includes a conduit having a first end portion disposed inside of the first fluid passage and a second end portion disposed outside of the first fluid passage in fluid communication with the second passage of the gear box assembly. The seal assembly includes a collar disposed about the second end portion of the conduit, and a radial sealing interface disposed between an outer conduit surface of the conduit and an inner collar surface of the collar, wherein the radial sealing interface supports a first radial seal. The seal assembly includes an axial sealing interface disposed between an axial face of the collar and an opposing axial face of the gear box assembly, wherein the axial sealing interface supports a face seal.

Abstract: A thermally compensated bore guide system for a shaft, the shaft configured to translate along a longitudinal axis, is provided. The thermally compensated bore guide system includes an inner bore defined within a component. The inner bore is configured to circumferentially surround at least a portion of the shaft, wherein the inner bore is non-linear in response to the thermally compensated bore guide system being at a first thermal condition and wherein the inner bore is configured to be linear and to define a bore axis substantially aligned with the longitudinal axis in response to the thermally compensated bore guide system being at a second thermal condition.

Abstract: A thermally compensated bore guide system for a shaft, the shaft configured to translate along a longitudinal axis, is provided. The thermally compensated bore guide system includes an inner bore defined within a component. The inner bore is configured to circumferentially surround at least a portion of the shaft, wherein the inner bore is non-linear in response to the thermally compensated bore guide system being at a first thermal condition and wherein the inner bore is configured to be linear and to define a bore axis substantially aligned with the longitudinal axis in response to the thermally compensated bore guide system being at a second thermal condition.

Abstract: Aspects of the disclosure include a system for controlling an exhaust gas communicated from an engine system to a turbine component of a turbocharger system. The system can include an engine having an operational speed; a turbocharger system including a turbine component, the exhaust gas being output from the engine in an exhaust line; a controller in communication with the engine; and a sensor disposed in the exhaust line being in communication with the controller, the system operating according to the following method: measuring the first temperature of the exhaust gas, determining if the measured first temperature of the exhaust gas is within a temperature safety window of the system; calculating an engine speed of the engine; and adjusting an engine speed setpoint and speed of the engine based on the measured first temperature and the calculated engine speed.

Abstract: Aspects of the disclosure include a system for controlling an exhaust gas communicated from an engine system to a turbine component of a turbocharger system. The system can include a sensor configured to determine a temperature of the exhaust gas; and a controller configured to adjust an engine system speed based on the temperature of the exhaust gas being greater than or less than a temperature safety window.

Abstract: A connecting rod includes an elongate rod shank with a small end at a first axial end of the rod shank and a big end at the second axial end of the rod shank. The big end includes a body part and a cap part adapted to releasably couple to the body part. When the cap part is coupled to the body part, the cap part and body part cooperate to define a crank pin receiving bore and abut at first and second spaced apart interfaces. The cap part defines an aperture proximate the first interface that is adapted to receive a threaded fastener that engages and clamps the cap part to the body part. The cap part includes a side portion that extends radially beyond a largest radius from a crank pin bore center to the first interface. The side portion is substantially radially concentrated adjacent the first interface.

Abstract: A connecting rod includes an elongate rod shank with a small end at a first axial end of the rod shank and a big end at the second axial end of the rod shank. The big end includes a body part and a cap part adapted to releasably couple to the body part. When the cap part is coupled to the body part, the cap part and body part cooperate to define a crank pin receiving bore and abut at first and second spaced apart interfaces. The cap part defines an aperture proximate the first interface that is adapted to receive a threaded fastener that engages and clamps the cap part to the body part. The cap part includes a side portion that extends radially beyond a largest radius from a crank pin bore center to the first interface. The side portion is substantially radially concentrated adjacent the first interface.

Abstract: In an engine having a rocker member adapted to rock about an axis intermediate the rocker member and a pushrod extending from a lower body to an upper body and engaging an end of the rocker member, a gasket for sealing the lower body to the upper body is provided. The gasket includes a sealing portion adapted to substantially seal at least a portion of the upper body to the lower body, and a pushrod support portion extending outwardly from the sealing portion adapted to engage the pushrod. At least a portion of the pushrod support portion engaging the pushrod is constructed from a material that is softer than the material of the pushrod.