180 results about "Opposed-piston engine" patented technology

A combustion chamber for an internal combustion engine is disclosed in which the piston has a large squish region at a peripheral location on the piston top and a depression in the center of the piston top. A side injector sprays fuel into the depression in the piston top through a channel defined in the squish region. In some embodiments, two injectors are provided that are diametrically opposed to each other. In some embodiments, the engine is an opposed-piston engine in which each piston has the squish regions and depressions in the piston top.

In an air handling system of a uniflow-scavenged, two-stroke cycle opposed-piston engine, repeatable trapped mass and composition are achieved by determining provision of air handling setpoints that control operation of the engine's air handling system components. In some aspects, these setpoints govern operations of the air handling system by actively controlling the intake manifold pressure (IMP), EGR flow, and exhaust channel backpressure.

In an opposed piston engine, a pair of pistons are disposed in opposition in the bore of a cylinder. The cylinder includes first liquid coolant grooves having a first cooling capacity to cool a portion of the cylinder extending from a central portion toward an exhaust port, and second liquid coolant grooves having a second cooling capacity, less than the first cooling capacity, to cool a portion of the cylinder extending from the central portion toward an inlet port. Each piston includes a cylindrical skirt with a crown and an open end opposite the crown, a piston rod with a bore, a first end attached to a back surface of the crown, and a second end extending through the open end of the skirt, a radial array of liquid coolant flow passages in communication with the bore and disposed between the first end and the back surface of the crown, and a single wristpin retained on the second end section of the piston rod and positioned externally to the piston.

A combustion chamber for an opposed-piston engine includes a squish zone defined between circumferential peripheral areas of opposing end surfaces of the pistons, a cavity defined by one or more bowls in the end surfaces, and at least one injection port that extends radially through the squish zone into the cavity. The cavity has a cross-sectional shape that imposes a tumbling motion on air flowing from the squish zone into the cavity.

Load transfer point offset of rocking journal bearings in uniflow-scavenged, opposed-piston engines with phased crankshafts includes differing offsets for the load transfer points of opposed pistons. More specifically, under the condition that a first crankshaft leads the second crankshaft, an angular offset of a rocking journal wristpin of a piston coupled to the first crankshaft proportional to an offset of the first crankshaft relative to the second crankshaft is made to ensure adequate oil film thickness to the wristpin when it experiences a peak combustion pressure during a power stroke

A four-stroke opposed piston engine includes a rotating cylinder with a circumference and an aperture defined through the circumference, first and second opposing pistons, optional first and second opposing cylindrical spacers, first and second opposing piston caps, a spark rod that bisects the cylinder with insulating elements, and a pair of opposing gears.

The invention discloses a shaft type connecting rod transmission system and an opposed piston engine; and a traditional reciprocating linear motion is converted to a rotating motion in the same direction, so that the reliability of the transmission system is effectively improved, the transmission system is simplified to become more compact, and effective utilization of a space between the back surface of a piston of an internal combustion engine and a cylinder becomes possible. The shaft type connecting rod transmission system comprises a main shaft and at least one linear reciprocating motion unit, wherein the linear reciprocating motion unit comprises at least one linear reciprocating motion body. The linear reciprocating motion bodies are fixedly connected with one ends of corresponding shaft type connecting rods; the other ends of the shaft type connecting rods are fixedly connected with one sides of corresponding push-pull frames; and the axles of the shaft type connecting rods and the main shaft are perpendicular to each other. Slip blocks are arranged in the push-pull frames; two transverse outer side walls of the slip blocks and two transverse inner side walls of the push-pull frames are formed to vertical slide fit; inner rings of the slip blocks have inner teeth with elliptic indexing circles; and the inner teeth are circularly engaged with gears correspondingly arranged on the main shaft. Reversing mechanisms are arranged between the main shaft and the slip blocks.

A combustion chamber for an opposed-piston engine has an elongated asymmetrical shape in longitudinal section that runs along a chamber centerline, between diametrically-opposed openings of the combustion chamber through which fuel is injected. The asymmetry apportions combustion chamber volume to provide additional clearance on a side of the chamber centerline toward which swirl is directed, thereby giving a fuel plume space to swing without hindrance in response to swirl.

Belonging to the field of internal-combustion engine, the invention in particular relates to an opposed-piston engine, comprising a cylinder, a working piston, a crank shaft and the like; wherein the cylinder is provided with an air piston which is opposite to the working piston and moves in opposite direction; the cylinder block face at one side of the air piston is provided with an intake valve and an outtake valve; the intake valve is communicated with the atmosphere, the air piston is provided with a mechanism which can enable the air piston to reset; the air outtake is connected with an air storage mechanism for storing high pressure gas by an oil-gas separating device; the middle part of the cylinder is provided with a combustion chamber which is provided with an air inlet, an air outlet, a fueling injection device and an ignition unit; the air inlet is connected with the gas storage mechanism by a first electromagnetic valve. With the opposed-piston engine adopted, oil fuel consumption and vibration can be reduced by big margins and motorcycles or single-cylinder automobiles with even smaller vibration than the vibration of 4-cylinder automobiles can be produced; in addition, the engine of the invention can serve as auxiliary power of hybrid vehicles.

The invention relates to an opposed piston engine comprising at least one cylinder, at least two pistons arranged to be reciprocated within the same cylinder in an opposed manner, at least one intake port through the cylinder wall, at least one exhaust port through the cylinder wall, at least one shaft arranged to be rotated by reciprocal motion of the opposed pistons, at least one reciprocatable sleeve valve within the cylinder for controlling porting of one or both of the at least one intake port and the at least one exhaust port, a sleeve valve driving mechanism for controlling reciprocal motion of the at least one sleeve valve, and a dwell mechanism. The dwell mechanism is configured to induce at least one period of dwell of the at least two pistons during their respective cycles of piston motion.

The present invention discloses an interference spray test device for an opposed piston engine. The device comprises a constant volume bomb system, an air intake and exhaust system, a fuel oil jettingsystem, a high-speed photographing system and a control and acquisition system; the constant volume bomb system is used for simulating the internal condition of a combustion chamber when opposed pistons are located at inner dead points so as to realize a fuel oil jetting, collision and atomization experiment; the air intake and exhaust system is used for providing corresponding jetting back pressure for the interior of the constant volume bomb of the constant volume bomb system and discharging oil mist exhaust gases in the process of the experiment; the fuel oil jetting system is used for establishing oil pressure meeting the requirements of the experiment and realizing fuel oil jetting; and the high-speed photographing system is used for capturing and recording spray structures in a spray field; and the control and acquisition system controls a spray direction, oil jetting pressure and a photographing process, realizes the photographing control of fuel oil jetting and atomization andobtains the process image of spray development, and completes the acquisition of test data. With the test device of the invention adopted, on the one hand, jetting back pressure in a cylinder can beeffectively simulated, and on the other hand, flexible adjustment of interference spray at different angles can be realized.

The centrally located ignition source in a combustion chamber is an electrical conductor spanning the general center of the combustion chamber, with a spark gap at the general center of the conductor. The device may be offset from the combustion chamber centerline, and/or the spark gap may be offset from the conductor center, as required. The centrally located ignition source is particularly well suited for use in an opposed piston engine having a rotary sleeve valve mechanism, with the conductor rotating with the sleeve valve and crossing the combustion chamber between the two pistons. An arcuate commutator section may be disposed upon the exterior of the rotary sleeve valve, with a contact finger making electrical contact between the electrical energy source and the commutator section to supply electrical energy to the ignition source. The device is also suitable for use in stationary installations, e.g., gas furnace combustors, etc.

An opposed-piston engine with a single crankshaft has a rocker-type linkage coupling the crankshaft to the pistons that utilizes a rotatable pivot rocker arm with full-contact plain bearings. A rocker-type linkage utilizes a rotatable pivot bearing with an eccentric aspect to vary translation of piston linkage along the axial direction of a cylinder, which shifts the top dead center (TDC) and bottom dead center (BDC) locations of a piston so as to change the volume of charge air compressed during the power stroke.

A combustion chamber for an opposed-piston engine has a rotationally skewed shape in a longitudinal section that is orthogonal to a chamber centerline, between diametrically-opposed openings of the combustion chamber through which fuel is injected. The rotationally skewed shape interacts with swirl to generate a tumble bulk charge air motion structure that increases turbulence.

An opposed-piston engine includes a ported cylinder and a pair of pistons disposed to reciprocate in the bore of the cylinder. A combustion chamber is defined by opposing shaped piston end surfaces as the pistons approach respective top dead center (TDC) locations in the bore. At the end of scavenging, the shaped end surfaces of the pistons interact with swirl to produce turbulence in the charge air motion in the combustion chamber; the additional bulk motions include tumble. Fuel is injected into the turbulent charge air motion along a major axis, of the combustion chamber.

A two-cycle, opposed piston engine with side-mounted crankshafts and cylinders isolated from mechanical stresses of the engine includes tailored cooling of cylinders and symmetrical cooling of the interior surfaces of piston crowns. Each opposed piston includes a compliant member that permits movement of an axially-centered rod mounted in the piston in order to maintain axial alignment with the bore of a cylinder in which the piston is disposed during engine operation. A single wristpin is disposed externally of the piston to connect the piston with connecting rods that run between the piston and the crankshafts.

An opposed-piston engine that forms an inviscid layer between pistons and the respective cylinder walls. In an aspect, the opposed-piston engine utilizes a Scotch yoke assembly that includes rigidly connected opposed combustion pistons. In an aspect, the Scotch yoke assembly is configured to transfer power from the combustion pistons to a crankshaft assembly. In an aspect, the crankshaft assembly can be configured to have dual flywheels that are internal to the engine, and can be configured to assist with an exhaust system, a detonation system, and/or a lubrication system.

The invention discloses a pneumatic opposed-piston engine which comprises internal combustion cylinders, pneumatic cylinders and a crankshaft, wherein two internal combustion pistons are arranged in one internal combustion cylinder in an opposed mode, pneumatic pistons are arranged in one pneumatic cylinder and connected with the internal combustion pistons, one internal combustion piston in the internal combustion cylinder is rotatablely connected with a rod journal of the crankshaft through a connecting rod, the other internal combustion piston is rotatablely connected with another rod journal of the crankshaft through another connecting rod, a phase difference exists between the two rod journals, a compressed gas inlet of the pneumatic cylinder is communicated with a gas inlet channel of an internal combustion engine of the internal combustion cylinder, and the displacement of one pneumatic cylinder or the displacement sum of all the pneumatic cylinders is greater than the displacement sum of all the internal combustion cylinders. The pneumatic opposed-piston engine disclosed by the invention is simple in structure and high in efficiency.

A cylinder for opposed-piston engines includes a liner with a bore and longitudinally displaced intake and exhaust ports near respective ends thereof. An intermediate portion of the liner between the exhaust and intake ports contains a combustion chamber formed when the end surfaces of a pair of pistons disposed in opposition in the bore are in close mutual proximity. A compression sleeve encircles and reinforces the intermediate portion of the liner. An annular grid of pegs disposed between the intermediate portion and the compression sleeve supports the compression sleeve against the liner and defines a turbulent liquid flow path extending across the intermediate portion in a direction that parallels the longitudinal axis of the liner.