Abstract: The disclosure relates to the technical field of cabinet splicing and specifically relates to a quick-splicing structure and a cabinet. A quick-splicing structure for quick connection between two surfaces includes at least one group of slidably fitting components and a plurality of groups of locking components. The slidably fitting components include a first member and a second member that are slidably fitted and disposed on the two surfaces. The locking components include a first fastener and a second fastener that are fitted to be locked and respectively disposed on the two surfaces, and the plurality of groups of locking components and the slidably fitting components are arranged in an alternating manner in a locking direction. The disclosure further provides a cabinet including the quick-splicing structure. A plurality of the cabinets are connected horizontally and/or vertically through the quick-splicing structure.

Abstract: The disclosure relates to the technical field of cabinet splicing and specifically relates to a quick-splicing structure and a cabinet. A quick-splicing structure for quick connection between two surfaces includes at least one group of slidably fitting components and a plurality of groups of locking components. The slidably fitting components include a first member and a second member that are slidably fitted and disposed on the two surfaces. The locking components include a first fastener and a second fastener that are fitted to be locked and respectively disposed on the two surfaces, and the plurality of groups of locking components and the slidably fitting components are arranged in an alternating manner in a locking direction. The disclosure further provides a cabinet including the quick-splicing structure. A plurality of the cabinets are connected horizontally and/or vertically through the quick-splicing structure.

Abstract: The present invention belongs to the technical field of diesel engines, and particularly relates to an engine cooling system and a cooling method therefor. In the engine cooling system of the present invention, when an engine needs to be warmed up, a first valve is opened, a lower engine body water storage chamber is in communication with an upper engine body water storage chamber, and some of the cooling water directly flows into the lower engine body water storage chamber from the upper engine body water storage chamber. The flow of the cooling water entering an engine body is reduced, and under the condition that heat dissipated by the engine is unchanged, the temperature rise of the cooling water flowing through the engine body such as a cylinder sleeve upper cooling water chamber and a cylinder sleeve lower water jacket is faster, such that an engine warming effect is improved.

Abstract: The present invention belongs to the technical field of diesel engines, and particularly relates to an engine cooling system and a cooling method therefor. In the engine cooling system of the present invention, when an engine needs to be warmed up, a first valve is opened, a lower engine body water storage chamber is in communication with an upper engine body water storage chamber, and some of the cooling water directly flows into the lower engine body water storage chamber from the upper engine body water storage chamber. The flow of the cooling water entering an engine body is reduced, and under the condition that heat dissipated by the engine is unchanged, the temperature rise of the cooling water flowing through the engine body such as a cylinder sleeve upper cooling water chamber and a cylinder sleeve lower water jacket is faster, such that an engine warming effect is improved.

Abstract: A cylinder head includes an intake throat and an intake duct, a valve seat ring is provided in an inner ring of the intake throat; a section of the intake duct is a tumble generating duct; and an extending direction of the tumble generating duct is oblique relative to the cylinder head bottom surface, the lower side surface of the tumble generating duct is a tumble guide surface, the lower end of which forms a tumble generating sharp angle, and the projection of the tumble generating sharp angle on the upper end circular surface of the valve seat ring is a sharp angle projection, the sharp angle projection is a protruding area protruding from the edge of the upper end circular surface of the valve seat ring, and the width of the middle part of the sharp angle projection is larger than the width of both ends thereof.

Abstract: A cylinder head includes an intake throat and an intake duct, a valve seat ring is provided in an inner ring of the intake throat; a section of the intake duct is a tumble generating duct; and an extending direction of the tumble generating duct is oblique relative to the cylinder head bottom surface, the lower side surface of the tumble generating duct is a tumble guide surface, the lower end of which forms a tumble generating sharp angle, and the projection of the tumble generating sharp angle on the upper end circular surface of the valve seat ring is a sharp angle projection, the sharp angle projection is a protruding area protruding from the edge of the upper end circular surface of the valve seat ring, and the width of the middle part of the sharp angle projection is larger than the width of both ends thereof.

Abstract: A filtering assembly that receives an inlet air includes a modulation panel subassembly, an air filter subassembly downstream of the modulation panel subassembly, wherein the air filter subassembly is configured to discharge the inlet air from the filtering assembly, and an arm subassembly configured to move the modulation panel subassembly and to move the air filter subassembly. The air filter subassembly moves into and out of a flow of the inlet air.

Abstract: Systems and methods are provided for providing control instructions to a pilot in the event of a loss of control of primary flight surfaces of an aircraft. The control instructions are determined using an emergency flight controller for receiving a pilot input, the emergency flight controller being in operable communication with at least one sensor for sensing aircraft parameters. The emergency flight controller is configured to determine target thrusts for the multiple engines and a target stabilizer position for the trimmable stabilizer on the basis of pilot input and sensed aircraft parameters. A guidance module is configured to provide instructions to a pilot as to how to control the engine thrusts toward the thrust targets and as how to control the trimmable stabilizer towards the target trimmable stabilizer position.

Abstract: A filtering assembly that receives an inlet air includes a modulation panel subassembly, an air filter subassembly downstream of the modulation panel subassembly, wherein the air filter subassembly is configured to discharge the inlet air from the filtering assembly, and an arm subassembly configured to move the modulation panel subassembly and to move the air filter subassembly. The air filter subassembly moves into and out of a flow of the inlet air.