Piston, in particular for an HPDI diesel/gas internal combustion engine

Patent metadata

Field	Value
Publication number	US-10890136-B2
Application number	US-201816196210-A
Country	US
Kind code	B2
Filing date	Nov 20, 2018
Priority date	Nov 20, 2017
Publication date	Jan 12, 2021
Grant date	Jan 12, 2021

Abstract

A piston for an internal combustion engine, such as a high-pressure direct injection (HPDI) diesel/gas internal combustion engine. The piston has a piston recess, in particular an omega piston recess. The piston has a piston crown face which is provided so as to extend annularly about a centre axis (M) of the piston. The piston has a plurality of piston stages, which are provided so as to extend annularly about the centre axis (M) and which are arranged between the piston crown face and the piston recess. The piston geometry can lead to an increase of the degree of engine efficiency with a simultaneous reduction of the exhaust emissions.

First claim

The invention claimed is:

1. A piston for an internal combustion engine, comprising:
a piston recess;
a piston crown face which is provided so as to extend annularly about a centre axis (M) of the piston; and
a plurality of piston stages which are provided so as to extend annularly about the centre axis (M) and which are arranged between the piston crown face and the piston recess,
wherein the plurality of piston stages have a radially inner piston stage and a radially outer piston stage;
the radially inner piston stage has a stage base, a stage wall and a transition region between the stage base of the radially inner piston stage and the stage wall of the radially inner piston stage;
the stage base of the radially inner piston stage is inclined with respect to a notional first plane, which intersects with the centre axis (M) at a right angle;
the transition region of the radially inner piston stage is constructed with a predetermined radius (R 4 );
the stage wall of the radially inner piston stage is inclined with respect to the centre axis (M);
the stage base of the radially inner piston stage and the stage wall of the radially inner piston stage are constructed in a planar manner;
the stage base of the radially inner piston stage and the stage wall of the radially inner piston stage are constructed so as to rise in a radial direction away from the centre axis (M);
the radially outer piston stage has a stage base, a stage wall and a transition region between the stage base of the radially outer piston stage and the stage wall of the radially outer piston stage;
the stage base of the radially outer piston stage is inclined with respect to a notional second plane which intersects with the centre axis (M) at a right angle;
the transition region of the radially outer piston stage is constructed with a predetermined radius (R 6 );
the stage wall of the radially outer piston stage extends parallel with the centre axis (M);
the stage base of the radially outer piston stage and the stage wall of the radially outer piston stage are constructed in a planar manner; and
the stage base of the radially outer piston stage is constructed so as to rise in a radial direction away from the centre axis.

2. The piston according to claim 1 , wherein the internal combustion engine is an HPDI diesel/gas internal combustion engine.

3. The piston according to claim 1 , wherein the piston recess is an omega piston recess.

4. The piston according to claim 1 , wherein the radially outer piston stage merges in a radial direction with respect to the centre axis (M) into the radially inner piston stage.

5. The piston according to claim 1 , wherein:
the radially inner piston stage merges via a beam splitter contour which is provided so as to extend annularly about the centre axis (M) into the piston recess; or
the radially outer piston stage merges into the piston crown face.

6. The piston according to claim 5 , wherein the radially outer piston stage merges into the piston crown face in a rounded manner.

7. The piston according to claim 5 , wherein:
the beam splitter contour is constructed as a projection which protrudes radially with respect to the centre axis (M); or
the beam splitter contour is provided with a predetermined radius (R 3 ) in a range between a value greater than 0 mm and 30 mm, or between 1 mm and 10 mm, or between 2 mm and 6 mm; or
the beam splitter contour defines at a radially innermost location of the beam splitter contour an inner diameter (D 1 ) which is in a range between 40% and 100%, or between 40% and 80%, or between 40% and 60%, of a piston outer diameter (D 0 ) of the piston; or
the beam splitter contour in an axial direction along the centre axis (M) is recessed with respect to the piston crown face in a range between 0% and 60%, or between 0% and 20%, or between 2% and 10%, of a maximum depth (H 0 ) of the piston recess.

8. The piston as claimed in claim 1 , wherein:
the predetermined radius (R 4 ) of the transition region of the radially inner piston stage is between a value greater than 0 mm and 10 mm, or between 1 mm and 8 mm, or between 1.5 mm and 6 mm; or
the stage wall of the radially inner piston stage is inclined at an angle (γ) between 0° and 60°, or between 0° and 45°, or between 15° and 45°, with respect to the centre axis (M); or
the stage wall of the radially inner piston stage merges over a predetermined radius (R 5 ) in a range between a value greater than 0 mm and 10 mm, or a value greater than 0 mm and 8 mm, or between 0.2 mm and 4 mm, into the radially outer piston stage.

9. The piston according to claim 1 , wherein:
the stage base of the radially inner piston stage is inclined at an angle (β) between 0° and 60°, or between 0° and 45°, or between 15° and 45°, with respect to the notional first plane; or
the transition region defines at a radially innermost location of the transition region an inner diameter (D 2 ) which is in a range between 50% and 95%, or between 60% and 85%, or between 60% and 70%, of a piston outer diameter (D 0 ) of the piston.

10. The piston according to claim 1 , wherein:
the stage base of the radially outer piston stage is inclined at an angle (δ) between 0° and 60°, or between 0° and 45°, or between 15° and 45°, with respect to the notional second plane; or
the predetermined radius (R 6 ) of the transition region of the radially outer piston stage is between a value greater than 0 mm and 10 mm, or between 1 mm and 8 mm, or between 1.5 mm and 6 mm, or
a height (H 3 ) of the stage wall of the radially outer piston stage is in a range between 0% and 60%, or between 0% and 10%, or between 1% and 5%, of a maximum depth (H 0 ) of the piston recess.

11. The piston according to claim 1 , wherein:
an undercut region which is provided so as to extend annularly about the centre axis (M), wherein:
the central protrusion and the centre axis (M) define an angle (α) in a range between 15° and 90°, or between 40° and 80°, or between 60° and 75°; or
the undercut region has a predetermined radius (R 2 ) in a range between a value greater than 0 mm and 50 mm, or between a value greater than 0 mm and 30 mm, or between 5 mm and 15 mm; or
the central protrusion has a predetermined radius (R 1 ) in a range between a value greater than 0 mm and 200 mm, or between a value greater than 0 mm and 50 mm, or between 5 mm and 25 mm; or
the central protrusion in an axial direction along the centre axis (M) is recessed with respect to the piston crown face in a range between 2% and 50%, or between 4% and 15%, or between 5% and 10%, of a maximum depth (H 0 ) of the piston recess.

12. The piston according to claim 11 , wherein the central protrusion is in the form of a cone tip or a truncated cone.

13. The piston according to claim 1 , wherein:
the piston crown face defines at a radially innermost location of the piston crown face an inner diameter (D 3 ) which is between 30% and 75%, or between 35% and 70%, or between 40% and 60%, of a piston outer diameter (D 0 ) of the piston; or
the piston crown face is constructed in a planar manner; or
the piston recess, the piston crown face or the plurality of piston stages are constructed in a rotationally symmetrical manner about the centre axis (M).

14. The piston according to claim 1 , wherein:
the plurality of piston stages are recessed in an axial direction along the centre axis (M) with respect to the piston crown face or raised with respect to the piston recess; or
the piston recess is recessed in an axial direction along the centre axis (M) with respect to the piston crown face or recessed with respect to the plurality o

Assignees

• Man Truck & Bus Ag

Inventors

• Díaz-Blanco Bruno Barciela
• Weberskirch Dirk Peter
• Sommermann Andreas
• Stein Marcus
• Dressel Tim

Classifications

• F02B23/06

  the combustion space being arranged in working piston (F02B23/04 takes precedence) · CPC title

• F02B7/06 Primary

  the fuel in the charge being gaseous · CPC title

• F02B23/0651

  the fuel spray impinging on reflecting surfaces or being specially guided throughout the combustion space · CPC title

• F02B43/00

  Engines characterised by operating on gaseous fuels; Plants including such engines (engines characterised by the gas-air charge being ignited by compression ignition of an additional fuel F02B7/06; engines convertible from gas to other fuel consumption F02B69/04) · CPC title

• F02B23/0672

  Omega-piston bowl, i.e. the combustion space having a central projection pointing towards the cylinder head and the surrounding wall being inclined towards the cylinder center axis (the surrounding wall being exactly vertical F02B23/0696) · CPC title