Direct-injection internal-combustion engine with dual sheet angle for producing a fuel mixture in a combustion chamber with dual combustion zone and low compression ratio, and method for using same

Patent metadata

Field	Value
Publication number	US-10024222-B2
Application number	US-201515306434-A
Country	US
Kind code	B2
Filing date	Apr 8, 2015
Priority date	Apr 24, 2014
Publication date	Jul 17, 2018
Grant date	Jul 17, 2018

Abstract

The present invention relates to a compression-ignition direct-injection internal-combustion engine with a compression ratio ranging between 13.5 and 16.5 including a combustion chamber limited on one side by upper face ( 44 ) of a piston ( 16 ) comprising a projection ( 48 ) arranged in the center of a concave bowl ( 46 ) with at least two mixing zones (Z 1 , Z 2 ), a fuel injection comprising at least one injector ( 30 ) projecting fuel in at least two fuel jet sheets ( 36, 38 ) with different sheet angles (A 1 , A 2 ). The fuel injector comprises two rows of injection orifices ( 33 a, 33 b ) arranged one above the other with the number of orifices of each row (Ninf, Nsup) is greater than or equal to −4·Ns+14 and less than or equal to −4·Ns+16 for the lower sheet or −4·Ns+18 for the upper sheet. Ns is the swirl number of this engine with a swirl number less than 1.5.

First claim

The invention claimed is:

1. A compression-ignition direct-injection internal-combustion engine comprising:
at least one cylinder, a cylinder head carrying fuel injection, a piston sliding in each of the at least one cylinder, a combustion chamber delimited on one side by an upper face of the piston comprising a projection extending in a direction of the cylinder head and disposed in a center of a concave bowl with at least two mixing zones, the fuel injection comprising one injector projecting fuel in at least upper and lower fuel jet sheets having different sheet angles with a lower sheet jet axis intersecting a lower mixing zone and an upper sheet jet axis intersecting an upper mixing zone, the fuel injection comprising an upper row of injection orifices and a lower row of injection orifices below the upper row of injection orifices, a number of injection orifices of the upper row of injection orifices being greater than a number of injection orifices of the lower row of injection orifices, and the number of orifices of each row is greater than or equal to 4Ns+14 and for the lower row is less than or equal to 4Ns+16 and for the upper row is less than or equal to 4Ns+18 and Ns is a swirl number of the engine.

2. An engine as claimed in claim 1 , wherein the swirl number Ns is less than 1.5.

3. A engine as claimed in claim 2 , comprising injecting fuel jets with the upper fuel jet sheet having an angular offset with respect to injecting fuel jets with the lower fuel jet sheet.

4. An engine as claimed in claim 1 , wherein the swirl number Ns is less than 1.

5. A engine as claimed in claim 4 , comprising injecting fuel jets with the upper fuel jet sheet having an angular offset with respect to injecting fuel jets with the lower fuel jet sheet.

6. An engine as claimed in claim 1 , comprising injecting fuel jets with the upper fuel jet sheet having an angular offset with respect to injecting fuel jets with the lower fuel jet sheet.

7. A fuel injection method for a compression-ignition direct-injection internal-combustion engine comprising at least one cylinder, a cylinder head carrying fuel injection, a piston sliding in each of the at least one cylinder, a combustion chamber delimited on one side by an upper face of the piston comprising a projection extending in a direction of the cylinder head and disposed in a center of a concave bowl with at least two mixing zones, the fuel injection comprising at least one injector projecting fuel in at least upper and lower fuel jet sheets having different sheet angles with a lower sheet jet axis intersecting a lower mixing zone and an upper sheet jet axis intersecting an upper mixing zone, the fuel injection comprising an upper row of injection orifices and a lower row of injection orifices below the upper row of injection orifices, a number of injection orifices of the upper row of injection orifices being greater than a number of injection orifices of the lower row of injection orifices, and the number of orifices of each row is greater than or equal to 4Ns+14 and for the lower row is less than or equal to 4Ns+16 and for the upper row is less than or equal to 4Ns+18 and Ns is a swirl number of the engine comprising:
injecting fuel in at least two fuel jet sheets with different sheet angles; and
the injecting of fuel occurs from two rows of injection orifices arranged one above the other.

8. A method as claimed in claim 7 , wherein a minimum compression ratio is 13.5 and a maximum compression ratio is 16.5.

9. A method as claimed in claim 8 , comprising injecting fuel jets with the upper fuel jet sheet having an angular offset with respect to injecting fuel jets with the lower fuel jet sheet.

10. A method as claimed in claim 7 , wherein the swirl number Ns is less than 1.5.

11. A method as claimed in claim 10 , comprising injecting fuel jets with the upper fuel jet sheet having an angular offset with respect to injecting fuel jets with the lower fuel jet sheet.

12. A method as claimed in claim 7 , wherein the swirl number Ns is less than 1.

13. A method as claimed in claim 7 , comprising injecting fuel jets with the upper fuel jet sheet having an angular offset with respect to injecting fuel jets with the lower fuel jet sheet.

Assignees

• Ifp Energies Now

Inventors

• Martinez Lionel
• RICHARD STéPHANE
• Laget Olivier

Classifications

• F02B23/0669 Primary

  having multiple fuel spray jets per injector nozzle · CPC title

• Y02T10/125

  Cross-Sectional Technologies · mapped topic

• Y02T10/12

  Improving ICE efficiencies · CPC title