公开(公告)号：US20200018220A1

公开(公告)日：2020-01-16

申请号：US16577728

申请日：2019-09-20

Applicant: DeltaHawk Engines, Inc.

Inventor： Douglas A. Doers ,  Robert A. Greco ,  Paul Olesen ,  Dennis Raymond Webb

IPC: F01P3/02 ,  F02B9/02 ,  F02B23/06 ,  F02B33/34 ,  F02B37/04 ,  F02B75/02 ,  F02F1/00 ,  F02F3/00

Abstract: A 2-cycle, direct-injection diesel engine configured to accommodate low cetane diesel and jet fuels. The engine includes combustion chambers having surfaces which are operable at high temperatures during engine operation to increase the combustion rate of low cetane fuels. The engine is further configured to reduce starting times in cold and/or low pressure situations such as those experienced during attempts to restart a plane engine at relatively high altitudes.

公开(公告)号：US10711681B2

公开(公告)日：2020-07-14

申请号：US16577728

申请日：2019-09-20

Applicant: DeltaHawk Engines, Inc.

Inventor： Douglas A. Doers ,  Robert A. Greco ,  Paul Olesen ,  Dennis Raymond Webb

IPC: F01P3/02 ,  F02B9/02 ,  F02F3/00 ,  F02B37/00 ,  F02B23/06 ,  F02B33/34 ,  F02B37/04 ,  F02B75/02 ,  F02F1/00 ,  F02B33/02 ,  F02B1/12 ,  F02B61/04

Abstract: A 2-cycle, direct-injection diesel engine configured to accommodate low cetane diesel and jet fuels. The engine includes combustion chambers having surfaces which are operable at high temperatures during engine operation to increase the combustion rate of low cetane fuels. The engine is further configured to reduce starting times in cold and/or low pressure situations such as those experienced during attempts to restart a plane engine at relatively high altitudes.

公开(公告)号：US10458307B2

公开(公告)日：2019-10-29

申请号：US16224281

申请日：2018-12-18

Applicant: DeltaHawk Engines, Inc.

Inventor： Douglas A. Doers ,  Robert A. Greco ,  Paul Olesen ,  Dennis Raymond Webb

IPC: F01P3/02 ,  F02B9/02 ,  F02B23/06 ,  F02B33/34 ,  F02B37/04 ,  F02B75/02 ,  F02F1/00 ,  F02F3/00 ,  F02B1/12 ,  F02B33/02 ,  F02B37/00 ,  F02B61/04

Abstract: A 2-cycle, direct-injection diesel engine configured to accommodate low cetane diesel and jet fuels. The engine includes combustion chambers having surfaces which are operable at high temperatures during engine operation to increase the combustion rate of low cetane fuels. The engine is further configured to reduce starting times in cold and/or low pressure situations such as those experienced during attempts to restart a plane engine at relatively high altitudes.

公开(公告)号：US20200291844A1

公开(公告)日：2020-09-17

申请号：US16892088

申请日：2020-06-03

Applicant: DeltaHawk Engines, Inc.

Inventor： Douglas A. Doers ,  Robert A. Greco ,  Paul Olesen ,  Dennis Raymond Webb

IPC: F01P3/02 ,  F02B9/02 ,  F02B23/06 ,  F02B33/34 ,  F02B37/04 ,  F02B75/02 ,  F02F1/00 ,  F02F3/00

Abstract: A 2-cycle, direct-injection diesel engine configured to accommodate low cetane diesel and jet fuels. The engine includes combustion chambers having surfaces which are operable at high temperatures during engine operation to increase the combustion rate of low cetane fuels. The engine is further configured to reduce starting times in cold and/or low pressure situations such as those experienced during attempts to restart a plane engine at relatively high altitudes.

公开(公告)号：US20190120117A1

公开(公告)日：2019-04-25

申请号：US16224281

申请日：2018-12-18

Applicant: DeltaHawk Engines, Inc.

Inventor： Douglas A. Doers ,  Robert A. Greco ,  Paul Olesen ,  Dennis Raymond Webb

IPC: F01P3/02 ,  F02B9/02 ,  F02B23/06 ,  F02B33/34 ,  F02B37/04 ,  F02B75/02 ,  F02F1/00 ,  F02F3/00

CPC classification number: F01P3/02 ,  F02B1/12 ,  F02B9/02 ,  F02B23/0627 ,  F02B33/02 ,  F02B33/34 ,  F02B37/00 ,  F02B37/04 ,  F02B61/04 ,  F02B75/02 ,  F02B2075/025 ,  F02B2201/02 ,  F02B2700/03 ,  F02F1/004 ,  F02F3/0084 ,  F05C2201/021

Abstract: A 2-cycle, direct-injection diesel engine configured to accommodate low cetane diesel and jet fuels. The engine includes combustion chambers having surfaces which are operable at high temperatures during engine operation to increase the combustion rate of low cetane fuels. The engine is further configured to reduce starting times in cold and/or low pressure situations such as those experienced during attempts to restart a plane engine at relatively high altitudes.