公开(公告)号：WO2005012714A3

公开(公告)日：2007-07-19

申请号：PCT/US2004013234

申请日：2004-04-28

Applicant: PAUL MARIUS A

Inventor： MARIUS A PAUL

IPC: F02K5/00 ,  F02K20060101 ,  F02K3/02

CPC classification number: F01D5/187 ,  F02C3/067 ,  F02C3/073 ,  F02C3/08 ,  F02C3/36 ,  F02C7/042 ,  F02C7/143 ,  F02K1/1207 ,  F02K3/10 ,  F02K3/105 ,  F02K7/16 ,  F02K7/18 ,  F02K9/78 ,  F05D2260/202 ,  F05D2260/40311

Abstract: Engine embodiments primarily designed for aircraft propulsion and power generation incorporating the Carnot cycle for efficient combustion with typical embodiments including air compressors having one or more stages with isothermal compression and including combustion and expansion chambers having in part isothermal expansion before final adiabatic expansion.

Abstract translation: 发动机实施例主要设计用于结合卡诺循环以用于有效燃烧的飞行器推进和发电，其典型实施例包括具有一个或多个等级压缩级的空气压缩机，并且包括在最终绝热膨胀之前具有部分等温膨胀的燃烧和膨胀室。