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1. WO2007086820 - DIESEL AIRCRAFT ENGINE

Publication Number WO/2007/086820
Publication Date 02.08.2007
International Application No. PCT/US2005/044262
International Filing Date 07.12.2005
IPC
F02B 75/06 2006.01
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
75Other engines, e.g. single-cylinder engines
06Engines with means for equalising torque
F02B 75/22 2006.01
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
75Other engines, e.g. single-cylinder engines
16Engines characterised by number of cylinders, e.g. single-cylinder engines
18Multi-cylinder engines
22with cylinders in V-, fan-, or star-arrangement
CPC
F02B 61/04
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
61Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing
04for driving propellers
F02B 75/24
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
75Other engines
16Engines characterised by number of cylinders, e.g. single-cylinder engines
18Multi-cylinder engines
24with cylinders arranged oppositely relative to main shaft and of "flat" type
F02B 75/246
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
75Other engines
16Engines characterised by number of cylinders, e.g. single-cylinder engines
18Multi-cylinder engines
24with cylinders arranged oppositely relative to main shaft and of "flat" type
246with only one crankshaft of the "pancake" type, e.g. pairs of connecting rods attached to common crankshaft bearing
Y10T 74/2183
YSECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
10TECHNICAL SUBJECTS COVERED BY FORMER USPC
TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
74Machine element or mechanism
21Elements
2173Cranks and wrist pins
2183Counterbalanced
Applicants
  • SCHRICK, INC. [US]/[US] (AllExceptUS)
  • FUCHS, Michael, J. [US]/[US] (UsOnly)
  • WEINZIERL, Steven, M. [US]/[US] (UsOnly)
Inventors
  • FUCHS, Michael, J.
  • WEINZIERL, Steven, M.
Agents
  • GOTTSCHALK, William, S.
Priority Data
11/072,62404.03.2005US
60/642,83711.01.2005US
Publication Language English (EN)
Filing Language English (EN)
Designated States
Title
(EN) DIESEL AIRCRAFT ENGINE
(FR) MOTEUR DIESEL D’AERONEF
Abstract
(EN)
The present invention is an engine, including two banks of cylinders in a flat, opposed cylinder arrangement and a crankshaft having a plurality throws, the two throws of each respective pair of throws being disposed adjacent to each and coplanar with respect to each other.
(FR)
La présente invention concerne un moteur qui comprend deux bancs de cylindres dans un agencement plat de cylindres opposés et un vilebrequin qui possède une pluralité de coups, les deux coups de chaque paire respective de coups étant disposés de façon adjacente l’un à l’autre et coplanaire l’un par rapport à l’autre.
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