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Numerical Analysis of Combustion and Flow Inside a Small Rotary Engine for Developing an Unmanned Helicopter Chiba University

SAE Technical Papers (1906-current) Available online

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Format:
Book
Conference/Event
Author/Creator:
YAMADA, Takafumi, author.
Conference Name:
Small Engine Technology Conference & Exposition (2007-10-30 : Nugata, Japan)
Language:
English
Physical Description:
1 online resource cm
Place of Publication:
Tokyo, JAPAN Society of Automotive Engineers of Japan 2007
Summary:
For a disaster relief and automatic inspections, an unmanned helicopter is strongly expected. To develop this, a very high power density source is required. A Wankel-type rotary engine can be the best candidate for the power source. In this study, the development of a very small rotary engine with a displacement of 30 cc is targeted. In order to improve the combustion efficiency, gas exchange and stable ignition, a multi dimensional simulation inside the combustion chamber was carried out. At first, the effect of volumetric efficiency on the maximum power is mentioned. Secondly, the effect of scavenging efficiency is discussed. Thirdly, a blow off through a plug hole is described. The position of plug hole was found important to reduce the blow off amount. Finally, the effect of combustion speed on the engine performance is predicted. As a result, the proposed design will be tested using a proto-type engine. Also, future subjects to achieve a high power density with a displacement of 30 cc will be solved by the authors' research in progress
Notes:
Vendor supplied data
Publisher Number:
2007-32-0098
Access Restriction:
Restricted for use by site license

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