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	<title type="text">ConairSystem.com - Patents</title>
	<subtitle type="text">Design, analysis and consulting services for aviation</subtitle>
	<link rel="alternate" type="text/html" href="http://www.conairsystem.com"/>
	<id>http://www.conairsystem.com/en/patents</id>
	<updated>2017-08-07T14:02:49+02:00</updated>
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	<entry>
		<title>Granted Patents</title>
		<link rel="alternate" type="text/html" href="http://www.conairsystem.com/en/patents/33-granted-patents"/>
		<published>2014-01-23T14:14:37+01:00</published>
		<updated>2014-01-23T14:14:37+01:00</updated>
		<id>http://www.conairsystem.com/en/patents/33-granted-patents</id>
		<author>
			<name>Super User</name>
			<email>info@conairsystem.com</email>
		</author>
		<summary type="html">&lt;ul&gt;
&lt;li&gt;Hybrid Aircraft Propulsion Control System, Czech patent No. 304135&lt;/li&gt;
&lt;li&gt;Hybrid Aircraft Propulsion System, Czech patent No. 300681&lt;/li&gt;
&lt;li&gt;Retractable Landing Gear Mechanism, Czech patent No. 289870&lt;/li&gt;
&lt;li&gt;Aircraft Engine Torsion Damper, Czech patent No. 282940&lt;/li&gt;
&lt;/ul&gt;</summary>
		<content type="html">&lt;ul&gt;
&lt;li&gt;Hybrid Aircraft Propulsion Control System, Czech patent No. 304135&lt;/li&gt;
&lt;li&gt;Hybrid Aircraft Propulsion System, Czech patent No. 300681&lt;/li&gt;
&lt;li&gt;Retractable Landing Gear Mechanism, Czech patent No. 289870&lt;/li&gt;
&lt;li&gt;Aircraft Engine Torsion Damper, Czech patent No. 282940&lt;/li&gt;
&lt;/ul&gt;</content>
	</entry>
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