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	<title type="text">ConairSystem.com - News</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/news</id>
	<updated>2017-08-07T14:00:35+02:00</updated>
	<generator uri="http://joomla.org" version="2.5">Joomla! - Open Source Content Management</generator>
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	<entry>
		<title>Development of new reciprocating engine for fixed and rotary-wing UAV </title>
		<link rel="alternate" type="text/html" href="http://www.conairsystem.com/en/news/42-development-of-new-reciprocating-engine-for-fixed-and-rotary-wing-uav"/>
		<published>2016-05-18T15:24:38+02:00</published>
		<updated>2016-05-18T15:24:38+02:00</updated>
		<id>http://www.conairsystem.com/en/news/42-development-of-new-reciprocating-engine-for-fixed-and-rotary-wing-uav</id>
		<author>
			<name>Super User</name>
			<email>info@conairsystem.com</email>
		</author>
		<summary type="html">&lt;p&gt;Reflecting the current development activities in the fixed and rotary-wing UAV sector, Conairsystem company initiated development of a new reciprocating engine intended for UAV applications in the 150 – 450 kg take-off weight range. The project is aimed at providing a versatile and reliable engine with a multi-fuel (HFE) capability for UAV propulsion applications. This time, ground tests of the engine demonstrator on the propeller test stand are performed. Conairsystem company is looking for cooperation with other companies in the development and utilization of the project. For more info see our &lt;a href=&quot;en/projects&quot; target=&quot;_self&quot; title=&quot;Projects&quot;&gt;Project page&lt;/a&gt;.&lt;/p&gt;</summary>
		<content type="html">&lt;p&gt;Reflecting the current development activities in the fixed and rotary-wing UAV sector, Conairsystem company initiated development of a new reciprocating engine intended for UAV applications in the 150 – 450 kg take-off weight range. The project is aimed at providing a versatile and reliable engine with a multi-fuel (HFE) capability for UAV propulsion applications. This time, ground tests of the engine demonstrator on the propeller test stand are performed. Conairsystem company is looking for cooperation with other companies in the development and utilization of the project. For more info see our &lt;a href=&quot;en/projects&quot; target=&quot;_self&quot; title=&quot;Projects&quot;&gt;Project page&lt;/a&gt;.&lt;/p&gt;</content>
	</entry>
	<entry>
		<title>Certification  Support of the DOA PBS Velká Bíteš – APU  Safir  5K/G Z8 project</title>
		<link rel="alternate" type="text/html" href="http://www.conairsystem.com/en/news/37-certification-support-of-the-doa-pbs-velka-bites-apu-safir-5k-g-z8-project"/>
		<published>2014-07-02T10:36:20+02:00</published>
		<updated>2014-07-02T10:36:20+02:00</updated>
		<id>http://www.conairsystem.com/en/news/37-certification-support-of-the-doa-pbs-velka-bites-apu-safir-5k-g-z8-project</id>
		<author>
			<name>Super User</name>
			<email>info@conairsystem.com</email>
		</author>
		<summary type="html">&lt;p&gt;With reference to the results of our certification support activities in the field of Auxiliary Power Units, a new bookmark &lt;a href=&quot;en/references&quot; target=&quot;_self&quot; title=&quot;References&quot;&gt;REFERENCES&lt;/a&gt; was added to our web pages. This new bookmark contains the latest information about our participation in the certification of the Auxiliary Power Unit (APU), successfully completed by the issue of ETSO certificate by the EASA (European Aviation Safety Agency).&lt;/p&gt;</summary>
		<content type="html">&lt;p&gt;With reference to the results of our certification support activities in the field of Auxiliary Power Units, a new bookmark &lt;a href=&quot;en/references&quot; target=&quot;_self&quot; title=&quot;References&quot;&gt;REFERENCES&lt;/a&gt; was added to our web pages. This new bookmark contains the latest information about our participation in the certification of the Auxiliary Power Unit (APU), successfully completed by the issue of ETSO certificate by the EASA (European Aviation Safety Agency).&lt;/p&gt;</content>
	</entry>
	<entry>
		<title>Granting of a Czech Patent (2nd October , 2013)</title>
		<link rel="alternate" type="text/html" href="http://www.conairsystem.com/en/news/34-granting-of-a-czech-patent-2nd-october-2013"/>
		<published>2013-10-02T13:24:37+02:00</published>
		<updated>2013-10-02T13:24:37+02:00</updated>
		<id>http://www.conairsystem.com/en/news/34-granting-of-a-czech-patent-2nd-october-2013</id>
		<author>
			<name>Super User</name>
			<email>info@conairsystem.com</email>
		</author>
		<summary type="html">&lt;p&gt;The Industrial Property Office (Patent Office) of the Czech Republic has granted a patent for the „Aircraft Hybrid Propulsion Control System”, Pat. No. 304135, to the co-authors J. Vycital and T. Moravec.&lt;/p&gt;</summary>
		<content type="html">&lt;p&gt;The Industrial Property Office (Patent Office) of the Czech Republic has granted a patent for the „Aircraft Hybrid Propulsion Control System”, Pat. No. 304135, to the co-authors J. Vycital and T. Moravec.&lt;/p&gt;</content>
	</entry>
	<entry>
		<title>AERO Friedrichshafen 2012 (18-19th April)</title>
		<link rel="alternate" type="text/html" href="http://www.conairsystem.com/en/news/27-aero-friedrichshafen-2012-18-19th-april"/>
		<published>2012-04-20T10:08:25+02:00</published>
		<updated>2012-04-20T10:08:25+02:00</updated>
		<id>http://www.conairsystem.com/en/news/27-aero-friedrichshafen-2012-18-19th-april</id>
		<author>
			<name>Super User</name>
			<email>info@conairsystem.com</email>
		</author>
		<summary type="html">&lt;p&gt;Conairsystem representatives visited the AERO Friedrichshafen 2012 (18-19th April), where they participated in the conferences and meetings dedicated to the electrical flight. Valuable contacts were established with the power plant, electrical power system manufacturers and also with the representative of the FAA involved in the rulemaking process for the emerging area of electrical aircraft.&lt;/p&gt;</summary>
		<content type="html">&lt;p&gt;Conairsystem representatives visited the AERO Friedrichshafen 2012 (18-19th April), where they participated in the conferences and meetings dedicated to the electrical flight. Valuable contacts were established with the power plant, electrical power system manufacturers and also with the representative of the FAA involved in the rulemaking process for the emerging area of electrical aircraft.&lt;/p&gt;</content>
	</entry>
	<entry>
		<title>The ConairSystem web pages launched</title>
		<link rel="alternate" type="text/html" href="http://www.conairsystem.com/en/news/23-the-conairsystem-web-pages-launched"/>
		<published>2012-04-01T23:04:11+02:00</published>
		<updated>2012-04-01T23:04:11+02:00</updated>
		<id>http://www.conairsystem.com/en/news/23-the-conairsystem-web-pages-launched</id>
		<author>
			<name>Super User</name>
			<email>info@conairsystem.com</email>
		</author>
		<summary type="html">&lt;p&gt;&lt;img src=&quot;images/news/web_pages_launched/web_pages_launched.jpg&quot; border=&quot;0&quot; alt=&quot;ConairSystem.com&quot; width=&quot;200&quot; height=&quot;153&quot; style=&quot;float: left; border: 0; margin-top: 2px; margin-bottom: 2px; margin-left: 0px; margin-right: 10px;&quot; /&gt;&lt;/p&gt;
&lt;p&gt;The ConairsSystem web pages were launched to offer design, analysis and consulting services for Aviation. These web pages also introduce own aviation development projects related to the electrical power and new piston engines design concepts.&lt;/p&gt;</summary>
		<content type="html">&lt;p&gt;&lt;img src=&quot;images/news/web_pages_launched/web_pages_launched.jpg&quot; border=&quot;0&quot; alt=&quot;ConairSystem.com&quot; width=&quot;200&quot; height=&quot;153&quot; style=&quot;float: left; border: 0; margin-top: 2px; margin-bottom: 2px; margin-left: 0px; margin-right: 10px;&quot; /&gt;&lt;/p&gt;
&lt;p&gt;The ConairsSystem web pages were launched to offer design, analysis and consulting services for Aviation. These web pages also introduce own aviation development projects related to the electrical power and new piston engines design concepts.&lt;/p&gt;</content>
	</entry>
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