Archive:Algie Composite Aircraft - Revision history

wikademia>Wikademia: moved Algie Composite Aircraft to Archive:Algie Composite Aircraft

2009-05-18T19:16:15Z

moved Algie Composite Aircraft to Archive:Algie Composite Aircraft

← Older revision	Revision as of 19:16, 18 May 2009
(No difference)

wikademia>Wikademia at 18:37, 13 April 2009

2009-04-13T18:37:49Z

@@ Line 4: / Line 4: @@
 *[http://members.iquest.net/~aca/ - Algie Composite Aircraft homepage]
 *[http://groups.yahoo.com/group/algiecompositeaircraft/?yguid=118519476 - Yahoo groups, Algie Composite Aircraft]
 {{ntnes}}
 [[Category:Aircraft manufacturers of the United States]]

wikademia>Wikademia at 18:36, 13 April 2009

2009-04-13T18:36:41Z

← Older revision		Revision as of 18:36, 13 April 2009
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	~~<!-- Please do not remove or change this AfD message until the issue is settled -->~~
	~~{{AfDM\|page=Algie Composite Aircraft\|logdate=2009 April 10\|substed=yes }}~~
	~~<!-- For administrator use only: {{oldafdfull\|page=Algie Composite Aircraft\|date=10 April 2009\|result='''keep'''}} -->~~
	~~<!-- End of AfD message, feel free to edit beyond this point -->~~
	~~{{Unreferenced\|date=April 2009}}~~
	~~{{Notability\|date=April 2009}}~~
	'''Algie Composite Aircraft''' is an [[aircraft kit]] company that is developing the LP1 kit. This is a high performance two seat [[aircraft]], featuring all [[carbon fiber]]/ [[Nomex]] [[honeycomb]] construction. Using modern composite fabrication techniques, it has an empty airframe weight at 210 lb. It is designed for high altitude cruise flight at high speed, cruise is 385 mph at 29,000 ft. The LP1 employs an [[elliptical wing]] planform for minimised induced drag. The engine used is the [[LS1]]/2/7 family of engines, basically stock except for a dry sump oiling system added. The engine's cruise rpm is kept to 3800 rpm, which the base LS1 produces about 300 hp at those revs. One of the unusual features of this design is its cockpit [[pressurisation]] system. The cockpit and engine are fed from a single large [[turbocharger]]. This turbo is capable of engine normalisation to FL300, and it has no cockpit pressure regulator, therefore the cockpit also is normalised to sea level pressure at this altitude, approx. 10 psi differential. The cabin door is of a plug-type design to withstand the 10 psi internal pressure, it retracts upwards and into the cabin roof area. Another innovative design feature is the cooling system. The engine has two angular mounted [[radiators]] that reside behind the cockpit seatbacks. These are fed cooling air from a large bellypan mounted [[NACA duct]] below the cockpit. Integrally designed with the cooling system is the turbo/ [[wastegate]] exhaust, which serves to scavenge the radiator exit air by high energy excitation principles, accelerating the low energy exit air to close to the free stream speeds. This gives the system the potential to reduce cooling drag to very low levels. Also of note, the wing uses hot engine coolant routed through the leading edge for a constant wing deice system. This feature also reduces cooling drag as it assists in cooling without needing ducted air, a zero drag cooling aid.		'''Algie Composite Aircraft''' is an [[aircraft kit]] company that is developing the LP1 kit. This is a high performance two seat [[aircraft]], featuring all [[carbon fiber]]/ [[Nomex]] [[honeycomb]] construction. Using modern composite fabrication techniques, it has an empty airframe weight at 210 lb. It is designed for high altitude cruise flight at high speed, cruise is 385 mph at 29,000 ft. The LP1 employs an [[elliptical wing]] planform for minimised induced drag. The engine used is the [[LS1]]/2/7 family of engines, basically stock except for a dry sump oiling system added. The engine's cruise rpm is kept to 3800 rpm, which the base LS1 produces about 300 hp at those revs. One of the unusual features of this design is its cockpit [[pressurisation]] system. The cockpit and engine are fed from a single large [[turbocharger]]. This turbo is capable of engine normalisation to FL300, and it has no cockpit pressure regulator, therefore the cockpit also is normalised to sea level pressure at this altitude, approx. 10 psi differential. The cabin door is of a plug-type design to withstand the 10 psi internal pressure, it retracts upwards and into the cabin roof area. Another innovative design feature is the cooling system. The engine has two angular mounted [[radiators]] that reside behind the cockpit seatbacks. These are fed cooling air from a large bellypan mounted [[NACA duct]] below the cockpit. Integrally designed with the cooling system is the turbo/ [[wastegate]] exhaust, which serves to scavenge the radiator exit air by high energy excitation principles, accelerating the low energy exit air to close to the free stream speeds. This gives the system the potential to reduce cooling drag to very low levels. Also of note, the wing uses hot engine coolant routed through the leading edge for a constant wing deice system. This feature also reduces cooling drag as it assists in cooling without needing ducted air, a zero drag cooling aid.

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	Image:ACA Autoclave.JPG\|ACA Autoclave for propeller blades, gearbox manufacture.		Image:ACA Autoclave.JPG\|ACA Autoclave for propeller blades, gearbox manufacture.
	</gallery>		</gallery>
			{{ntnes}}
	{{~~Aviation lists~~}}

	[[Category:Aircraft manufacturers of the United States]]		[[Category:Aircraft manufacturers of the United States]]

wikademia>Wikademia: 52 revisions

2009-04-12T00:52:30Z

52 revisions

← Older revision	Revision as of 00:52, 12 April 2009
(No difference)

wikademia>SmackBot: Date maintenance tags and general fixes

2009-04-11T04:11:52Z

Date maintenance tags and general fixes

← Older revision		Revision as of 04:11, 11 April 2009
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	<!-- For administrator use only: {{oldafdfull\|page=Algie Composite Aircraft\|date=10 April 2009\|result='''keep'''}} -->		<!-- For administrator use only: {{oldafdfull\|page=Algie Composite Aircraft\|date=10 April 2009\|result='''keep'''}} -->
	<!-- End of AfD message, feel free to edit beyond this point -->		<!-- End of AfD message, feel free to edit beyond this point -->
	{{~~unreferenced~~}}		{{Unreferenced\|date=April 2009}}
	{{~~notability~~}}		{{Notability\|date=April 2009}}
	'''Algie Composite Aircraft''' is an [[aircraft kit]] company that is developing the LP1 kit. This is a high performance two seat [[aircraft]], featuring all [[carbon fiber]]/ [[Nomex]] [[honeycomb]] construction. Using modern composite fabrication techniques, it has an empty airframe weight at 210 lb. It is designed for high altitude cruise flight at high speed, cruise is 385 mph at 29,000 ft. The LP1 employs an [[elliptical wing]] planform for minimised induced drag. The engine used is the [[LS1]]/2/7 family of engines, basically stock except for a dry sump oiling system added. The engine's cruise rpm is kept to 3800 rpm, which the base LS1 produces about 300 hp at those revs. One of the unusual features of this design is its cockpit [[pressurisation]] system. The cockpit and engine are fed from a single large [[turbocharger]]. This turbo is capable of engine normalisation to FL300, and it has no cockpit pressure regulator, therefore the cockpit also is normalised to sea level pressure at this altitude, approx. 10 psi differential. The cabin door is of a plug-type design to withstand the 10 psi internal pressure, it retracts upwards and into the cabin roof area. Another innovative design feature is the cooling system. The engine has two angular mounted [[radiators]] that reside behind the cockpit seatbacks. These are fed cooling air from a large bellypan mounted [[NACA duct]] below the cockpit. Integrally designed with the cooling system is the turbo/ [[wastegate]] exhaust, which serves to scavenge the radiator exit air by high energy excitation principles, accelerating the low energy exit air to close to the free stream speeds. This gives the system the potential to reduce cooling drag to very low levels. Also of note, the wing uses hot engine coolant routed through the leading edge for a constant wing deice system. This feature also reduces cooling drag as it assists in cooling without needing ducted air, a zero drag cooling aid.		'''Algie Composite Aircraft''' is an [[aircraft kit]] company that is developing the LP1 kit. This is a high performance two seat [[aircraft]], featuring all [[carbon fiber]]/ [[Nomex]] [[honeycomb]] construction. Using modern composite fabrication techniques, it has an empty airframe weight at 210 lb. It is designed for high altitude cruise flight at high speed, cruise is 385 mph at 29,000 ft. The LP1 employs an [[elliptical wing]] planform for minimised induced drag. The engine used is the [[LS1]]/2/7 family of engines, basically stock except for a dry sump oiling system added. The engine's cruise rpm is kept to 3800 rpm, which the base LS1 produces about 300 hp at those revs. One of the unusual features of this design is its cockpit [[pressurisation]] system. The cockpit and engine are fed from a single large [[turbocharger]]. This turbo is capable of engine normalisation to FL300, and it has no cockpit pressure regulator, therefore the cockpit also is normalised to sea level pressure at this altitude, approx. 10 psi differential. The cabin door is of a plug-type design to withstand the 10 psi internal pressure, it retracts upwards and into the cabin roof area. Another innovative design feature is the cooling system. The engine has two angular mounted [[radiators]] that reside behind the cockpit seatbacks. These are fed cooling air from a large bellypan mounted [[NACA duct]] below the cockpit. Integrally designed with the cooling system is the turbo/ [[wastegate]] exhaust, which serves to scavenge the radiator exit air by high energy excitation principles, accelerating the low energy exit air to close to the free stream speeds. This gives the system the potential to reduce cooling drag to very low levels. Also of note, the wing uses hot engine coolant routed through the leading edge for a constant wing deice system. This feature also reduces cooling drag as it assists in cooling without needing ducted air, a zero drag cooling aid.

wikademia>Bali ultimate: Wikipedia:Articles for deletion/Algie Composite Aircraft

2009-04-10T15:49:39Z

Wikipedia:Articles for deletion/Algie Composite Aircraft

← Older revision		Revision as of 15:49, 10 April 2009
Line 1:		Line 1:
			<!-- Please do not remove or change this AfD message until the issue is settled -->
			{{AfDM\|page=Algie Composite Aircraft\|logdate=2009 April 10\|substed=yes }}
			<!-- For administrator use only: {{oldafdfull\|page=Algie Composite Aircraft\|date=10 April 2009\|result='''keep'''}} -->
			<!-- End of AfD message, feel free to edit beyond this point -->
			{{unreferenced}}
			{{notability}}
	'''Algie Composite Aircraft''' is an [[aircraft kit]] company that is developing the LP1 kit. This is a high performance two seat [[aircraft]], featuring all [[carbon fiber]]/ [[Nomex]] [[honeycomb]] construction. Using modern composite fabrication techniques, it has an empty airframe weight at 210 lb. It is designed for high altitude cruise flight at high speed, cruise is 385 mph at 29,000 ft. The LP1 employs an [[elliptical wing]] planform for minimised induced drag. The engine used is the [[LS1]]/2/7 family of engines, basically stock except for a dry sump oiling system added. The engine's cruise rpm is kept to 3800 rpm, which the base LS1 produces about 300 hp at those revs. One of the unusual features of this design is its cockpit [[pressurisation]] system. The cockpit and engine are fed from a single large [[turbocharger]]. This turbo is capable of engine normalisation to FL300, and it has no cockpit pressure regulator, therefore the cockpit also is normalised to sea level pressure at this altitude, approx. 10 psi differential. The cabin door is of a plug-type design to withstand the 10 psi internal pressure, it retracts upwards and into the cabin roof area. Another innovative design feature is the cooling system. The engine has two angular mounted [[radiators]] that reside behind the cockpit seatbacks. These are fed cooling air from a large bellypan mounted [[NACA duct]] below the cockpit. Integrally designed with the cooling system is the turbo/ [[wastegate]] exhaust, which serves to scavenge the radiator exit air by high energy excitation principles, accelerating the low energy exit air to close to the free stream speeds. This gives the system the potential to reduce cooling drag to very low levels. Also of note, the wing uses hot engine coolant routed through the leading edge for a constant wing deice system. This feature also reduces cooling drag as it assists in cooling without needing ducted air, a zero drag cooling aid.		'''Algie Composite Aircraft''' is an [[aircraft kit]] company that is developing the LP1 kit. This is a high performance two seat [[aircraft]], featuring all [[carbon fiber]]/ [[Nomex]] [[honeycomb]] construction. Using modern composite fabrication techniques, it has an empty airframe weight at 210 lb. It is designed for high altitude cruise flight at high speed, cruise is 385 mph at 29,000 ft. The LP1 employs an [[elliptical wing]] planform for minimised induced drag. The engine used is the [[LS1]]/2/7 family of engines, basically stock except for a dry sump oiling system added. The engine's cruise rpm is kept to 3800 rpm, which the base LS1 produces about 300 hp at those revs. One of the unusual features of this design is its cockpit [[pressurisation]] system. The cockpit and engine are fed from a single large [[turbocharger]]. This turbo is capable of engine normalisation to FL300, and it has no cockpit pressure regulator, therefore the cockpit also is normalised to sea level pressure at this altitude, approx. 10 psi differential. The cabin door is of a plug-type design to withstand the 10 psi internal pressure, it retracts upwards and into the cabin roof area. Another innovative design feature is the cooling system. The engine has two angular mounted [[radiators]] that reside behind the cockpit seatbacks. These are fed cooling air from a large bellypan mounted [[NACA duct]] below the cockpit. Integrally designed with the cooling system is the turbo/ [[wastegate]] exhaust, which serves to scavenge the radiator exit air by high energy excitation principles, accelerating the low energy exit air to close to the free stream speeds. This gives the system the potential to reduce cooling drag to very low levels. Also of note, the wing uses hot engine coolant routed through the leading edge for a constant wing deice system. This feature also reduces cooling drag as it assists in cooling without needing ducted air, a zero drag cooling aid.

wikademia>DAlgie: Added autoclave picture.

2009-01-30T19:57:58Z

Added autoclave picture.

← Older revision		Revision as of 19:57, 30 January 2009
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	Image:DSCF0826ACA.JPG\|Elliptical wing buck		Image:DSCF0826ACA.JPG\|Elliptical wing buck
	Image:4blade6k.JPG\|4 blade propeller bucks		Image:4blade6k.JPG\|4 blade propeller bucks
			Image:ACA Autoclave.JPG\|ACA Autoclave for propeller blades, gearbox manufacture.
	</gallery>		</gallery>

wikademia>Sardanaphalus: updating link using AWB

2008-07-05T06:45:44Z

updating link using AWB

← Older revision		Revision as of 06:45, 5 July 2008
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	</gallery>		</gallery>

	{{~~airlistbox~~}}		{{Aviation lists}}

	[[Category:Aircraft manufacturers of the United States]]		[[Category:Aircraft manufacturers of the United States]]

wikademia>DAlgie at 01:23, 18 February 2008

2008-02-18T01:23:40Z

← Older revision		Revision as of 01:23, 18 February 2008
Line 11:		Line 11:
	Image:DSCF0386aca.JPG\|The LS1 engine layout		Image:DSCF0386aca.JPG\|The LS1 engine layout
	Image:DSCF0826ACA.JPG\|Elliptical wing buck		Image:DSCF0826ACA.JPG\|Elliptical wing buck
	Image:4blade6k.~~jpg~~\|4 blade propeller bucks		Image:4blade6k.JPG\|4 blade propeller bucks
	</gallery>		</gallery>

wikademia>DAlgie: added 4 blade prop bucks picture

2008-02-18T01:22:23Z

added 4 blade prop bucks picture

← Older revision		Revision as of 01:22, 18 February 2008
Line 11:		Line 11:
	Image:DSCF0386aca.JPG\|The LS1 engine layout		Image:DSCF0386aca.JPG\|The LS1 engine layout
	Image:DSCF0826ACA.JPG\|Elliptical wing buck		Image:DSCF0826ACA.JPG\|Elliptical wing buck
			Image:4blade6k.jpg\|4 blade propeller bucks
	</gallery>		</gallery>