CarterCopter
{{Short description|Experimental autogyro}}
{{Infobox aircraft
|name=CarterCopter
|image=
|caption=
|type=Experimental compound autogyro
|manufacturer=Carter Aviation Technologies
|first_flight=24 September 1998"CarterCopter". [http://aerofiles.com/_ca.html American airplanes]. www.aerofiles.com. Accessed on 5 October 2008.
|number_built=1
|developed_into=Carter PAV
}}
The CarterCopter is an experimental compound autogyro developed by Carter Aviation Technologies in the United States to demonstrate slowed rotor technology. On 17 June 2005, the CarterCopter became the first rotorcraft to achieve mu-1 (μ=1), an equal ratio of airspeed to rotor tip speed,{{usurped|1=[https://web.archive.org/web/20110516134228/http://www.cartercopters.com/mu-1.html Significance of μ-1 and the Technical Issues Involved]}}, Carter Aviation Technologies. but crashed on the next flight and has been inoperable since.[http://articles.janes.com/articles/Janes-All-the-Worlds-Aircraft/Carter-CarterCopter-CC1-United-States.html Carter CarterCopter CC1 (United States), Aircraft - Rotary-wing - Civil] Jane's all the world's aircraft, 28 June 2007. Retrieved: 19 February 2012. It is being replaced by the Carter Personal Air Vehicle.
Design and development
{{external media
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| image1 =[http://www.nerocam.com/Oshkosh/Pictures/CarterCopter.jpg 1998 version]
| image2 =[http://www.gizmag.com/go/2504/picture/4014/ Gallery of 10 photos]
| image3= [http://autogire.nuxit.net/Galerie_photos/Photos/cartercopter.gif CAD drawing]
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The CarterCopter is a pusher configuration autogyro with wings and a twin boom tail, intended as a prototype and a technology demonstrator.{{Cite web |url=http://www.cartercopters.com/cctd.html |title=CarterCopter Technology Demonstrator |access-date=2008-09-29 |archive-url=https://web.archive.org/web/20091226130115/http://www.cartercopters.com/cctd.html |archive-date=2009-12-26 |url-status=usurped }} The rotor is a two-bladed design weighted with {{convert|55|lb|kg}} depleted uranium at each tip, and it is mounted on a tilting mast, allowing the wing to stay at optimum wing efficiency at all speeds.
It is an all-composite design[http://www.flightglobal.com/pdfarchive/view/2001/2001%20-%201272.html Flight International 10 - 16 April 2001 General Aviation p28] with a hull pressurized up to
0.69 bar.
The tricycle undercarriage is retractable, and has a large travel to allow for landing at up to 20 ft/sec without bounce. The aircraft had been modified and rebuilt after an accident (a gear-up landing) in 2003.O'Brien, Kevin "Hognose". [http://www.aero-news.net/index.cfm?do=main.textpost&id=24af6d8c-b312-42f4-a84a-49b362f6dba0 CarterCopter Advances Towards Mu>1.0 (Part 1)] [http://www.aero-news.net/index.cfm?do=main.textpost&id=0967ae9e-0780-4dc2-8519-5b7960ac6e3d (Part 2)] Aero-News, April 2004. Accessed: 6 September 2011.
NASA had funded $1 million of the development using three research grants, and the aircraft managed to accomplish at least one of NASA's five goals.Howard, Scripps. [http://chronicle.augusta.com/stories/2000/12/22/tec_303243.shtml Gyroplane adds sci-fi touch to air travel] The Augusta Chronicle, 22 December 2000. Accessed: 25 September 2011. [https://news.google.com/newspapers?nid=2026&dat=20001221&id=hsMjAAAAIBAJ&sjid=LdEFAAAAIBAJ&pg=1402,2693187 Mirror]
=Concept=
The CarterCopter concept is a gyrocopter with an unusually stiff, relatively heavy rotor, supplemented with conventional wings. At low speed, the vehicle flies as a gyrocopter, and can pre-spin the rotor for a vertical takeoff and very brief hover (about 5 seconds),Henry Farkas and Claudius Klimt. [http://www.swaviator.com/html/issueMJ02/carter5602.html "The Next Big Thing in Aviation"] SW Aviator Magazine. Retrieved: 1 August 2012. and can land more or less vertically. Several technical challenges make flying a slow rotor difficult, but rotor stability is achieved through the combination of the rotor tip weights' location ahead of the blade center line (forward center of gravity) and the center of lift aft of the blade center line.
At high speed (above about 100 mph) the aircraft flies mostly using the fixed wings, with the rotor simply windmilling. The rotor spins with a tip speed below airspeed, which means that the retreating blade flies completely stalled. On a helicopter this would cause massive lift dissymmetry and insoluble control issues but the fixed wings keep the aircraft in the air and stable.
The low rotation speed and flat feathering of the rotor means that it causes little drag, and the company claims that the aircraft would be potentially able to leverage the advantages of fixed wings as well as gyrocopters, giving almost all the capabilities of helicopters (except hovering) but with a relatively simple mechanical system. Carter Aviation also claims the system is safer than a typical fixed-wing aircraft, and others{{Citation needed|date=September 2011}} have remarked that the design is much safer, much less complex and less expensive than a helicopter, a tilt-rotor or the Boeing X-50 Dragonfly Canard Rotor/Wing.{{usurped|1=[https://web.archive.org/web/20110516142610/http://www.cartercopters.com/pr_2009-07-30c.html SAFER by DESIGN]}}, Press Release, July 2009, Carter Aviation Technologies.{{usurped|1=[https://web.archive.org/web/20110708122446/http://www.cartercopters.com/popular_mechanics_award.html Popular Mechanic's Design and Engineering 2000 Award]}}, 14 December 2000, Carter Aviation Technologies. The CarterCopter should be capable of higher airspeeds now only achievable by fixed-wing aircraft, but also able to land like an autogyro in any small area in an emergency.
=Takeoff=
At takeoff the pilot angles the top rotor flat (zero angle of attack) and spins it to very high speed (between 365 and 425 rpm).Charnov, Bruce H. [https://www.amazon.co.uk/gp/reader/1567205038/ref=sib_fs_bod?ie=UTF8&p=S00W&checkSum=IzFSxnzYaApBvgB2GYXMsZiIKMtOrnddijM3FCLVXx4%3D#reader-link From Autogiro to Gyroplane: The Amazing Survival of an Aviation Technology] page 329. From 2003. Retrieved August 2011. {{ISBN|978-1-56720-503-9}} The rotor is then disconnected from the engine and the angle of attack of the main rotor blades is increased suddenly so that the vehicle leaps into the air. The aircraft's main rotor has enough momentum due to heavy counterweights in the tips that it can hover for a short time safely. The pilot then applies full power to the rear pusher propeller and the vehicle starts to move forwards. As it does so, air is forced through the main rotor, spinning it faster and generating more lift. The vehicle climbs into the air, flying as an autogyro.
=Cruising=
Once the CarterCopter gets up to a forward speed of about {{convert|90|mph}}, its stubby, lightweight wings provide most of the lift. The pilot can then flatten the angle of attack of the main rotor so it produces very little lift, dramatically reducing the amount of induced drag created by the rotor. Although the rotor is unused at high speed, the rotor is kept spinning at about 80 RPM as the rotation keeps the rotor stretched, preventing excessive flapping.{{usurped|1=[https://web.archive.org/web/20091124191031/http://www.cartercopters.com/faq-general.html FAQ 3]}} Carter Aviation Technologies[http://articles.janes.com/articles/Janes-All-the-Worlds-Aircraft/Carter--CarterCopters-LLC-United-States.html Carter - CarterCopters LLC (United States), Aircraft - Manufacturer] Jane's all the world's aircraft, 10 September 2008. Retrieved: 19 February 2012.
Normally a helicopter or gyrocopter cannot fly forward at the same speed as or faster than its rotor tip speed. This is because the low airspeed of the retreating rotor blade would cause retreating blade stall, whilst the advancing rotor blade would be traveling at twice the speed of the aircraft, producing uncontrollable flight due to dissymmetry of lift.
However, with the CarterCopter, the fixed wings provide the lift required to remain aloft. Since the rotor is unloaded, the aerodynamic forces on the rotor are very minor. This means that a CarterCopter can theoretically fly much faster than the tip speed of the rotor. The rotors would still experience flapping as they rotate due to dissymmetry of lift between the two sides of the vehicle, but Carter Aviation claims this is manageable.
The claimed theoretical maximum speed of a CarterCopter type aircraft is around 500 mph (800 km/h),{{usurped|1=[https://web.archive.org/web/20110708122453/http://www.cartercopters.com/pr_1999-06-11.html PRESS RELEASE, June 11, 1999]}}, Carter Aviation Technologies. which would be about twice as fast as the helicopter flight airspeed record.[http://www.fai.org/fai-record-file/?recordId=11659 Rotorcraft World Records] {{webarchive|url=https://web.archive.org/web/20131203033038/http://www.fai.org/fai-record-file/?recordId=11659 |date=2013-12-03 }}. Fédération Aéronautique Internationale (FAI). Note search under E-1 Helicopters and "Speed over a straight 15/25 km course".
=Achievements=
{{external media
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| image1 =[http://media.defenseindustrydaily.com/images/AIR_Helicopter_Mu_Diagram_lg.gif Diagram and formula of μ (Mu)]
}}
The prototype's engine was normally aspirated, and hence limited to just 320 hp (240 kW) and the aircraft went about 173 mph (270 km/h);Wise, Jeff. [http://www.popsci.com/military-aviation-space/article/2005-01/jay-carter-jr "Jay Carter, Jr."] Popular Science, 2005. Retrieved: 14 July 2012. [https://books.google.com/books?id=wgKpEb86UPIC&pg=PA63 Magazine] which is still ~40% faster than a conventional autogyro but slower than gyrodynes of the 1950s. A custom gyroplane can go 168.29 km/h (104.6 mph),Cartier, Kerry. "[http://www.pra.org/index.php?option=com_content&view=article&id=120:faqs&catid=61:Gyroplanes&Itemid=110 Gyroplane FAQs] {{webarchive|url=https://web.archive.org/web/20080502104312/http://www.pra.org/index.php?option=com_content&view=article&id=120:faqs&catid=61:Gyroplanes&Itemid=110|date=2008-05-02}}." Popular Rotorcraft Association, 14 February 2008. Retrieved: 3 November 2010. and Carter says the Carter Personal Air Vehicle goes {{convert|200|mph|kn+km/h}}.Jon Tatro. "{{usurped|1=[https://web.archive.org/web/20131111111351/http://www.cartercopters.com/system/sdocs/14/original/Carter%20Aviation%20Press%20Release%20-%202013-11-08%20(Mu%201).pdf?1383946559 Carter Aviation repeats historic mark - breaking the mu-1 barrier]}}" Carter, November 8, 2013. Accessed: November 11, 2013.
At 4,000 lbs weight, the CCTD can climb 750 fpm.
From 1999 to 2001 there were 4 recorded instances of non-fatal crashes,[http://www.pra73.net/NewslettersPDF/PrintJuly2005_NL.pdf June 2005 PRA 73 meeting] {{webarchive|url=https://web.archive.org/web/20110724020421/http://www.pra73.net/NewslettersPDF/PrintJuly2005_NL.pdf |date=2011-07-24 }} page 4, PRA73 website July 2005. Retrieved 7 August 2010.[https://www.ntsb.gov/ntsb/brief.asp?ev_id=20001212X20241&key=1 Probable cause] NTSB, 6 April 2001. Retrieved: 7 August 2010."[http://www.aero-news.net/index.cfm?do=main.textpost&id=bc60fe4c-9d51-4532-a545-560aee19b984 Group to Restore Carter Copter Prototype]" Aero-News, June 5, 2003. Accessed: April 10, 2014. while Carter claims 10 accidents over 7 years,{{usurped|1=[https://web.archive.org/web/20091124191031/http://www.cartercopters.com/faq-general.html FAQ 19]}} Carter Aviation Technologies all non-fatal.Norris, Guy. [http://www.flightglobal.com/articles/2005/07/12/200217/carter-claims-mu-record-but-suffers-another-crash.html Carter claims Mu record, but suffers another crash] Flight Global, 12 July 2005. Accessed: 18 January 2011. [http://www.flightglobal.com/news/articles/carter-claims-mu-record-but-suffers-another-crash-200217/ Mirror]
Test pilot Larry Neal claimed that the CarterCopter is a challenge to fly because it is a combination of helicopter, autogyro and fixed-wing aircraft.Neal, Larry. {{usurped|1=[https://web.archive.org/web/20080513073555/http://www.cartercopters.com/files/cc_article.pdf "Pilot Report: CarterCopters® Technology Demonstrator"]}} [http://www.pra.org Popular Rotorcraft Association] {{Webarchive|url=https://web.archive.org/web/20110207173218/http://pra.org/ |date=2011-02-07 }} / Carter Aviation, March/April 2002. Retrieved: 14 July 2012.
The CarterCopter achieved its maximum mu (mu is the ratio of airspeed to rotor tip speed)[http://www.flightglobal.com/articles/2005/07/12/200219/what-is-the-mu-1-barrier.html What is the Mu-1 barrier?] Flight Global, 12 July 2005. Accessed: 18 January 2011.{{usurped|1=[https://web.archive.org/web/20091124191031/http://www.cartercopters.com/faq-general.html FAQ 5]}} Carter Aviation Technologies of 1.0 for a brief moment on June 17, 2005, the first time any rotary aircraft has reached this level. CarterCopter's pilot claimed that there was no great drama, and mu 1 was reached accidentally due to normal variations in rotor RPM (at 107 rpm) and vehicle airspeed; the pilot described it as 'smooth' with no significant vibration.Anderson, Rod. [http://issuu.com/contact.magazine/docs/issue_83_carter_copter The CarterCopter and its legacy] Issue 83, Contact Magazine, 30 March 2006. Accessed: 11 December 2010. [http://contactmagazine.com/Issue83/Issue_83__3-4.pdf Mirror] The tests were performed under a US Army contract. Carter says they repeated mu-1 with the PAV in 2013.
However, on the next test flight the same day in 2005, the CarterCopter made a hard landing (crashed),[https://www.ntsb.gov/aviationquery/brief.aspx?ev_id=20050802X01139&key=1 Probable cause] NTSB, 25 July 2007. Retrieved: 7 August 2010. causing significant damage, but the pilots were unhurt. The crash was caused by failing propeller bolts which damaged wires controlling the rotor. The propeller was designed by Carter, and was an 8 ft scimitar controllable-pitch propeller weighing 15 lbs and had a thrust of 1850 lbf.Jeff Lewis and Claudius Klimt. [http://issuu.com/contact.magazine/docs/issue_83_carter_copter The CarterCopter and its legacy: Carter's high performance, hollow-blade propellers] pages 11-15. Issue 83, Contact Magazine, 30 March 2006. Accessed: 18 April 2015. It was initially believed that the CarterCopter was unrepairable; later inspection showed that it could be repaired, but the company chose to work on a small open wingless autogyro demonstrator instead.{{usurped|1=[https://web.archive.org/web/20110614075914/http://www.cartercopters.com/weekly_update_archive_2005_3.html Archive 2005]}} Carter Aviation Technologies, 25 July 2005. Retrieved: 7 August 2010. Also later in 2005 and using lessons learned from the CarterCopter, design began on the subsequent compound aircraft, the Carter PAV,{{usurped|1=[https://web.archive.org/web/20110614075934/http://www.cartercopters.com/weekly_update_archive_2006_1.html Archive 2006]}} Carter Aviation Technologies, 2 January 2006. Retrieved: 7 August 2010. "For the past several months, Carter has been designing a new aircraft""[http://www.texomashomepage.com/story/cartercopter-prototype-in-the-works/d/story/uOmm7icg60K07MJ3plwu3A CarterCopter prototype in the works] {{webarchive|url=https://web.archive.org/web/20141224223303/http://www.texomashomepage.com/story/cartercopter-prototype-in-the-works/d/story/uOmm7icg60K07MJ3plwu3A |date=2014-12-24 }}" Texomas, 20 December 2006. Accessed: 26 January 2014. which flew in 2011.Paur, Jason. [https://www.wired.com/autopia/2011/01/new-autogyro-is-an-alternative-to-flying-cars/ New autogyro is an alternative to flying cars] {{webarchive|url=https://web.archive.org/web/20140304234500/http://www.wired.com/autopia/2011/01/new-autogyro-is-an-alternative-to-flying-cars/ |date=March 4, 2014 }} Wired (magazine), 21 January 2011. Accessed: 21 January 2011.
The company claims that the testing indicated{{usurped|1=[https://web.archive.org/web/20081002031534/http://www.cartercopters.com/cctd_flight_data.html CCTD flight test data]}} Carter Aviation Technologies. Retrieved: 7 August 2010.{{Citation needed|date=March 2010}}
that the vehicle architecture could potentially outperform helicopters on every dimension except sustained hover, and should be much cheaper to buy and maintain. The company also claims that it also very nearly matches the L/D of fixed wing General Aviation aeroplanes at cruise speed - but with near-vertical takeoff and landing. However, jump take-off ability using the stored rotor energy has never been shown to more than about 16 feet with the wing attached.
NASA has made computer models of the CarterCopter rotor above mu=1 and up to 400 knots airspeed.Floros, Matthew W. & Johnson, Wayne. [http://halfdome.arc.nasa.gov/publications/files/Floros_%20JAHS2009.pdf "Performance Analysis of the Slowed-Rotor Compound Helicopter Configuration"] {{webarchive|url=https://web.archive.org/web/20111017120736/http://halfdome.arc.nasa.gov/publications/files/Floros_%20JAHS2009.pdf |date=2011-10-17 }} Journal of the American Helicopter Society
Specifications
{{Aircraft specs
|ref=Aviation Week,Warwick, Graham. [http://www.aviationweek.com/aw/blogs/aviation_week/on_space_and_technology/index.jsp?plckController=Blog&plckBlogPage=BlogViewPost&newspaperUserId=a68cb417-3364-4fbf-a9dd-4feda680ec9c&plckPostId=Blog%3aa68cb417-3364-4fbf-a9dd-4feda680ec9cPost%3a6b70a5dd-92ff-4169-87fb-2b34b4658ff1&plckScript=blogScript&plckElementId=blogDest Carter flies VTOL hybrid] Aviation Week, 26 January 2011. Accessed: 27 January 2011.
American Helicopter Society,Matthew W. Floros & Wayne Johnson. [https://apps.dtic.mil/sti/pdfs/ADA529853.pdf Stability Analysis of the Slowed-Rotor Compound Helicopter Configuration] p5, American Helicopter Society, June 2004. Accessed: 3 March 2012.
CarterCopters.com{{cite web|url=http://www.cartercopters.com/first_proto.html|title=CarterCopter CCTD|accessdate=12 April 2012|publisher=Carter Aviation Technologies|url-status=usurped|archiveurl=https://web.archive.org/web/20120414224840/http://www.cartercopters.com/first_proto.html|archivedate=14 April 2012}}
|prime units?=kts
|capacity=5 including flight crew
|span ft=32
|aspect ratio=13.4
|airfoil=NACA 65 series
|empty weight lb=2000
|max takeoff weight lb=4200
|fuel capacity={{convert|800|lb|kg|abbr=on|0}}
|eng1 number=1
|eng1 name= GM
|eng1 type=V-6 crate engine
|eng1 kW=
|eng1 hp=350
|eng1 kn=
|eng1 lbf=
|prop blade number=2
|prop name=Carter scimitar controllable-pitch propeller
|prop dia ft=8
|rot number=1
|rot dia ft=32
|rot area sqft=804.35
|cruise speed kmh=230
|cruise speed note=at sea level
:::projected: {{convert|400|mph|km/h|abbr=on|0}} at {{convert|50,000|ft|m|abbr=on|0}}
|range miles=2500
|range note=with reserve, {{convert|800|lb|kg|abbr=on|0}} fuel load
:::{{convert|1,000|mi|km|abbr=on|0}} with reserve, {{convert|400|lb|kg|abbr=on|0}} fuel load
|ceiling ft=10000
|lift to drag=7 at {{convert|170|mph|km/h|abbr=on|0}}
}}
See also
{{aircontent
|see also=
- Sikorsky S-72 - compound helicopter with rigid stoppable rotor
- McCulloch J-2 - an autogyro with clutched rotor
- McDonnell XV-1
|related=
|similar aircraft=
}}
References
{{Reflist}}
External links
- Official website {{usurped|1=[https://web.archive.org/web/19971014121738/http://www.cartercopters.com/ Carter Aviation Technologies]}}
- [https://web.archive.org/web/20100114140713/http://www.pilotbug.com/?tag=cartercopter PilotBug article]
- [http://findarticles.com/p/articles/mi_qa3897/is_200212/ai_n9149827/ Flight Journal article from 2002]
- [https://web.archive.org/web/20100102044649/http://www.internetage.com/cartercopters/ Fan site]
{{Helicopters and rotorcraft}}