7/31/2023 0 Comments Carter copter![]() ![]() It also achieved a speed of 174 kn (322 km/h 200 mph), and the rotor was slowed down to 113 rpm. Īccording to Carter, the PAV reached Mu-1 on 7 November 2013. Ĭarter says that the PAV has a lift to drag ratio of 10–15, and reached an advance ratio of 0.85 in 2012. The previous CarterCopter was designed using a flight simulator. Carter views the lack of a PAV flight simulator as a mistake, and attempts to build one. Carter received funding from the Wichita Falls Economic Development Corporation in 2010 to complete the PAV. Īs of June 2012, development of the PAV is a year behind schedule due to various technical problems, and a delay of a further year was caused by rotor RPM software control issues. It flew a few hours at a time, but its flight certificate restricted it to within 5 miles (8.0 km) of Olney. The PAV flew traffic patterns with wings at Olney in January 2012, and has since flown winged test flights. There are some electrical issues with the aircraft, and it is not in volume production. Ĭarter stated that the PAV performed its first zero-roll jump take-off on 18 January 2011, to a height of 120 feet (37 m). The first flight occurred on 5 January 2011 at Olney without wings and lasted 36 minutes, which qualified Carter for a milestone payment. Larry Neal was also one of the pilots of the CarterCopter at Olney in 2005. The PAV was taxi tested in autumn of 2010 at Olney Airport after FAA Special Airworthiness Certificate on 27 July 2010, and performed traffic pattern movement on 2 December 2010, piloted by Larry Neal at the controls and co-pilot Robert Luna. In 2014, Carter said they bought back the license from AAI and is seeking production partners outside USA, hoping for production 3–5 years later. ![]() Usually a CDR is performed before a vehicle is built. "Critical Design Review" (CDR) for AAI Corporation was performed around January 2010 when the prototype was already being built. The first product in the AAI agreement was to be an autonomous slowed rotor/compound (SR/C) aircraft based on the Carter Personal Air Vehicle. The agreement committed CarterCopters to developing the technology to maturity, in exchange for exclusive rights to develop UAVs for the next 40 years. On 16 November 2009, the AAI Corporation (a division of Textron) signed a 40-year exclusive license agreement with the company concerning all unmanned aircraft systems, one of which was intended to deliver 3,000 pounds (1,400 kg) of cargo similar to the unmanned Kaman K-MAX, but over a future range of 1,300 nautical miles (2,400 km) compared to the demonstrated 150 nautical miles (280 km) or more of the K-MAX. Several changes and development problems occurred along the way twin boom was deemed unnecessary, so a single boom was constructed, and flaws in rotor blades and hub were revealed during testing and then corrected. ![]() When the CarterCopter was damaged in 2005 due to a gear-up landing caused by pilot error, the cost of repair was deemed higher than the cost of making a new aircraft with the added benefit of incorporating lessons learned from the first aircraft. Heavy weights (75 pounds or 34 kilograms each) are placed in the rotor tips to enhance rotational energy and to reduce flapping. The design has an unpowered rotor mounted on top of the fuselage, wings like a conventional fixed-wing aircraft mounted underneath, and a controllable pitch pusher propeller at the rear of the fuselage. ![]() The Carter PAV ( Personal Air Vehicle) is a two-bladed, compound autogyro developed by Carter Aviation Technologies to demonstrate slowed rotor technology. ![]()
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