Resources Contact Us Home
Inverted airfoil pylon for an aircraft

Image Number 7 for United States Patent #7770841.

An aircraft including a wing and a pylon, wherein the pylon provides an airfoil inverted for an airfoil of the wing, and an improvement and method for improved flight dynamics for 20 and 30 Series LEARJET.RTM. is provided. The improvement includes an increased distance between a leading edge of a wing and an intake of an engine of the aircraft, which reduces drag and increases lift for improved flight dynamics of the aircraft. The inverted airfoil of the pylon negates an influence of the pylon on flight dynamics for improved overall flight dynamics of the aircraft. The method includes steps of removing an original engine from an original pylon, removing the original pylon from the fuselage of the aircraft, and mounting a new pylon in a new location adjacent to the fuselage, wherein the new location is aft of the original location.

  Recently Added Patents
Luggage locator
Wireless local area network for a concentrated photovoltaic system
Electromagnetic wave emission device
Systems and methods for design and construction of NMR transceiver circuits
System for purifying exhaust gas and method for controlling the same
Print preview display of confirmation page with main page based on selected display method
Piling light
  Randomly Featured Patents
Eject mechanism with grip in finisher
Control apparatus for an internal combustion engine
Use of a composition which regulates oxidation/reduction reactions intracellularly and/or extracellulary in a staining or sorting process
Intramedullary interlock screw
Oxidation of carbohydrates by means of peroxidases and nitroxy radicals
Disabling an implantable medical device
High-sensitivity capacitive oil deterioration and level sensor
Sequential fluid injection process for oil recovery from a gas cap
Multi-spot laser surgical apparatus and method
Method and apparatus for powder surface treating