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
Semiconductor apparatus
Image heating device
Methods and apparatus for adapting network characteristics in telecommunications systems
Cycloalkylamine substituted isoquinoline derivatives
Global codebook for coordinated multi-point processing
Navigating applications using side-mounted touchpad
Support core for cold shrink tube
  Randomly Featured Patents
Conveyor belt cleaner scraper blade with sensor and method of manufacture
Moving device as well as a component placement device provided with such a moving device
Voice actuated heating apparatus
Flow differentiation scheme for magnetic resonance angiography
Slide drive apparatus and slide drive method for pressing machine
System for, and method of, selectively providing the operation of toy vehicles
Display apparatus and method for controlling backlight that can reduce image distortion due to local dimming
Imaging apparatus and method for cleaning transfer/conveyer means
Effectors of dipeptidyl peptidase IV for topical use
Washing apparatus