Patent · US Active

Vortex generators to improve performance of flush air inlets

US8544799B2 · kind B2 · utility

8Cited by
2References
10Claims
0Family size

Assignee

Inventors

Key dates

Filing dateFeb 15, 2008
Grant dateOct 1, 2013
Priority date
Expiry dateNov 27, 2029

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/10
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A VG (vortex generator) placed on a body surface (aircraft or similar), upstream of a flush air inlet, in order to generate vortexes that will sweep away the boundary layer in front of the inlet, inducing a downwash effect in the freestream airflow, such VG consisting of a wing (1) parallel to the surface of the aircraft or similar, said wing supported by a support (2) or a pair of supports (2) such as fins disposed in a divergent angle; the VG considerably improves the inlet ram recovery ratio and the mass flow ratio of the air inlet and it has an effect of reduction of the VG boundary layer thickness, thus reducing the distortion level of the flow entering the inlet as the inlet ingests more freestream air and the vortexes are not ingested by the inlet.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.