Patent · US Active

Ultra-rapid air vehicle and related method for aerial locomotion

US9079661B2 · kind B2 · utility

5Cited by
22References
13Claims
0Family size

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Key dates

Filing dateDec 20, 2010
Grant dateJul 14, 2015
Priority date
Expiry dateDec 7, 2031

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T90/40
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

The invention concerns an ultra-rapid air vehicle together with a method of aerial locomotion by means of an ultra-rapid air vehicle, where the air vehicle is propelled by a system of motors formed of turbojets (TB1, TB2), ramjets (ST1, ST2) and a rocket motor which can be made streamlined to reduce the drag of the base during the cruise phase, and where the vehicle has a gothic delta wing (A) fitted with moving fins (a1, a2) at both outer ends of the trailing edge of the delta wing (A).

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