Patent · US Active

Method of controlling a buoyancy system for an aircraft, a buoyancy system implementing said method, and an aircraft

US9004400B2 · kind B2 · utility

3Cited by
14References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 21, 2011
Grant dateApr 14, 2015
Priority date
Expiry dateApr 29, 2033

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C27/006
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A buoyancy system (2) includes at least one float (3), a deployment assembly (30) having at least one deployment member (34) for deploying the float (3), an engagement controller (5) which activates the deployment assembly (30), and at least two immersion sensors (20) for issuing an order for automatic deployment of the float (3) to the deployment assembly (30). The deployment assembly (30) is provided with a memory (31) containing a pre-established list of events. The deployment assembly (30) deploys each float (3) when a predetermined event occurs.

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