Patent · US Active

Parachute architecture for low-altitude VTOL aircraft

US11273919B2 · kind B2 · utility

0Cited by
12References
19Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 4, 2019
Grant dateMar 15, 2022
Priority date
Expiry dateNov 3, 2040

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D17/725
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

In an embodiment, a system to deploy a plurality of parachutes includes a plurality of parachute canopies each packed in a canister, a plurality of rockets adapted to extract an associated canopy from the canister, and a controller. The controller is configured to determine that an aircraft is at least one of: in a hover mode of operation and a forward flight mode of operation. In response to the determination that the aircraft is in the hover mode of operation, the controller applies a hover deployment sequence including by instructing the plurality of parachutes to deploy substantially simultaneously. In response to the determination that the aircraft is in the forward mode of operation and above a threshold airspeed, the controller applies a forward deployment sequence including by instructing the plurality of parachutes to deploy in a predefined sequence.

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