Earthly Dynamics, LLC

United States of America

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1-4 of 4 for Earthly Dynamics, LLC Sort by
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2022 1
Before 2021 3
IPC Class
B64D 17/34 - Load suspension adapted to control direction or rate of descent 3
B64D 17/02 - Canopy arrangement or construction 2
B64D 17/18 - Vent arrangement or construction 2
B64D 17/22 - Load suspension 2
B64D 17/24 - Rigging lines 1
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Found results for  patents

1.

One-time flare mechanism

      
Application Number 16055122
Grant Number 11434011
Status In Force
Filing Date 2018-08-05
First Publication Date 2022-09-06
Grant Date 2022-09-06
Owner Earthly Dynamics, LLC (USA)
Inventor
  • Costello, Mark F
  • Ward, Michael Brian

Abstract

A one-time flare mechanism system for use with an aerial payload system is describe which uses minimal actuation force to produce a reliable flare with minimal shock to the payload, parafoil and rigging.

IPC Classes  ?

  • B64D 17/34 - Load suspension adapted to control direction or rate of descent
  • B64D 17/38 - Releasable fastening devices between parachute and load or pack

2.

One-time flare mechansim

      
Application Number 14923619
Grant Number 10137995
Status In Force
Filing Date 2015-10-27
First Publication Date 2018-11-27
Grant Date 2018-11-27
Owner Earthly Dynamics, LLC (USA)
Inventor
  • Costello, Mark F
  • Ward, Michael Brian
  • Scheuermann, Edward James

Abstract

A one-time flare mechanism system for use with an aerial payload system is described which uses minimal actuation force to produce a reliable flare with minimal shock to the payload, parafoil and rigging.

IPC Classes  ?

3.

In canopy bleed air actuator with mesh vent

      
Application Number 14709606
Grant Number 09573692
Status In Force
Filing Date 2015-05-12
First Publication Date 2017-02-21
Grant Date 2017-02-21
Owner Earthly Dynamics, LLC (USA)
Inventor
  • Costello, Mark F
  • Ward, Michael Brian
  • Scheuermann, Edward James
  • Bergeron, Keith
  • Shurtliff, Michael Wayne
  • Noetscher, Gregory Michael

Abstract

A system is described to control the flight path of a parafoil. The physical control mechanism is a series of actuators embedded within the parafoil canopy that open a series of meshed venting systems in the upper surface of the parafoil canopy. Opening and closing the meshed venting system changes the forces and moments acting on the parafoil canopy in a consistent manner such that it can be used for flight control. The meshed venting system includes an internal sealing flap and a mesh member.

IPC Classes  ?

  • B64D 17/34 - Load suspension adapted to control direction or rate of descent
  • B64D 17/22 - Load suspension
  • B64D 17/18 - Vent arrangement or construction
  • B64D 17/02 - Canopy arrangement or construction

4.

In canopy bleed air actuator

      
Application Number 14479530
Grant Number 09428277
Status In Force
Filing Date 2014-09-08
First Publication Date 2016-08-30
Grant Date 2016-08-30
Owner Earthly Dynamics, LLC (USA)
Inventor
  • Costello, Mark F
  • Bergeron, Keith
  • Shurtliff, Michael Wayne
  • Noetscher, Gregory Michael
  • Ward, Michael Brian
  • Scheuermann, Edward James

Abstract

A system is described to control the flight path of a parafoil. The physical control mechanism is a series of actuators embedded within the parafoil canopy that open a series of holes via slits in the upper surface of the parafoil canopy. Opening and closing the holes changes the forces and moments acting on the parafoil canopy in a consistent manner such that it can be used for flight control. The embedded actuator is attached to a structural cell wall of the parafoil canopy. A control line from the actuator extends through a ring attached to the leading edge of the slit in the upper surface of the parafoil canopy and back down to the lower surface of the parafoil canopy along the opposite side non-structural cell wall.

IPC Classes  ?

  • B64D 17/34 - Load suspension adapted to control direction or rate of descent
  • B64D 17/22 - Load suspension
  • B64D 17/18 - Vent arrangement or construction
  • B64D 17/02 - Canopy arrangement or construction