Automatic reserve or primary parachute activation device

• US 7,073,752 B2
• Filed: 10/25/2004
• Issued: 07/11/2006
• Est. Priority Date: 10/24/2003
• Status: Expired due to Fees

• Current Assignee: Cybernet Systems Corporation
• Original Assignee: Cybernet Systems Corporation
• Inventors: Voronka, Nestor, Jacobus, Charles J., Johnson, Derek M., Namineni, Pavan
• Primary Examiner(s): BAREFOOT, GALEN L
• Application Number:
  US10/972,703
• Publication Number:
  US 20050127243A1
• Time in Patent Office: 624 Days
• Field of Search: 244/142, 244/152, 244147-149, 438/119, 342/62, 701/3, 701/215
• US Class Current: 244/149
• CPC Class Codes: B64D 17/56 responsive to barometric pressure

Abstract

An electronic automatic reserve or primary parachute activation device incorporates partial or complete capture of freefaller or tethered parachute jumper kinematics to rapidly and reliable determine when to automatically activate deployment of the primary or reserve chute. This device uses means for directly measuring acceleration, velocity and/or position in addition to air pressure change to enable reliable detection of chute deployment conditions earlier than is possible with conventional pressure change activated automated activations devices. This is important when the activation decision must be made within 5–10 seconds of the initiation of the jump as is the case for military low altitude parachuting.

Claims

1. Apparatus for determining when to automatically deploy a primary or reserve parachute, comprising:

a plurality of accelerometers, each providing an output with respect to a different axis; and

a processor for integrating the outputs of the accelerometer to determine velocity; and

a mechanism for deploying the chute if the velocity exceeds a predetermined value.

2. The apparatus of claim 1, wherein the processor is further operative to determine the jumper'"'"'s position.

3. The apparatus of claim 1, further including one or more devices for estimating the jumper'"'"'s altitude based upon atmospheric pressure.

4. The apparatus of claim 1, wherein the accelerometers are MEMS accelerometers.

5. The apparatus of claim 1, further including plurality of gyroscopes, each providing an output with respect to a different axis;

and

wherein the processor is further operative to determine position and orientation as a function of the outputs of the gyroscopes.

6. The apparatus of claim 5, wherein the gyroscopes are MEMS gyroscopes.

7. The apparatus of claim 1, including 3 accelerometers oriented along 3 orthogonal axes.

8. The apparatus of claim 5, including 3 accelerometers oriented along 3 orthogonal axes.

12. The apparatus of claim 1, wherein the accelerometers are MEMS accelerometers.

13. The apparatus of claim 1, wherein the gyroscopes are MEMS gyroscopes.

9. Apparatus for determining when to automatically deploy a primary or reserve parachute, comprising:

a plurality of accelerometers, each providing an output with respect to a different axis; and

a plurality of gyroscopes, each providing an output with respect to a different axis;

a processor for determining position and orientation as a function of the outputs of the accelerators and gyroscopes,

a mechanism for deploying the chute if the velocity or position are outside a safe range.

10. The apparatus of claim 9, including 3 accelerometers oriented along 3 orthogonal axes.

11. The apparatus of claim 9, including 3 gyroscopes oriented along 3 orthogonal axes.