Pneumatic parachute deployment system
A pneumatic parachute deployment system is disclosed. In various embodiments, a pneumatic parachute deployment system as disclosed herein includes a bladder configured to control a parachute's expansion in at least one dimension, and an inflation mechanism configured to inflate the bladder. The bladder is inflated when the parachute is deployed, and in various embodiments may be used to speed deployment of the parachute and/or restrict the parachute to opening at least initially only to a limited extent.
1. A parachute deployment system, comprising:
a bladder configured to:
control a parachute's expansion in at least one dimension, wherein the bladder includes a plurality of inflatable sections at least two of which are unequal in length, wherein the bladder is initially attached to the parachute and constrains a radius of an opening of the parachute from exceeding a predetermined length, wherein the controlling of the parachute's expansion comprises to:
determine whether an aircraft utilizing the system is traveling at high speeds;
in response to a determination that the aircraft utilizing the system is traveling at high speeds:
continue to constrain the radius of the opening of the parachute;
while the radius is constrained, determine whether the aircraft utilizing the system is traveling at low speeds; and
in response to a determination that the aircraft utilizing the system is traveling at low speeds, release the parachute from the bladder to allow the radius of the opening of the parachute to exceed the predetermined length; and
an inflation mechanism configured to inflate the bladder.
2. The system of claim 1 , wherein an end of the bladder is in contact with the parachute.
3. The system of claim 1 , wherein an end of the bladder is attached to an aircraft and an opposite end of the bladder is in contact with the parachute.
4. The system of claim 1 , wherein the bladder is inflated when the parachute is deployed.
5. The system of claim 1 , wherein one or more additional bladders are used.
6. The system of claim 1 , wherein multiple bladders are interconnected and inflated from a common point.
7. The system of claim 1 , wherein the bladder exerts a force on a canopy of the parachute from within the canopy.
8. The system of claim 1 , wherein the bladder pushes tethers of the parachute out from a center of the parachute.
9. The system of claim 1 , wherein the bladder is folded inside of itself and the plurality of inflatable sections are defined by the folding of the bladder.
10. The system of claim 1 , wherein the bladder is configured to be inflated a section at a time.
11. The system of claim 9 , wherein a fold in the bladder is secured using a fixture that breaks when a predetermined amount of force is exerted on the fixture.
12. The system of claim 1 , wherein the bladder is packed or folded using multiple fixtures of different strengths.
13. The system of claim 1 , wherein the system performs actions based on flight conditions.
14. The system of claim 1 , wherein the bladder is used to increase a radius of an opening of the parachute quickly in the event the aircraft utilizing the system is traveling at low speeds.
15. The system of claim 1 , wherein the bladder is detached from the parachute in the event the aircraft utilizing the system is traveling at low speeds.
16. The system of claim 1 , wherein the bladder is attached to one or more tethers of the parachute, a canopy of the parachute, or an object attached to the parachute.
17. The system of claim 1 , wherein a rate of inflation of the bladder is determined based on flight conditions.