Parachute riser cradle
US-11970274-B2 · Apr 30, 2024 · US
US10407175B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10407175-B2 |
| Application number | US-201816103036-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 14, 2018 |
| Priority date | Oct 13, 2017 |
| Publication date | Sep 10, 2019 |
| Grant date | Sep 10, 2019 |
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Official abstract text for this publication.
A parachute system includes a release that detachably couples a self-propelled projectile and parachute canopy to each other. The release detaches the two from each other in response to a triggering of the release. There is also a first path between the release and a payload where the first path includes the parachute canopy and a suspension line between the parachute canopy and the payload. At least part of the suspension line is bound such that the first path is effectively shorter than a second path. In response to the first path being drawn taut, the suspension line becomes unbound so that the first path becomes effectively longer than the second path. In response to the second path being drawn taut after the suspension line becomes unbound, the release is triggered.
Opening claim text (preview).
What is claimed is: 1. A system, comprising: a parachute canopy; a tow line configured to detachably couple a self-propelled projectile and the parachute canopy via a pin, wherein the tow line is directly attached to the parachute canopy; the self-propelled projectile which in response to ignition of the self-propelled projectile is configured to: pull on the tow line and extract the parachute canopy from a container; and exert a greater pulling force on the tow line than on a release line; the release line configured to trigger a release of the pin in response to the self-propelled projectile pulling on the release line; and the pin configured to releasably couple the self-propelled projectile and the parachute canopy. 2. A system, comprising: a parachute canopy; a tow line configured to detachably couple a self-propelled projectile and the parachute canopy via a pin; the self-propelled projectile which in response to ignition of the self-propelled projectile is configured to pull on the tow line and extract the parachute canopy from a container; a bundled and shorter line configured to become an unbundled and longer line in response to the self-propelled projectile pulling on the tow line, wherein unbundling and lengthening of the shorter line causes the self-propelled projectile to exert a greater pulling force on the tow line than a release line; the release line configured to trigger a release of the pin in response to the self-propelled projectile pulling on the release line; and the pin configured to releasably couple the self-propelled projectile and the parachute canopy. 3. The system recited in claim 1 , wherein: the pin includes a first component and a second component which are secured against each other using a restrainer; the self-propelled projectile is configured to pull on the release line and cause the restrainer to break which in turn permits the first component and the second component to separate from each other; and the separation of the first component and the second component triggers the release of the pin. 4. The system recited in claim 1 , wherein: the pin includes a first component and a second component which are secured against each other using a restrainer; the restrainer includes one or more of the following: a zip tie, a line, or fabric; the self-propelled projectile is configured to pull on the release line and cause the restrainer to break which in turn permits the first component and the second component to separate from each other; and the separation of the first component and the second component triggers the release of the pin. 5. A method, comprising: providing a parachute canopy; providing a tow line configured to detachably couple a self-propelled projectile and the parachute canopy via a pin, wherein the tow line is directly attached to the parachute canopy; providing the self-propelled projectile which in response to ignition of the self-propelled projectile is configured to: pull on the tow line and extract the parachute canopy from a container; and exert a greater pulling force on the tow line than on a release line; providing the release line configured to trigger a release of the pin in response to the self-propelled projectile pulling on the release line; and providing the pin configured to releasably couple the self-propelled projectile and the parachute canopy. 6. The method recited in claim 5 , wherein there is a bundled and shorter line configured to become an unbundled and longer line in response to the self-propelled projectile pulling on the tow line, wherein unbundling and lengthening of the shorter line causes the self-propelled projectile to exert a greater pulling force on the tow line than the release line. 7. The method recited in claim 5 , wherein: the pin includes a first component and a second component which are secured against each other using a restrainer; the self-propelled projectile pulling on the release line causes the restrainer to break which in turn permits the first component and the second component to separate from each other; and the separation of the first component and the second component triggers the release of the pin. 8. The method recited in claim 5 , wherein: the pin includes a first component and a second component which are secured against each other using a restrainer; the restrainer includes one or more of the following: a zip tie, a line, or fabric; the self-propelled projectile pulling on the release line causes the restrainer to break which in turn permits the first component and the second component to separate from each other; and the separation of the first component and the second component triggers the release of the pin.
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