Parachute deployment system using decoupled tow and release lines

US10407175B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10407175-B2
Application numberUS-201816103036-A
CountryUS
Kind codeB2
Filing dateAug 14, 2018
Priority dateOct 13, 2017
Publication dateSep 10, 2019
Grant dateSep 10, 2019

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

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.

First claim

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.

Assignees

Inventors

Classifications

  • B64D17/24Primary

    Rigging lines · CPC title

  • Deployment · CPC title

  • B64D17/725Primary

    by explosive means · CPC title

  • in association with aircraft, e.g. for braking thereof · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US10407175B2 cover?
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…
Who is the assignee on this patent?
Kitty Hawk Corp
What technology area does this patent fall under?
Primary CPC classification B64D17/24. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Sep 10 2019 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).