Propellant grain for optimizing the interior ballistic performance of a weapon
A method of manufacturing and optimizing energetic propellant grains includes generating an optimal surface area to mass fraction burned ratio profile for a predetermined solid structure including propellant grains; using the profile as a target function of a topological optimization process to gene...
Gespeichert in:
Hauptverfasser: | , , , , |
---|---|
Format: | Patent |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | |
---|---|
container_issue | |
container_start_page | |
container_title | |
container_volume | |
creator | Gaynor, Andrew T Robinette, Eric J Schmidt, John R Conroy, Paul J Wildman, Raymond A |
description | A method of manufacturing and optimizing energetic propellant grains includes generating an optimal surface area to mass fraction burned ratio profile for a predetermined solid structure including propellant grains; using the profile as a target function of a topological optimization process to generate a 3D form of a propellant grain; developing a negative of the 3D form of the propellant grain; mixing and densifying the negative with an energetic material in an uncured form in a mixer to create a structure including the energetic material and embedded negative; and solvating the negative from the structure, wherein the negative comprises a 3D propellant grain. The developing of the negative of the 3D form of the propellant grain may occur using a predetermined material in an additive manufacturing process. The negative may be soluble in the predetermined material, and the energetic material may be insoluble in the predetermined material. |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US10906848B2</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US10906848B2</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US10906848B23</originalsourceid><addsrcrecordid>eNqNyj0KAkEMQOFtLES9QzyAsP4ga6soViKo9RKHzBqYTcJMQPD0buEBrB48vnF1uWY1SgnFocvIAlEzqDn3_GHpwF8ELE6Zh__ElLg4BzDKA-xRAoFGQHgTmsq0GkVMhWa_Tqr56Xg_nBdk2lIxDCTk7eO2rHf1ttk0-9X6H_MFW6s3Kg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Propellant grain for optimizing the interior ballistic performance of a weapon</title><source>esp@cenet</source><creator>Gaynor, Andrew T ; Robinette, Eric J ; Schmidt, John R ; Conroy, Paul J ; Wildman, Raymond A</creator><creatorcontrib>Gaynor, Andrew T ; Robinette, Eric J ; Schmidt, John R ; Conroy, Paul J ; Wildman, Raymond A</creatorcontrib><description>A method of manufacturing and optimizing energetic propellant grains includes generating an optimal surface area to mass fraction burned ratio profile for a predetermined solid structure including propellant grains; using the profile as a target function of a topological optimization process to generate a 3D form of a propellant grain; developing a negative of the 3D form of the propellant grain; mixing and densifying the negative with an energetic material in an uncured form in a mixer to create a structure including the energetic material and embedded negative; and solvating the negative from the structure, wherein the negative comprises a 3D propellant grain. The developing of the negative of the 3D form of the propellant grain may occur using a predetermined material in an additive manufacturing process. The negative may be soluble in the predetermined material, and the energetic material may be insoluble in the predetermined material.</description><language>eng</language><subject>CHEMISTRY ; EXPLOSIVES ; EXPLOSIVES OR THERMIC COMPOSITIONS ; MANUFACTURE THEREOF ; MATCHES ; METALLURGY ; USE OF SINGLE SUBSTANCES AS EXPLOSIVES</subject><creationdate>2021</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210202&DB=EPODOC&CC=US&NR=10906848B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25555,76308</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210202&DB=EPODOC&CC=US&NR=10906848B2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Gaynor, Andrew T</creatorcontrib><creatorcontrib>Robinette, Eric J</creatorcontrib><creatorcontrib>Schmidt, John R</creatorcontrib><creatorcontrib>Conroy, Paul J</creatorcontrib><creatorcontrib>Wildman, Raymond A</creatorcontrib><title>Propellant grain for optimizing the interior ballistic performance of a weapon</title><description>A method of manufacturing and optimizing energetic propellant grains includes generating an optimal surface area to mass fraction burned ratio profile for a predetermined solid structure including propellant grains; using the profile as a target function of a topological optimization process to generate a 3D form of a propellant grain; developing a negative of the 3D form of the propellant grain; mixing and densifying the negative with an energetic material in an uncured form in a mixer to create a structure including the energetic material and embedded negative; and solvating the negative from the structure, wherein the negative comprises a 3D propellant grain. The developing of the negative of the 3D form of the propellant grain may occur using a predetermined material in an additive manufacturing process. The negative may be soluble in the predetermined material, and the energetic material may be insoluble in the predetermined material.</description><subject>CHEMISTRY</subject><subject>EXPLOSIVES</subject><subject>EXPLOSIVES OR THERMIC COMPOSITIONS</subject><subject>MANUFACTURE THEREOF</subject><subject>MATCHES</subject><subject>METALLURGY</subject><subject>USE OF SINGLE SUBSTANCES AS EXPLOSIVES</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNyj0KAkEMQOFtLES9QzyAsP4ga6soViKo9RKHzBqYTcJMQPD0buEBrB48vnF1uWY1SgnFocvIAlEzqDn3_GHpwF8ELE6Zh__ElLg4BzDKA-xRAoFGQHgTmsq0GkVMhWa_Tqr56Xg_nBdk2lIxDCTk7eO2rHf1ttk0-9X6H_MFW6s3Kg</recordid><startdate>20210202</startdate><enddate>20210202</enddate><creator>Gaynor, Andrew T</creator><creator>Robinette, Eric J</creator><creator>Schmidt, John R</creator><creator>Conroy, Paul J</creator><creator>Wildman, Raymond A</creator><scope>EVB</scope></search><sort><creationdate>20210202</creationdate><title>Propellant grain for optimizing the interior ballistic performance of a weapon</title><author>Gaynor, Andrew T ; Robinette, Eric J ; Schmidt, John R ; Conroy, Paul J ; Wildman, Raymond A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US10906848B23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2021</creationdate><topic>CHEMISTRY</topic><topic>EXPLOSIVES</topic><topic>EXPLOSIVES OR THERMIC COMPOSITIONS</topic><topic>MANUFACTURE THEREOF</topic><topic>MATCHES</topic><topic>METALLURGY</topic><topic>USE OF SINGLE SUBSTANCES AS EXPLOSIVES</topic><toplevel>online_resources</toplevel><creatorcontrib>Gaynor, Andrew T</creatorcontrib><creatorcontrib>Robinette, Eric J</creatorcontrib><creatorcontrib>Schmidt, John R</creatorcontrib><creatorcontrib>Conroy, Paul J</creatorcontrib><creatorcontrib>Wildman, Raymond A</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Gaynor, Andrew T</au><au>Robinette, Eric J</au><au>Schmidt, John R</au><au>Conroy, Paul J</au><au>Wildman, Raymond A</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Propellant grain for optimizing the interior ballistic performance of a weapon</title><date>2021-02-02</date><risdate>2021</risdate><abstract>A method of manufacturing and optimizing energetic propellant grains includes generating an optimal surface area to mass fraction burned ratio profile for a predetermined solid structure including propellant grains; using the profile as a target function of a topological optimization process to generate a 3D form of a propellant grain; developing a negative of the 3D form of the propellant grain; mixing and densifying the negative with an energetic material in an uncured form in a mixer to create a structure including the energetic material and embedded negative; and solvating the negative from the structure, wherein the negative comprises a 3D propellant grain. The developing of the negative of the 3D form of the propellant grain may occur using a predetermined material in an additive manufacturing process. The negative may be soluble in the predetermined material, and the energetic material may be insoluble in the predetermined material.</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng |
recordid | cdi_epo_espacenet_US10906848B2 |
source | esp@cenet |
subjects | CHEMISTRY EXPLOSIVES EXPLOSIVES OR THERMIC COMPOSITIONS MANUFACTURE THEREOF MATCHES METALLURGY USE OF SINGLE SUBSTANCES AS EXPLOSIVES |
title | Propellant grain for optimizing the interior ballistic performance of a weapon |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-15T07%3A24%3A04IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=Gaynor,%20Andrew%20T&rft.date=2021-02-02&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS10906848B2%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |