SAFETY SYSTEM, A HELICOPTER FITTED WITH SUCH A SYSTEM, AND A SAFETY METHOD SEEKING TO AVOID AN UNDESIRABLE EVENT

A safety system seeking to avoid an undesirable event while piloting a helicopter. According to the invention, the system is remarkable in that it comprises a computer making it possible at any instant t to generate a three-dimensional envelope of fallback paths for the helicopter, the envelope bein...

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Hauptverfasser:	BELANGER Nicolas, DAMIANI Nicolas, VIOLETTE Arnaud, NIKOLAJEVIC Konstanca
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS PHYSICS SIGNALLING TRAFFIC CONTROL SYSTEMS TRANSPORTING
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creator	BELANGER Nicolas DAMIANI Nicolas VIOLETTE Arnaud NIKOLAJEVIC Konstanca
description	A safety system seeking to avoid an undesirable event while piloting a helicopter. According to the invention, the system is remarkable in that it comprises a computer making it possible at any instant t to generate a three-dimensional envelope of fallback paths for the helicopter, the envelope being obtained by calculating, at the instant t, a set of positions that can be reached by the helicopter during a predetermined flight duration, the computer having parameters previously set with data relating to the flight capabilities of the helicopter and including at least one of the following capabilities: maximum speeds and accelerations in all three spatial directions, minimum turning radii for yaw, nose-down, and/or nose-up movements, maximum weight of the transported load, and maximum stresses.
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According to the invention, the system is remarkable in that it comprises a computer making it possible at any instant t to generate a three-dimensional envelope of fallback paths for the helicopter, the envelope being obtained by calculating, at the instant t, a set of positions that can be reached by the helicopter during a predetermined flight duration, the computer having parameters previously set with data relating to the flight capabilities of the helicopter and including at least one of the following capabilities: maximum speeds and accelerations in all three spatial directions, minimum turning radii for yaw, nose-down, and/or nose-up movements, maximum weight of the transported load, and maximum stresses.</description><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; HELICOPTERS ; PARACHUTES ; PERFORMING OPERATIONS ; PHYSICS ; SIGNALLING ; TRAFFIC CONTROL SYSTEMS ; TRANSPORTING</subject><creationdate>2016</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=20160804&DB=EPODOC&CC=US&NR=2016225269A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20160804&DB=EPODOC&CC=US&NR=2016225269A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BELANGER Nicolas</creatorcontrib><creatorcontrib>DAMIANI Nicolas</creatorcontrib><creatorcontrib>VIOLETTE Arnaud</creatorcontrib><creatorcontrib>NIKOLAJEVIC Konstanca</creatorcontrib><title>SAFETY SYSTEM, A HELICOPTER FITTED WITH SUCH A SYSTEM, AND A SAFETY METHOD SEEKING TO AVOID AN UNDESIRABLE EVENT</title><description>A safety system seeking to avoid an undesirable event while piloting a helicopter. According to the invention, the system is remarkable in that it comprises a computer making it possible at any instant t to generate a three-dimensional envelope of fallback paths for the helicopter, the envelope being obtained by calculating, at the instant t, a set of positions that can be reached by the helicopter during a predetermined flight duration, the computer having parameters previously set with data relating to the flight capabilities of the helicopter and including at least one of the following capabilities: maximum speeds and accelerations in all three spatial directions, minimum turning radii for yaw, nose-down, and/or nose-up movements, maximum weight of the transported load, and maximum stresses.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>HELICOPTERS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>SIGNALLING</subject><subject>TRAFFIC CONTROL SYSTEMS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2016</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjMEKwjAQRHvxIOo_LHhVsBELHmOzNcE2Kd1NpadSJJ5EC_X_saJ49jQ85s1Mo55khtwANcRYrECCxtykrmSsIDPMqOBsWAP5VI_tz7PqTZ9xgaydAkI8GXsEdiBrZ0bBgrcKyVTykCNgjZbn0eTa3Yaw-OYsWo4fqV6H_tGGoe8u4R6erSexiRMhdiLZy3j7n_UCVmA4Gw</recordid><startdate>20160804</startdate><enddate>20160804</enddate><creator>BELANGER Nicolas</creator><creator>DAMIANI Nicolas</creator><creator>VIOLETTE Arnaud</creator><creator>NIKOLAJEVIC Konstanca</creator><scope>EVB</scope></search><sort><creationdate>20160804</creationdate><title>SAFETY SYSTEM, A HELICOPTER FITTED WITH SUCH A SYSTEM, AND A SAFETY METHOD SEEKING TO AVOID AN UNDESIRABLE EVENT</title><author>BELANGER Nicolas ; DAMIANI Nicolas ; VIOLETTE Arnaud ; NIKOLAJEVIC Konstanca</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2016225269A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2016</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>HELICOPTERS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>SIGNALLING</topic><topic>TRAFFIC CONTROL SYSTEMS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>BELANGER Nicolas</creatorcontrib><creatorcontrib>DAMIANI Nicolas</creatorcontrib><creatorcontrib>VIOLETTE Arnaud</creatorcontrib><creatorcontrib>NIKOLAJEVIC Konstanca</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BELANGER Nicolas</au><au>DAMIANI Nicolas</au><au>VIOLETTE Arnaud</au><au>NIKOLAJEVIC Konstanca</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SAFETY SYSTEM, A HELICOPTER FITTED WITH SUCH A SYSTEM, AND A SAFETY METHOD SEEKING TO AVOID AN UNDESIRABLE EVENT</title><date>2016-08-04</date><risdate>2016</risdate><abstract>A safety system seeking to avoid an undesirable event while piloting a helicopter. According to the invention, the system is remarkable in that it comprises a computer making it possible at any instant t to generate a three-dimensional envelope of fallback paths for the helicopter, the envelope being obtained by calculating, at the instant t, a set of positions that can be reached by the helicopter during a predetermined flight duration, the computer having parameters previously set with data relating to the flight capabilities of the helicopter and including at least one of the following capabilities: maximum speeds and accelerations in all three spatial directions, minimum turning radii for yaw, nose-down, and/or nose-up movements, maximum weight of the transported load, and maximum stresses.</abstract><oa>free_for_read</oa></addata></record>
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language	eng
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subjects	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS PHYSICS SIGNALLING TRAFFIC CONTROL SYSTEMS TRANSPORTING
title	SAFETY SYSTEM, A HELICOPTER FITTED WITH SUCH A SYSTEM, AND A SAFETY METHOD SEEKING TO AVOID AN UNDESIRABLE EVENT
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