7/23/2019 Model 525 Relentless Advanced Fly-By-Wire – The Pilot’s Safety Advantage
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Bell Helicopter Textron Inc. i" ! #holly o#ned "ub"idi!ry of Textron Inc. Bell Helicopter Textron C!n!d! $i%ited i" ! #holly o#ned "ub"idi!ry of Textron Intern!tion!l Holding &.$'! #holly o#ned "ub"idi!ry of Textron Inc. (!ch co%p!ny i" ! "ep!r!te leg!l entity !nd ! %e%ber of the Textron f!%ily of co%p!nie".) 2014 Bell Helicopter Textron Inc. All regi"tered tr!de%!r*" !re the property of their re"pective o#ner".
Model 525 Relentless AdvancedFly-By-Wire – The Pilot’s Safety
Advantage
Mie Both!ell " A!ais Ra#a – Bell $elico%ter
+th (A&A otorcr!ft &y%po"iu%
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$elico%ter Safety Revie!
, &iffer fro' fi(ed-!ing
– )%erate lo! s%eed* lo! altit+de* &,* .M/
, /ontrolled Flight into Terrain 0/F.T1
– 34 of /F.T accidents res+lt in fatalities 0TSB1
– )cc+r .M/* ,M/* 'o+ntaino+s* flat terrain
– Flight %hases for /F.T accidents 0FAA A/ 6-6781
o Taeoff and cli'9: 254
o A%%roach and landing: 864
o /r+ise: 8;54
, /a+ses
– <oss of sit+ational a!areness 0in 9oth vertical andhori#ontal a(es1
– S%atial disorientation affected 9y vis+al c+es andaircraft handling =+alities
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Selected $elico%ter /ase St+dies
, ight flight in the >+lf of Me(ico – ?the flight cre!’s fail+re to identify and arrest the helico%ter’s
descent for +ndeter'ined reason* !hich res+lted in controlledflight into terrain@
, A%%roach in the Shetland .slands – ?the co'9ination of the nose-high attit+de* lo! airs%eed* high rate
of descent* and high %o!er %laced the helico%ter in a vorte(-ringstate@
, $MS helico%ter crash into terrain in &, conditions – ?contin+ed flight into +nno!n !eather conditions* !hich res+lted
in his fail+re to 'aintain clearance !ith the gro+nd@ – ?%ress+re to co'%lete the 'ission ind+ced 9y the %ilot-in-co''and
as a res+lt of the e'ergency 'edical services o%eration@
, &ivided %ilot attention
– ?The %ilot stated that d+ring lift-off he !as distracted 9y %ersonson the gro+nd !aving ar's; The aircraft drifted to the left andcontacted a tree after !hich the %ilot landed the aircraft and itrolled over@
/o''on the'es – lo! sit+ational a!areness* high %ilot !orload* ands%atial disorientation
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Fi(ed-Wing FBW
, Fi(ed-!ing ind+stry ahead of co''ercial rotorcraft inado%tion of FBW
, ot all fi(ed-!ing iss+es translate to helico%ters
, FBW Side-stic controller iss+es – An accident ca+sed 9y s%atial disorientation !as co'%o+nded 9y
conflicting control in%+ts fro' the %ilot and co-%ilot side sticcontrollers;
– An incident !here the co-%ilot +nintentionally activated the stic
?taeover@ 9+tton !hile the %ilot !as co''anding a flare forlanding; – Several incidents !here 9oth %ilot and co%ilot are 'aing control
in%+ts and the FBW syste' s+''ed the in%+ts ca+sing ?a9r+%t'ane+vers@;
, e!'an and <a'9regt closing co''ent – ?overall FBW and envelo%e %rotection have %revented accidents
and saved lives; .n the %ast 65 years* there have 9een 2 stallaccidents in co''ercial trans%ort o%erations !ith 8 fatalities –not one !as a FBW air%lane@
FBW Technology has 'ade /o''ercial Fi(ed-Wing Aviation Safer
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Pro%osed Sol+tions
, Fro' FAA* /AA – .ncreased +se of Terrain A!areness and Warning Syste'
0TAWS1 – &efine 'ore consistent %roced+res for dis%atch into .M/ – .ncreased %ilot training – es%ecially in the +se of a+to%ilots
or related syste's as !ell as 9etter 'onitoring of aircraftstate 9y the flight cre!
, Fro' Roger $oh* C; W; $arding st+dies
– Dse of sta9ility and control a+g'entation to decrease %ilot!orload
– <ined %ilot !orload* s%atial a!areness to helico%terhandling =+alities
– Dse of Translational Rate /o''and 0TR/1 and Position$old 0P$1 to significantly lo!er %ilot attention de'and andred+ce s%atial disorientation in lo! s%eedElo! altit+de
– Si'+lation st+dies sho!ed TR/ " P$ red+ced %ilot!orload and i'%roved handling =+alities
/o''on the'es – Address Pilot !orload* a!areness* training*%roced+res
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Bell’s Sol+tion for Safety - FBW
, Bell 525 Relentless
, M+lti-role Part 2 /ivil Trans%ort
, World’s first commercial Fly-by-Wire helicopter
7/23/2019 Model 525 Relentless Advanced Fly-By-Wire – The Pilot’s Safety Advantage
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,oice of the /+sto'er – .'%roved $elico%ter Safety
, Cu"to%er Advi"ory P!nel
– Corpor!te !nd -IP
– irefighting
– /il !" Producer" /P3
– &e!rch !nd e"cue &A3P!r!public
– Helicopter (%ergency 5edic!l &ervice H(5&3
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525 FBW &esign for Safety Philoso%hy
, Provide defa+lt feat+res !hich a+to'atically red+ce%ilot !orload* increase %ilot sit+ational a!areness*and i'%rove aircraft handling =+alities
, Pilot is al!ays in co''and directing the co'%+ter!hile the control la!s achieve the %ilot’s desire !ithacc+racy* s'oothness* and grace
, .f red+ced a+g'entation is necessary 0%erha%s d+eto a syste' fail+re1* the %ilot al!ays has the o%tionof reverting to a 9aseline ?al!ays availa9le@ direct
control strategy
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Pilot /ontrols
, Side-Stic /yclic " /ollective – &etent detection
o .n-detent – /<AW defa+lto )+t-of-detent – Pilot co''and
– Bee%s sle! reference s%eed*altit+de G
– Force Tri' Release resetsdetent* reference* and releasesforces
, Traditional Pedals – &etent detection
o .n-detent – /<AW defa+lto )+t-of detent – Pilot co''and
, Mechanically interconnected%ilot and co%ilot controls – <essons learned fro' fi(ed-!ing
FBW iss+es
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525 FBW– Pilot Worload Red+ction
, /ontin+o+s f+ll ti'e sta9ili#ation in res%onse to !ind* g+sts and otherdist+r9ances
, F+ll ti'e defa+lt attit+de* s%eed* vertical s%eed* and altit+de holds
de%ending +%on the control a(is and airs%eed – S%eed hold frees the %ilot fro' having to 'ae %itch attit+de
corrections via longit+dinal cyclic to reg+late air s%eed
, &eco+%ling the control a(es
– Actively co''and the longit+dinal a(is for e(a'%le* 9+t !ill still holdthe altit+de 0vertical1* 9an angle 0lateral1* and heading 0directional1
– Provide the a%%ro%riate tail rotor thr+st co''and to co+nteract the'ain rotor tor=+e
– <i'iting the reference vertical descent rate as a f+nction of airs%eed –
,RS %rotection
, TR/EP$ at $over and <o! S%eed
– /ritical in lo! altit+de and &, !here helico%ter 'issions co''onlyocc+r – $MS* SAR* Firefighting* )il " >as
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525 FBW – .ncreased Sit+ational A!areness
, &is%lace'ent tri' for cyclic and collective
– Main rotor s!ash%late 'argin a!areness
, /ollective Tactile /+eing
– A): M/P* T)P li'its
– ).: /ontin+o+s* 2 'in* 73 sec li'its
– Pilot ?%+ll-thro+gh@ of tactile c+e
, AR/ $ori#on Flight &ec
– .ntegrated >lass Flight &ec
– .ncreased over-the-nose visi9ility
– T/AS-..* $TAWS* Synthetic ,ision
– &e-cl+ttered coc%it layo+t
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525 FBW– Standardi#ed Behavior
, A+to'atic s!itching9et!een flight regi'es – $),RETR/
– <o! S%eed
– $igh S%eed
, /onsistent /AT-APerfor'ance
– Tae advantage ofTR/EP$
– Standardi#ed training
– o e(%os+re d+ring ).
, A+torotation Assist – Mini'i#e rotor droo%
– Standardi#ed a+torotationentry for training
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$overETR/ Perfor'ance - Si'+lation
Translational Rate Command
Position Hold
Rate Command
Speed Hold
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/oncl+sion
, /ontri9+ting factors to $elico%ter /F.T and related accidents
– $igh %ilot !orload
– <oss of sit+ational a!areness
– <o! altit+de* lo! s%eed* .M/ and &,
, Dse of FBW i'%roves helico%ter handling =+alities and thereforesafety
– Red+ced %ilot !orload
– .ncreased s%atial a!areness
, S%ecific 525 design-for-safety FBW strategies incl+de
– TR/EP$ at lo! s%eed* lo! altit+de
– defa+lt s%eed* attit+de* and vertical s%eed hold f+nctionality
– 'echanically interconnected side-stic controllers
– collective tactile c+eing
– dis%lace'ent tri' !ith 'argin a!areness
– control a(is deco+%ling
– /AT-A %erfor'ance
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Bell Helicopter Textron Inc. i" ! #holly o#ned "ub"idi!ry of Textron Inc. Bell Helicopter Textron C!n!d! $i%ited i" ! #holly o#ned "ub"idi!ry of Textron Intern!tion!l Holding &.$'! #holly o#ned "ub"idi!ry of Textron Inc. (!ch co%p!ny i" ! "ep!r!te leg!l entity !nd ! %e%ber of the Textron f!%ily of co%p!nie".) 2014 Bell Helicopter Textron Inc. All regi"tered tr!de%!r*" !re the property of their re"pective o#ner".
H+estions