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DEPENDENT

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Cll.r,,, _ = '76,. I

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C._= +/)|55 /P_

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(=ss rr/SEc)

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APPENDIX D SHEET _%D 4572 C_ D6"!9856 LIST OF ILLUSTRATIONS PAGE FIGT_E i BLOCK DIAGPAM - ELEVATOR (AUTOPiLOT MODE) ELEVATOR TBANSIENT _SPONSE ", E_ECTRA""_AL* MODE) - RIGHT HAND MASTEB "TELEVATCB TRANSIENT RESPONSE (ELECTRICAL FIGb.'RE 3 MODE) - LEFT HAND MASTER FIG[_RE ELEVATOR FREQUENCY RESPONSE BLOCK DIAGRAM - AILERON (AUTOPI_T MODE) FIGURE 5 F IGL_RE 6 AILERON TRANSIENT Pe_-POHSE (ELECTRICAL MODE) AILERON FREQUENCY RESPONSE FIGURE 7 FIGURE 8 AILERON PCU }_YSTEFESIS BLOCK DIAGRAM - SPOILER DRIVE P.C.U.

FIGURE 9 FIGURE I0 SPOILER DRIVE ACTUATOR T_A_SIENT I_ZSPONSE FIGURE II SPOILER DRIVE PCU F_Qb_/_CY RESPONSE F iGS_LE 12 SPOILER CQNTROL SYS_ HYS"I_ESIS _ vs _,c TEST NO. 655-i FIGURE 1 SPOILER CONTROL SYST_ HYSTERESIS NO. 7 SPOILEB POSITION _-s. _ c SPOILER PCU INPUT TO RH _I[£RON HYS_:d_ESIS SPOILER ACTJATOR #6 TRANSIENT RE_P'¢NSE (ELECT_LI CAL MODE ) FIGURE 16 FREQD_NCY RESPONSE FOR SPOI_R PANEL #2 (ELECTR_ i CAL MODE) F_GT_ un_ 17 RUDDE_ TRANSI_JT R_PONSE (ELE_.CTBICAL MODE) FIGURE 18 THRUST MODULATION SYST'_M ELECTRICAL MODE T_SIENT RESPONSE SHEE'[ '_ I

NUMBER D6- 19856 REV L[R THE BDIJNG CO.... _¥ APPENDIX D - AIRPLANE ELECTRO-I_YDBAULIC POW_ CONTROL U_ITS The 367-80 al.-plane is equipped with electro-_Tdraulic power control units on the following controls: Left hand elevator, right hLna elevator, spoilers, rudder, aileron, later_l control system (spoiler drive PC0).

In additlon, the thrust reversers are controlied by _n electric servo system which drives the reverser levers which in turn control the clam shell hydraulic actuators.

Durin_ the -80 variable s%abillty programs, zhe electro-bydrauli¢ actuatcrs are utilized to accept si@;nals from the airborne computer and drive the -80 control surfaces to perform the dynamics of the simulated airplane..

For this we na_e 5 degree of freedom control, zhe pitching equation by elevator, the roll equation by wheel {laterai _ontroi), the drag equation by thrust reverser modulation, the yawing moment equatlon by rudder, and the lift equat$on by spoilers_ For each of the &fore_entloned systems %his appendix contains a block diagram, transient response, frequency response, the line_rized transfer functions, surface rate limits, and displacement l_mits° Also, _be h_-steresls of the lateral control system is included.

In sumnarizln_ the 367-@0 is equipped wlZh the e!ectre-hydra_iic actuators on eac_ controlled axes except thrust reversers, the _vn_mics of which are very _oed and the f_quency response entirely sufficient for use is a variable sZability control system.

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CH[_'X

ELEVATOR TRANSIENT R[.5PD,_F

APR . [ELLC__TRId_II_ .MI'_£?

APR THE BOEING COMPANY • i| B I)6 -- 19856 I

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AILERON ('AU'fOPILOT MODE.)

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TIi_RE _. $IC.,_ND5 MAX e.LAM 51.18L4. RMT_ = . THRUST MO, DLIL,qTION 5VSTEM '_ REVISED CN _C"lc ELECTRICAL M,ODE.

TR/INS! ENT RE.SPOIOSE..

i APR L APR PAGF: THE BOEING COMPANY '1)20 m NUMBER _,>-I'_:_$6 REV LTR ,_,, m'ONJN_ .......

LIMITATIONS This document is controlled by _,i_e_ro-_'_es _ta_': " All revisions to this document shall be approved by the above noted organization prior to release.

DDC AVAILABILITY NOTICE Qualified requesters may obtain copies of this document from DDC.

Foreign announcement and dissemination of this report by DDC is not authorized.

U. S. Government agencies may obtain copies of this document di- rectly from DDC. Other qualified DDC users shall request through The Boeing Company, Seattle, Wn.

U. S. military agencies may obtain copies of this document directly from DDC. Other users shall request through The Boeing Company, Seattle, Wn.

All distributation of this document is controlled. Qualified DDC users

7-1

shall request through The Boeing Company, Seattle, Wn.

PROPRIETARY NOTES SHEET AO 457=' C 1_700_ NUMBER .... ])6-19856 REV LTR ACTIVE SHEET RECORD ADDED SHEETS ADDED SHEETS SHEET _e ne SHEET I-- I- I-- I- Jl NUMBER SHEET NUMBER SHEET SHEET SHEET > > > > NUMBER NUMBER NUMBER NUMBER > LILI ILl IJJ LLI ggl iv E I h6 _8 1, 1,9 T 32 A 5T lh 15 6o APPENDIX J 17 &-I i8 A-2 A-3 A-_ A-5 A-6 A-7 2_ A-8 A-9 25a A-10 A-II 21' A-12 A-13 A 29 A-Z_ 30 A A-15 31 A-16 A-17 33 A-18 3h A-19 35 A-20 36 A-21 37 A-22 A-23 A-2_ _o A-25 hz A-26 1,2 h3 h5 SHEET b All) 4._l-lt I 6-7000 NUMBER -,-,.,.. mO,4_"JAFO co,.,.-..,,,,.,. REV LTR SHEET ,..J NUMBER

>

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-.. "i :--L. 0 i-,- r_ "4 " "J:: _-___-_ r'.> - > I AID 45726-R1 NUMBER ",-,= m,_'_lrJ_ll_'_ ' =o.,.A,,,v REV LTR ACTIVE SHEET RECORD ADDED SHEETS ADDED SHEETS SHEET = SHEET .v iv Ix I- In I-- I-- I-- NUMBER SHEET " SHEET NUMBER -" SHEET _ SHEET ...a > > NUMBER > NUMBER I&l ,,>, NUMBER ,,>, NUMBER 144 M.I ¢1£ iv n,,,, n,,, O-3 D-h D...5 D-7 1>-8 D-9 I)-10 D-11 A D-12 D-13 D-I_ D-15 D-16 D-17 D-19 D-20 a b A C d A • A

I

SHEET e.

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