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Page Title: CONSTANT RUNOUT VALVE (CROV) WEIGHT SELECTOR
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Table 3-1.—Leading Particulars of Mk 7 Mod 3 Recovery Equipment
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Figure 3-4.—Sectional view of Mk 7 CROV.

system (fig. 3-3) to rotate the CROV cam. Rotation of this cam forces a plunger down onto a set of levers (fig. 3-4), which in turn forces a valve sleeve and valve stem down  to  mate  with  a  valve  seat  to  close  the  valve, shutting off the flow of fluid from the engine cylinder to the engine accumulator, bringing the aircraft to a stop. As stated earlier, the CROV is designed to bring all aircraft, regardless of weight, to a controlled stop while using  approximately  the  same  amount  of  flight  deck landing  area.  This  is  accomplished  by  adjusting  the allowable   opening   of   the   CROV,   a   smaller,   more restrictive opening to arrest a heavy aircraft or a large valve opening to arrest a light aircraft. CONSTANT RUNOUT VALVE (CROV) WEIGHT SELECTOR The  aircraft  weight  selector  makes  it  possible  to adjust  the  CROV  for  aircraft  of  different  weights  by varying the valve opening. See figure 3-4. The  size  of  the  initial  valve  opening  is  adjusted while the arresting engine is in the BATTERY position. The lead screw receives rotary motion from the motor unit  or  handwheel  and  converts  it  into  linear  motion. This linear motion positions the upper lever and drives the local and remote indicators. In  each  of  the  two  levers  (upper  and  lower),  the distance between the fulcrum and roller is constant. On the upper lever, the distance between the fulcrum and the   point   of   application   of   force   from   the   cam   is variable, its greatest length being twice that of the lower lever.  The  lever  arm  ratio  of  each  lever,  therefore,  is variable between 1:1 and 2:1. When the upper lever is fully extended, the ratio of each lever is 1:1. In this setting the initial opening of the control   valve   upon   engagement   of   an   aircraft   is maximum. The resulting rotation of the cam, caused by the   crosshead   moving   inward,   forces   the   plunger downward.   A   plunger   movement   of   1   inch,   acting through the upper lever, would move the lower lever 1 inch;  the  lower  lever,  in  turn,  would  move  the  valve sleeve and stem 1 inch downward. The   cam   is   a   disc   plate   type   with   the   desired contour machined on its periphery. As the cam rotates, it  forces  the  plunger  down.  The  plunger  is  fitted  with rollers, top and bottom. The  bottom  roller  on  the  plunger  acts  against  the top flat bearing surface of the upper lever. The pivot end of the upper lever has a bushed hole that mates with the clevis  end  of  the  lead  screw  yoke.  The  upper  lever  is connected to the clevis end of the yoke by a pin. This pin extends beyond the sides of the yoke and acts as a shaft and has a bushed roller mounted on each extended end.  The  rollers  ride  inside  the  guide  attached  to  the housing. The block end of the yoke is connected to the lead screw by two dowel pins. This connection provides the means by which the lead screw adjusts (moves) the upper lever. 3-6 INDICATOR PLATE CONTROL VALVE CAM RAM TRAVEL AND DECK RUNOUT DIAL CONTROL VALVE REF (CROV) DRIVE CHAINS PULLEY PULLEYS CONTROL VALVE DRIVE CABLE MOVEABLE CROSSHEAD PULLEYS ADJUSTABLE ANCHOR ABE3f0303 Figure 3-3.—Constant runout valve drive system.

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