Jam detection system
A jam detection system for use with a spool valve. The jam detection system includes a spool, a safety sleeve which surrounds the spool, a case which surrounds the safety sleeve, a supply-pressure line, and a return-pressure line. The jam detection system comprises a control volume, an input orifice, an outlet line and a pressure detection element. The control volume is configured to be fluidly connected to the supply-pressure line via the input orifice. The control volume is configured to be fluidly connected to the return-pressure line via the outlet line. The pressure detection element is configured to detect the pressure or a change in pressure within the control volume.
1 . A helicopter rotor actuator control system comprising:
a spool valve and a jam detection system,
the spool valve comprising:
a spool;
a safety sleeve which surrounds the spool;
a case which surrounds the safety sleeve, a supply-pressure line, and a return-pressure line; and
the jam detection system comprising:
a control volume, an input orifice, an outlet line and a pressure detection element;
wherein the control volume is configured to be fluidly connected to the supply-pressure line via the input orifice;
wherein the control volume is configured to be fluidly connected to the return-pressure line via the outlet line; and
wherein the pressure detection element is configured to detect the pressure or a change in pressure within the control volume'
wherein:
the spool and case are so configured that the spool occupies a rest position when the spool is not jammed within the safety sleeve, and
the spool is configured to move from the rest position when the spool is jammed within the safety sleeve.
2 . The helicopter rotor actuator control system according to claim 1 , wherein the output line comprises an outlet orifice.
3 . The helicopter rotor actuator control system according to claim 2 , wherein the pressure detection element comprises one or more of a pressure switch, a pressure sensor, and a mechanical switch and a membrane.
4 . The helicopter rotor actuator control system according to claim 3 , wherein the system comprises a control unit, and the control unit is in communication with the pressure detection element.
5 . The helicopter rotor actuator control system according to claim 4 , wherein the pressure detection element generates a signal if the pressure detection element detects a change of pressure within the control volume, and the signal is communicated to the control unit.
6 . The helicopter rotor actuator control system according to claim 5 , wherein the pressure detection element generates a signal if the pressure detection element detects a change of pressure within the control volume greater than a predetermined pressure change.
7 . The helicopter rotor actuator control system according to claim 1 , wherein the safety sleeve at least partially prevents flow of fluid along the outlet line when the safety sleeve is in the rest position.
8 . The helicopter rotor actuator control system according to claim 7 , wherein:
the input orifice is configured to permit a first rate of fluid flow from the supply-pressure line into the control volume;
fluid flows along the outlet line at a second rate of fluid flow when the safety sleeve is in the rest position; and
the first rate of fluid flow is greater than the second rate of fluid flow.
9 . The helicopter rotor actuator control system according to claim 8 , wherein:
the input orifice is configured to permit a first rate of fluid flow from the supply-pressure line into the control volume;
fluid flows along the outlet line at a third rate of fluid flow when the safety sleeve is not in the rest position; and
the first rate of fluid flow is less than the third rate of fluid flow.
10 . The helicopter rotor actuator control system according to claim 1 , wherein the input orifice is in fluid communication with the control volume via a pressure line.
11 . The helicopter rotor actuator control system according to claim 1 , comprising another spool valve.
12 . The helicopter rotor actuator control system according to claim 11 , wherein a common input actuates the spool of each spool valve.
13 . The helicopter rotor actuator control system according to claim 12 , wherein the input is a user operable control lever.