Flexible response secured mechanical balancing for multiple control actuators with a common output

• US 9,470,248 B2
• Filed: 08/20/2014
• Issued: 10/18/2016
• Est. Priority Date: 09/17/2013
• Status: Active Grant

• Current Assignee: Airbus Helicopters Deutschland Gmbh (Airbus SE)
• Original Assignee: Airbus Helicopters Deutschland Gmbh (Airbus SE)
• Inventors: Paulmann, Gregor
• Primary Examiner(s): Lazo, Thomas E
• Application Number:
  US14/463,832
• Publication Number:
  US 20150075149A1
• Time in Patent Office: 790 Days
• Field of Search: 915/09, 915/10, 915/12
• US Class Current: 1/1
• CPC Class Codes: F15B 18/00 Parallel arrangements of independent servomotor systems
• CPC Class Codes: F15B 2211/8757 using redundant components or assemblies

Abstract

A flexible response secured mechanical balancing device (D) for multiple hydraulic control actuators (1-2) with a common output member (5a-b). The balancing device (D) provides flexible/continuous fluid-pressure force fight compensation. Balance valves (17-20) are commanded to balance fluid-pressure from a first fluid-pressure network (52a) of a second actuator (2). Each fluid-pressure commanded balance valve (17-20) is arranged to allow relief of differential pressure, directly into a dedicated first (52a) or second fluid-pressure network (52b). A fluid-pressure controlled locking device (21-22) is allowing inhibiting the corresponding pairs of balance valves (17-20) e.g. in case of loss of fluid-pressure. The invention typically applies to vehicles (A) including: aircrafts, rotorcrafts, drones.

Claims

1. A mechanical balancing device for a fluid-pressure actuating system;

the actuating system including first fluid-pressure connecting means to a first fluid-pressure network and second first fluid-pressure connecting means to a second fluid-pressure network, the first fluid-pressure network being independent from the second fluid-pressure network and both networks being connected to the mechanical balancing device;

the actuating system having at least a first actuator and a second actuator, the first fluid-pressure connecting means are for linking and feeding the first actuator with fluid-pressure from the first fluid-pressure network, while the second fluid-pressure connecting means are for linking and feeding the second actuator with fluid-pressure from the second fluid-pressure network;

the first actuator and the second actuator being mechanically linked to cooperate for displacing at least a first common output member and a second common output member between two extreme control positions;

the first and second actuators includes respectively a first and second movable piston each severing an extraction fluid-pressure chamber and a refraction fluid-pressure chamber,

wherein for the fluid-pressure balancing device to provide flexible/continuous force fight compensation for respective first and second actuators, the fluid-pressure balancing device includes, for each of first/second-extension/retraction chambers of the first and second actuators, one dedicated fluid-pressure commanded balance valve;

a first balance valve being commanded to balance fluid-pressure from the first fluid-pressure network to a given extension fluid-pressure chamber of the first actuator, is rigidly coupled by a corresponding coupling rod to a cooperating second balancing valve balancing fluid-pressure from the second fluid-pressure network to a given extension fluid-pressure chamber of the second actuator;

while a third balancing valve commanded to balance fluid-pressure from the first fluid-pressure network to a given retraction fluid-pressure chamber of the first actuator, is rigidly coupled by another corresponding coupling rod to a cooperating fourth balancing valve balancing fluid-pressure from the first fluid-pressure network to a given retraction fluid-pressure chamber of the second actuator;

each fluid-pressure commanded balance valve being arranged to allow relief of differential pressure, directly into a dedicated return pressure relief line of an associated first fluid-pressure network or an associated second fluid-pressure network;

a locking assembly cooperating with the mechanical balancing device and includes, for each of a pair of first/second balance valves and third/fourth first balance valves, a fluid-pressure controlled locking device, each locking device having first and second retainer pins adapted to engage with the corresponding coupling rods thus inhibiting the corresponding pair of first/second balance valves and third/fourth first balance valves, in case of loss of fluid-pressure in one of the first fluid-pressure network or the associated second fluid-pressure network.

2. A mechanical balancing device according to claim 1, wherein each fluid-pressure balancing valve is having a cylinder bore forming a corresponding chamber and therein a slidably movable piston which is displaced under pressure supplied from a corresponding tap line;

if displaced, the slidably movable piston is opening a connection port which supplies the corresponding chamber with pressure to a corresponding pressure relief line forming a return circuit of the affected fluid-pressure network, to allow relief of this pressure;

the fluid-pressure balancing device includes a flow restrictor in the corresponding tap line, to provide a damping function against instable fluid-pressure feeding of the corresponding slidably movable piston in the balance valve.

3. A mechanical balancing device according to claim 2, wherein the cylinder bore is sealed with the slidably movable piston of each of the balance valve through high accuracy direct mating, with reduced friction.

4. A mechanical balancing device according to claim 2, wherein the slidably movable piston of each of the balance valve is equipped with at least one pressure compensating groove;

the corresponding cylinder bore being connected to the corresponding pressure relief line so as to return any resulting internal leakage losses inside the cylinder bore, back to a corresponding pressure relief line of the affected fluid-pressure network.

5. A mechanical balancing device according to claim 2, wherein each of the cylinder bore is physically separated from any other cylinder bore of another chamber in the fluid-pressure balancing device, for avoiding common cause failure and providing independent fluid-pressure networks.

6. A mechanical balancing device according to claim 2, wherein a pair of the slidably movable pistons of the balancing valves for extension/retraction along the actuating direction of the first and second actuators are mechanically connected by a corresponding coupling rod with a retainer piston;

the coupling rod is arranged to displace the slidably movable pistons of the corresponding balancing valves in a cylinder bore of the mechanical balancing device, according to current fluid-pressure values at differential fluid-pressures in related extension/retraction chambers of the first and second actuators;

the location inside the corresponding cylinder bore and/or the distance between the pair of mechanically connected slidably movable pistons of the corresponding balancing valves being determined so as to ensure an overlap of the each slidably movable piston with a respective connection port of corresponding of pressure relief lines in the related extension/refraction chamber.

7. A mechanical balancing device according to claim 6, wherein in at least one of the coupling rod includes adjustment means, the adjustment means being capable of modifying a location along the actuating direction of each slidably movable piston of the corresponding balancing valves inside a corresponding cylinder bore and/or the distance between both pistons of a given pair of mechanically connected slidably movable pistons to ensure a symmetric overlap of the each slidably movable piston with a respective connection port of the pressure relief lines.

8. A mechanical balancing device according to claim 1, wherein at least one locking device is including adjustment means and the retainer piston is including a retainer pin;

the adjustment means ensure simultaneous closure of the corresponding tap lines to return in the connected balancing valves when the retainer pin engages with a hollow housing of complementary shape in a corresponding coupling rod, thus operating a self-centering.

9. A mechanical balancing device according to claim 8, wherein in an active-active operational mode of the actuator system, at least one of the locking device having at least one engagement spring for a retainer pin, each spring engagement being arranged to oppose to respective fluid-pressure in the corresponding locking device and to lock the corresponding coupling rod thus allowing for commanding the actuator system in a passive-active operational mode.

10. An actuating system for a vehicle, the actuating system having multiple fluid-pressure actuators;

the actuating system having at least one mechanical balancing device according to claim 1, wherein in the actuating system a plurality of fluid-pressure actuators cooperate together so as to produce a power force capable of displacing simultaneously common output members;

a simultaneous displacing of the common output members being chosen among;

linear motion and rotational motion.

11. An actuating system according to claim 10, wherein the displacing of the common output members is a linear motion and a balancing direction of the mechanical balancing device is parallel to the actuating direction of the actuators in the actuating system.

12. An actuating system according to claim 10, wherein the common output members are dedicated to operation control in a vehicle;

the common output members commanding a vehicle operating control for displacing between two extreme positions one of a group of;

surfaces, flaps, brakes, arms, spoilers, flaps, through operation of the fluid-pressure actuators.

13. A vehicle equipped with at least one actuator system according to claim 10, wherein the vehicle is an aircraft.

14. A vehicle equipped with at least one actuator system according to claim 10, wherein the vehicle is an aircraft with remote piloting functions, e.g like a remotely pilotable aircraft or a drone or UAV.

15. A vehicle equipped with at least one actuator system according to claim 10, wherein the vehicle is a rotary wing aircraft.