Failure tolerant rotor blade pitch angle controlling device

Abstract

A mechanically simple rotor system is a novel mechanism that collectively drives the pitch of the rotor blades by combining the input from three separate servos. Each servo can be controlled by redundant control systems. This configuration reduces total error caused by any one system and allows the continuation of rotor pitch control in the event of one or more servo or system failures.

Claims

1. A failure tolerant rotor blade collective pitch angle controlling device, comprising: a. a plurality of rotor blades, each with a pitch axis of rotation along its length; b. a rotor hub that interconnects said plurality of rotor blades and hinges each rotor blade of said plurality of rotor blades about said pitch axis of rotation; c. a plurality of rotor blade pitch arms, each connecting to a rotor blade of the plurality of rotor blades on one end, to allow transmission of moments to control blade pitch, and each other end extends away from each rotor blade of the plurality of rotor blades of said pitch axis of rotation; d. a rotor shaft that spins and transmits torque, gyroscopic moments and thrust forces along a rotor spin axis; e. a rotating collective fitting of rigid material that spins with and translates along said rotor shaft spin axis to uniformly transmit pitch commands to all rotor blades of said plurality of rotor blades, simultaneously; a plurality of rotor links, each that connect the other end of each blade pitch arm of said plurality of pitch arms, through a hinge or spherical bearing, to said rotating collective fitting, also through a hinge or spherical bearing; g. said plurality of rotor links rotate with said rotor hub, said plurality of rotor blades, said plurality of rotor pitch arms and said rotor shaft about the said rotor shaft spin axis; h. a slider that one end connects to said rotating collective fitting through a rotational bearing and translates along said rotor shaft spin axis to control pitch of said plurality of rotor blades but does not rotate; i. a swivel plate of rigid material that connects to said slider through a spherical joint to allow relative changes in orientation between the said swivel plate and said slider; j. three irreversible actuators, each connected to a stationary structure on one end and to said swivel plate on each other end, to control and adjust said swivel plate orientation and position by modifying the length of each actuator of said three irreversible actuators, thereby, uniformly adjusting the pitch of all said plurality of rotor blades simultaneously by averaging the input of each said three irreversible actuators, even if one or more actuators of said three irreversible actuators fail.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a side view of the voting rotor pitch control systemtwo-bladed rotor shown.

(2) FIG. 2 is a enlarged view of the rotor hub, rotor blade, blade pitch arm and rotor link.

(3) FIG. 3 is a perspective view of the voting rotor pitch control system schematic.

(4) The preferred embodiment of the present invention is a mechanical voting pitch control system that allows averaging from three irreversible servos 89 or actuator inputs to drive rotor blade 41 pitch positions collectively and in unison. (FIG. 1). In the event one or more servos 89 or control systems stop functioning or function improperly, the other servo or servos can drive the pitch system. FIG. 1 depicts a side view of the present invention, showing only two rotor blades and associated linkages for clarity. The preferred embodiment has six rotor blades 41 but the invention may have more or less. Rotor blades 41 and control arms 103 have pitch positions controlled by movement of three irreversible servos 89 which are each connected to stationary structure 90 through a spherical bearing 98. The servos 89 are also connected to a swivel plate 93 through spherical bearings 98 that pivots around a spherical bearing 86 that is part of or attached to the slider 101. The spherical bearing 86 may bear against the swivel plate 93 directly or bear against a race that connects to the swivel plate 93. The three servo connections define a plane that determines the position of the slider 101 along the rotor shaft 85. The swivel plate 93 and the slider 101 do not rotate with the rotor shaft. Bearings 107 allow rotational isolation of the rotor shaft 85 and the slider 101 while still maintaining lateral continuity between both. The bearings 107 do not restrict the slider 101 from translating along the rotor shaft 85. The slider 101 is connected to a rotating collective fitting 91 through a rotational bearing 105 that is captured by a retaining clip 97 that resides in a machined groove. The rotational bearing 105 isolates the rotational movement of the collective fitting 91 to that of the slider 101 while still maintaining lateral and axial positioning. The collective fitting 91 translates along the rotor shaft and moves each rotor link 87 the same axial distance the slider 101 moves. Each rotor link 87 is attached to a blade pitch arm 103, which is rigidly attached to a blade. The rotor pitch arms 103 convert linear motion of the links 87 to rotational motion of the blade 41 about each blade pitch axis. A set of links 99 is attached between the collective fitting 91 and the rotor hub 43 through a series of hinges 94. These maintain rotational position between the rotor head 43 and collective fitting 91 without impeding relative axial movement along the rotor shaft 85. Similarly, another set of links 109 attaches the swivel plate 93 to stationary structure 90 on a vehicle or other machine. These links 109 keep the swivel plate 93 from rotating with the rotor shaft 85 while still allowing the swivel plate to pivot freely about its spherical bearing center. A spherical bearing 92 is required to attach the link 109 to the swivel plate 93 to allow independent rotation.

(5) Other embodiments of the present invention may control the rotors pitch in a similar manner using different geometry and components but maintaining the ability to mechanically vote using a swivel plate 93 and multiple servos or actuators. The preferred embodiment uses three irreversible actuators to determine the swivel plate 93 orientation and position. Other embodiments of the present invention may use more than three reversible servos or actuators to vote and provide control redundancy to the rotor pitch system. A reversible servo or actuator is one that does not maintain position when power or commanded signal is lost. Still another embodiment of this invention is a system that contains multiple parallel pitch mechanisms that controls pairs of rotor blades attached opposite to each other on the rotor hub 43. Each system is driven by a servo 89, actuator or sets of either to independently control the pitch of pairs of rotor blades. For instants, a rotor hub containing six rotor blades could be controlled by three independent pitch mechanisms. Loads from the paired blades would be balanced across the rotor hub 43 even if they were commanded at different pitch angles from the other blade sets, or if they were inoperative.

(6) The forgoing is considered as illustrative only to the principal of the invention. Further, since numerous changes and modification will occur to those skilled in the art, it is not desired to limit the invention to the exact construction and operation shown and described above, and accordingly, all suitable modifications and equivalents may be resorted to falling within the scope of the invention.