Exemplary embodiments of this invention generally relate to an integrated drive generator, and more particularly, to a fixed wobbler of a hydraulic unit of an integrated drive generator.
Aircrafts currently rely on electrical, pneumatic, and hydraulic systems for secondary power. A typical electrical system utilizes an integrated drive generator (IDG) coupled to each engine to provide a fixed frequency power to the distribution system and loads. One type of IDG includes a generator, a hydraulic unit, and a differential assembly arranged in a common housing. The differential assembly is operably coupled to a gas turbine engine via an input shaft. The rotational speed of the input shaft varies during the operation of the gas turbine engine. The hydraulic unit cooperates with the differential assembly to provide a constant speed to the generator throughout engine operation.
Due to packaging constraints, components of the hydraulic unit, such as variable and fixed wobblers must be redesigned.
According to one embodiment of the invention a fixed wobbler of a hydraulic unit includes a body having a first end and an opposite second end, the first end defining a first surface, and the second end defining a second surface oriented at an angle relative to the first surface, the body having an outer diameter and an inner wall defining an inner diameter, wherein the outer diameter is approximately 2.1655+0.0000−0.0007 inches (5.5004+0.000−0.0018 cm), and wherein the inner diameter is approximately 1.043±0.003 inches (2.6492±0.0076 cm).
In addition to one or more of the features described above, or as an alternative, further embodiments may include wherein the body further comprises a cutout formed in the first surface about at least a portion of the inner wall; where the cutout defines an inner shoulder having a radius of approximately 0.156±0.015 inches (0.3962±0.1381 cm); wherein the angle is between approximately 12.75° and approximately 16.75°; wherein the angle is approximately 14.75°; wherein the body further comprises a locking feature formed in the body outer diameter, the locking feature defined by an inner rear wall and a pair of side walls; wherein the locking feature has a length of approximately 0.503±0.010 inches (1.2777±0.0254 cm); wherein a distance between the side walls is approximately 0.250+0.005−0.000 inches (0.635+0.0127−0.000 cm); wherein a distance from the inner rear wall to a centerpoint of the outer diameter is approximately 0.982+0.000−0.010 inches (2.4943+0.000−0.0254); wherein the second surface comprises a friction-reducing coating; wherein the friction-reducing coating is between approximately 3 microns and approximately 5 microns; wherein the friction-reducing coating is an Amorphous Diamond-like Carbon Coating; wherein the inner wall includes a corner break that is less than or equal to approximately 0.005 inches (0.0127 cm); and wherein the body first end includes a first corner break disposed adjacent to a second corner break, the first corner break oriented relative to the first surface at a second angle, wherein the second angle is approximately 40°+0.00°−0.25°.
The subject matter, which is regarded as the invention, is particularly pointed out and distinctly claimed in the claims at the conclusion of the specification. The foregoing and other features, and advantages of the invention are apparent from the following detailed description taken in conjunction with the accompanying drawings in which:
The detailed description explains embodiments of the invention, together with advantages and features, by way of example with reference to the drawings.
Referring now to
An example of an IDG 16 including a housing 18 is shown in
Referring now to
The operation of the hydraulic unit 32 in an IDG 16 of an aircraft involves transmission of torque from an engine of the airplane to an input, which rotates the input shaft 50 of the hydraulic unit 32 about axis A. The cylinder block 38 of the pump 34 is connected to the input shaft 50 for rotation therewith. Pistons 52 within the cylinder block 38 of the pump 34 are displaced during this rotation an amount which is a function of the setting of a variable wobbler 54 of the pump 34. Variable wobbler 54 sets the stroke of each piston 52 depending on its angular position around axis A and on the setting of the wobbler itself.
Hydraulic fluid under pressure from the pump 34 is delivered to the hydraulic motor 36 through the port plate 44 for rotating the cylinder block 40 and an output shaft 56 to which it is fixedly connected. A fixed wobbler 58 of the motor 36 is fixed so that the operating speed of the motor 36 is a function of the displacement of the pump 34. Fixed wobbler 58 sets the stroke of each piston 52 depending on its angular position around axis A. The rotary output from output shaft 56 is added to or subtracted from the rotary motion from the engine through the conventional differential gearing of an IDG 16 for operating an electrical generator at a substantially constant rotational speed. That is, since the speed of the rotation from the airplane engine to the input 50 of the hydraulic unit 32 will vary, the position of the variable wobbler 54 is adjusted in response to these detected speed variations for providing the necessary reduction or increase in this speed for obtaining the desired constant output speed to the generator. During normal operation, there is a hydrostatic balance of the cylinder blocks and port plate. Although the hydraulic unit illustrated and described herein refers to the variable unit as a pump and the fixed unit as a motor, hydraulic units having other configurations, such as where the variable unit functions as a motor and the hydraulic unit operates as a pump for example, are within the scope of the invention.
Referring now to
As shown in
First end 64 may include a cutout 72 formed in first surface 68 and defining a cutout surface 74, for example, to reduce size and weight of fixed wobbler 58. Cutout surface 74 may define an inner shoulder 75 (
First surface 68 may include a coating to reduce friction and wear between surface 70 and pistons 52. In one embodiment, the coating is titanium nitride disposed by physical vapor deposition. However, other friction-reducing coating materials (e.g., Amorphous Diamond-like Carbon Coating) may be disposed on surface 70 by other suitable methods. Further, additional portions and surfaces of fixed wobbler 58 may include the coating described herein (e.g., cutout surface 74). In one embodiment, the coating has a thickness of approximately 1-4 microns. In another embodiment, the coating has a thickness of 1-4 microns. In one embodiment, the coating has a thickness of approximately 3-5 microns. In another embodiment, the coating has a thickness of 3-5 microns.
Body 62 defines an outer diameter 76 and includes an inner wall 78 defining an inner diameter 80. In one embodiment, outer diameter 76 is approximately 2.1655+0.0000−0.0007 inches (5.5004+0.000−0.0018 cm). In another embodiment, outer diameter 76 is 2.1655 inches+0.0000−0.0007 inches. Outer diameter 76 may include a corner break 77 (
In one embodiment, inner diameter 80 is approximately 1.043±0.003 inches (2.6492±0.0076 cm). In another embodiment, inner diameter 80 is 1.043±0.003 inches. As illustrated in
With further reference to
Body 62 includes a locking feature or key 86 formed in outer diameter 76. Key 86 is configured to receive a portion of housing 42 or other component (e.g., a stepped pin) to facilitate preventing rotation of fixed wobbler 58 within housing 42. Key 86 includes inner rounded corners 88, an inner rear wall 90, and side walls 92 (
While the invention has been described in detail in connection with only a limited number of embodiments, it should be readily understood that the invention is not limited to such disclosed embodiments. Rather, the invention can be modified to incorporate any number of variations, alterations, substitutions or equivalent arrangements not heretofore described, but which are commensurate with the spirit and scope of the invention. Additionally, while various embodiments of the invention have been described, it is to be understood that aspects of the invention may include only some of the described embodiments. Accordingly, the invention is not to be seen as limited by the foregoing description, but is only limited by the scope of the appended claims.