Exemplary embodiments pertain to integrated drive generators and, more particularly, to a differential with a sun gear configuration for an integrated drive generator.
In general, aircraft electric power generation utilizes a hydro-mechanical transmission that receives a power input, at variable speed, from an engine to drive a generator at a constant speed. The hydro-mechanical transmission includes a differential to convert the variable speed of the engine to the constant speed for the generator.
At present, a configuration of the differentials used in the hydro-mechanical transmission for aircraft electric power generation is a two ring gear configuration. The two ring gear configuration includes a first ring gear to first planet gear mesh, a first planet gear to second planet gear mesh, and second planet gear to second ring gear mesh configuration. The two ring gear configuration has a specific differential ratio of one (1) due to the first and second planet gears being the same size. This specific differential ratio limits the two ring gear configuration to a lower input speed range. In addition, the two ring gear configuration forces specific packaging arrangements of the hydro-mechanical transmission. Particularly, the differential must be side-to-side with a hydraulic unit and include gearing between the differential and the hydraulic unit.
According to one embodiment of the present invention, an input driven gear for an integrated drive generator is provided. The input driven gear comprises a gear body having an outer diametric wall, an inner diametric wall, a plurality of fastening holes, and a fastening structure aligned with the plurality of fastening holes, wherein the outer diametric wall includes a plurality of outer gear teeth.
Additional features and advantages are realized through the techniques of the present invention. Other embodiments and aspects of the invention are described in detail herein and are considered a part of the claimed invention. For a better understanding of the invention with the advantages and the features, refer to the description and to the drawings.
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:
In contrast to the sun-less differential type described above, embodiments herein relate to piece-part, sub-assembly, assembly, and component levels of a differential composed of a sun gear configuration and utilized in an integrated drive generator.
An integrated drive generator is a hydro-mechanical transmission that drives a synchronous salient pole generator. The integrated drive generator is a constant speed output, variable speed input transmission that includes the differential and a hydraulic unit. In general, the integrated drive generator utilizes the variable speed input from an accessory gear box of an engine to drive or control a hydraulic unit, which in turn drives or controls a churn leg member of the differential. As the differential is driven, speeds of each speed member of the differential are then summed to generate the constant speed output to drive the synchronous salient pole generator.
The differential can include speed members, such as a carrier shaft, which supports the planet gears; a sun gear; and a ring gear. The carrier shaft is driven based on the variable speed input from the engine. Note that the speed of the carrier shaft can be directly proportional to the engine speed. The carrier shaft through the planet gears drives the sun gear, which in turn drives the ring gear. The sun gear itself is independently varied (e.g., actively controlled) so that as the variable speed of the carrier shaft is transferred to the sun gear, the ring gear can be driven at a constant speed. The ring gear, thus, drives the synchronous salient pole generator at the constant speed output.
To actively control the sun gear, a piston, pump, and motor set of the hydraulic unit are utilized to vary a speed of the sun gear. The piston, pump, and motor set can be a back-to-back axial piston pump configuration, where one portion is a motor and the other portion is a pump. A first portion of the back-to-back axial piston pump configuration is driven proportionally off the speed of the engine (e.g., similar to the carrier shaft) and utilizes a variable swash plate to control displacement of the first portion. Note that based on the angle of the variable swash plate and whether that angle is a negative or positive sign the first portion can be a pump or a motor. Thus, the first portion drives or is driven by a fixed displacement pump (e.g., a second portion of the back-to-back axial piston pump configuration), which in turn controls the sun gear speed.
In view of the above, the differential of the integrated drive generator comprises a specific differential ratio (e.g., at or close to 0.5) that enables the receipt of any input speed along an extensive range. In this way, the integrated drive generator can be utilized in a high speed pad of an aircraft electric power generation system. In addition, the differential enables packaging advantages for the integrated drive generator, such as enabling the differential to be in-line with the hydraulic unit (e.g., enables coaxial packaging), which eliminates gearing between the sun gear and the hydraulic unit and reduces a size of a front region of the integrated drive generator.
Turning now to
In accordance with an aspect of an embodiment, the outer diametric wall 305 can include a plurality of outer gear teeth. The outer gear teeth may be 112 in number and mate with another gear with 50 teeth in number, in accordance with an embodiment. The outer gear teeth may include side surfaces that are carbonized and/or a top surface that is not carbonized.
Further, the input driven gear includes a plurality of outer holes 331 and a plurality of inner holes 333. The holes 331, 333 may be circumferentially aligned in a pattern on the input driven gear 115. For example, the plurality of outer holes 331 may total 18 and be symmetrically spaced about a geometric center of the input driven gear 115. The plurality of inner holes 333 may total 6 and be symmetrically spaced about a geometric center of the input driven gear 115. The holes 331, 333 can add structural stability and/or decrease the total mass of the input driven gear 115. Each hole 331, 333 may have an inner hole wall 334.
The input driven gear 115 also includes a plurality of fastening holes 335 for attaching the input driven gear to the carrier shaft 215. The plurality of fastening holes 335 may total 3 and may be symmetrically spaced about the geometric center of the input driven gear 115. In some embodiments, the plurality of inner holes 333 and the plurality of fastening holes 335 may be intersperse amongst each other and/or divide one another into groupings as shown in
Turning now to
In some embodiments, the demarcation 401 can be about 2.1 inches (e.g., 2.150); the demarcation 402 can be about 2.0 inches (e.g., 2.020); the demarcation 403 can be about 1.6 inches (e.g., 1.647); the demarcation 404 can be about 1.0 inches (e.g., 1.075); and the demarcation 405 can be about 0.3 inches (e.g., 0.374). Further, in some embodiments, the demarcation 410 can be about 1.3 inches (e.g., 1.374); the demarcation 411 can be about 0.1 inches (e.g., 0.096); the demarcation 412 can be about 0.7 inches (e.g., 0.729); the demarcation 413 can be about 1.1 inches (e.g., 1.140); the demarcation 414 can be about 0.6 inches (e.g., 0.645); and the demarcation 415 can be about 1.2 inches (e.g., 1.236).
In some embodiments, the demarcation 422 can be about 0.7 inches (e.g., 0.732); the demarcation 423 can be about 1.3 inches (e.g., 1.382); the demarcation 424 can be about 1.8 inches (e.g., 1.862); and the demarcation 425 can be about 2.1 inches (e.g., 2.117). Further, in some embodiments, demarcation 427 can be about 0.8 inches (e.g., 0.861). In addition, in some embodiments, the demarcation 430 can be about 0.05 inches (e.g., 0.048); the demarcation 431 can be about 1.3 inches (e.g., 1.372); the demarcation 432 can be about 1.1 inches (e.g., 1.166); the demarcation 433 can be about 0.7 inches (e.g., 0.769); the demarcation 434 can be about 1.2 inches (e.g., 1.214); and the demarcation 435 can be about 0.6 inches (e.g., 0.603).
In some embodiments, the demarcation 442 can be about 0.7 inches (e.g., 0.779); the demarcation 443 can be about 1.1 inches (e.g., 1.180); and the demarcation 444 can be about 0.4 inches (e.g., 0.401). Further, in some embodiments, the demarcation 452 can be about 0.9 inches (e.g., 0.912); the demarcation 453 can be about 0.2 inches (e.g., 0.219); and the demarcation 454 can be about 1.1 inches (e.g., 1.131).
Turning now to
The primary focal point of the first leg is located by demarcations 520, 521, where are respectively measured from the X-axis and Y-axis. In some embodiments, the demarcation 520 can be about 0.4 inches (e.g., 0.401), while the demarcation 520 can be about 1.4 inches (e.g., 1.435).
The primary focal point of the second leg is located by demarcations 522, 523, where are respectively measured from the X-axis and Y-axis. In some embodiments, the demarcation 522 can be about 1.4 inches (e.g., 1.443), while the demarcation 523 can be about 0.3 inches (e.g., 0.370).
The primary focal point of the third leg is located by demarcations 524, 525, where are respectively measured from the X-axis and Y-axis. In some embodiments, the demarcation 524 can be about 1.0 inches (e.g., 1.042), while the demarcation 525 can be about 1.0 inches (e.g., 1.065).
Each leg of the fastening structure 500 may also include a secondary focal point. The secondary focal point of the first leg is located by demarcations 530, 531, where are respectively measured from the X-axis and Y-axis. In some embodiments, the demarcation 530 can be about 0.1 inches (e.g., 0.102), while the demarcation 531 can be about 1.4 inches (e.g., 1.487).
The secondary focal point of the second leg is located by demarcations 532, 533, where are respectively measured from the X-axis and Y-axis. In some embodiments, the demarcation 532 can be about 1.3 inches (e.g., 1.339), while the demarcation 533 can be about 0.6 inches (e.g., 0.655).
The secondary focal point of the third leg is located by demarcations 534, 535, where are respectively measured from the X-axis and Y-axis. In some embodiments, the demarcation 534 can be about 1.2 inches (e.g., 1.237), while the demarcation 535 can be about 0.8 inches (e.g., 0.832).
Also, in
Further, demarcations 542, 543 illustrate an angle at which both the second edge and the third edge are shifted with respect to the y-axis. This angled may be any slope at or between 15 degrees to 75 degrees. In some embodiments, the angle is 30 degrees.
In
In
In some embodiments, the demarcation 711 can be about 0.4 inches (e.g., 0.425); the demarcation 713 can be about 0.1 inches (e.g., 0.125); and the demarcation 714 can be about 0.2 inches (e.g., 0.227). Further, in some embodiments, the demarcation 716 can be about 5.0 inches (e.g., 5.190). The demarcations 717, 718 may illustrate a 0.060 inch turn from the first inner diametric edge 321 and the top surface of the input driven gear 115. The demarcation 721 can be about 1.5 inches (e.g., 1.560); the demarcation 722 can be about 1.4 inches (e.g., 1.420); and the demarcation 723 can be about 1.3 inches (e.g., 1.3592), while the angle of the demarcation 725 can be 30 degrees.
The terminology used herein was chosen to best explain the principles of the embodiments, the practical application or technical improvement over technologies found in the marketplace, or to enable others of ordinary skill in the art to understand the embodiments disclosed herein. The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” and/or “comprising,” when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one more other features, integers, steps, operations, element components, and/or groups thereof. Furthermore, the term “about” is intended to include the degree of error associated with measurement of the particular quantity based upon the equipment available at the time of filing the application. For example, “about” can include a range of ±8% or 5%, or 2% of a given value.
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.
Number | Name | Date | Kind |
---|---|---|---|
2288206 | Pierpont | Jun 1942 | A |
3043090 | Sundt | Jul 1962 | A |
3527121 | Moore | Sep 1970 | A |
3851537 | Nickstadt | Dec 1974 | A |
4252035 | Cordner et al. | Feb 1981 | A |
4488053 | Cronin | Dec 1984 | A |
4609842 | Aleem et al. | Sep 1986 | A |
4617835 | Baker | Oct 1986 | A |
4734590 | Fluegel | Mar 1988 | A |
4953663 | Sugden | Sep 1990 | A |
4965477 | Stadler et al. | Oct 1990 | A |
5028803 | Reynolds | Jul 1991 | A |
5472383 | McKibbin | Dec 1995 | A |
5728022 | Schultz | Mar 1998 | A |
5845731 | Buglione et al. | Dec 1998 | A |
6178840 | Colbourne et al. | Jan 2001 | B1 |
6258004 | Johnston | Jul 2001 | B1 |
6799953 | Nelson | Oct 2004 | B2 |
6893208 | Frosini et al. | May 2005 | B2 |
7195578 | Dalenberg et al. | Mar 2007 | B2 |
7472547 | Grosskopf et al. | Jan 2009 | B2 |
8187141 | Goleski et al. | May 2012 | B2 |
8267826 | Duong et al. | Sep 2012 | B2 |
8485936 | Makulec et al. | Jul 2013 | B2 |
8925421 | Vanderzyden et al. | Jan 2015 | B2 |
9115794 | Vanderzyden et al. | Aug 2015 | B2 |
9410572 | Shoup et al. | Aug 2016 | B2 |
20040042698 | Yamamoto et al. | Mar 2004 | A1 |
20050006164 | Teraoka | Jan 2005 | A1 |
20060079370 | Kushino | Apr 2006 | A1 |
20060205560 | Meier | Sep 2006 | A1 |
20080108471 | Deutsch | May 2008 | A1 |
20090101465 | Hart et al. | Apr 2009 | A1 |
20090203492 | Okabe | Aug 2009 | A1 |
20100167863 | Lemmers | Jul 2010 | A1 |
20100284836 | Grosskopf et al. | Nov 2010 | A1 |
20110105270 | Matsuoka et al. | May 2011 | A1 |
20130068057 | Grosskoph | Mar 2013 | A1 |
20130260951 | Norem et al. | Oct 2013 | A1 |
20130288840 | Grosskopf et al. | Oct 2013 | A1 |
20140008170 | Vanderzyden et al. | Jan 2014 | A1 |
20140030356 | Jiang et al. | May 2014 | A1 |
20150013488 | Matsuoka et al. | Jan 2015 | A1 |
20150125277 | Ward | May 2015 | A1 |
20160003339 | Roberts, III et al. | Jan 2016 | A1 |
20160016368 | Kunishima | Jan 2016 | A1 |
20160032969 | Kovach et al. | Feb 2016 | A1 |
20160215815 | Ryu et al. | Jul 2016 | A1 |
Number | Date | Country | |
---|---|---|---|
20160290469 A1 | Oct 2016 | US |