![]() Differential unit gear shrouds
专利摘要:
A gear shroud arrangement includes a mounting plate (102) defining an aperture (104) therethrough. A first cylindrical shroud (106) is included having a first end (108) and an opposed second end (110), wherein the first end of the first shroud is connected to an outer periphery of the mounting plate and is aligned with the aperture. A backing plate (112) is mounted to the second end of the first shroud. A second cylindrical shroud (114) extends from the backing plate in a direction opposite the first shroud. 公开号:EP3708873A1 申请号:EP19213732.1 申请日:2019-12-05 公开日:2020-09-16 发明作者:Glenn C. Lemmers Jr.;Derek R. Hochstetler 申请人:Hamilton Sundstrand Corp; IPC主号:F16H48-00
专利说明:
[0001] The present disclosure relates to gear shrouds, and more particularly to gear shrouds for gears Integrated Drive Generators (IDGs). 2. Description of Related Art [0002] Generators are connected to gas turbine engines so that aircraft can generate on board electricity. In order to produce useful power, generators need to be driven at a substantially constant speed. To drive a generator at a constant speed using a gas turbine engine that runs at very different speeds at different stages in a flight, a constant speed drive (CSD) can be connected between the gas turbine engine and the generator. A CSD is a type of transmission that reduces the range of speed at its input to a much narrower range of speed at its output to provide a nearly constant output speed over a range of input speeds. A CSD and generator can be integrated together into a single unit called an IDG. [0003] The conventional techniques have been considered satisfactory for their intended purpose. However, there is an ever present need for improved CSDs and IDGs. This disclosure provides a solution for this need. SUMMARY OF THE INVENTION [0004] A gear shroud arrangement includes a mounting plate defining an aperture therethrough. A first cylindrical shroud is included having a first end and an opposed second end, wherein the first end of the first shroud is connected to an outer periphery of the mounting plate and is aligned with the aperture. A backing plate is mounted to the second end of the first shroud. A second cylindrical shroud extending from the backing plate in a direction opposite the first shroud. [0005] The first shroud can extend counter-clockwise from a first position between an 11 o'clock position and a 12 o'clock position as viewed toward the mounting plate and a 6 o'clock position relative to the 12 o'clock position. The second shroud can extend counter-clockwise from the 12 o'clock position as viewed toward the mounting plate and a position between a 9 o'clock position and a 8 o'clock position relative to the 12 o'clock position. The first shroud can be mostly convex, wherein a concavity is defined in the first shroud between a 10 o'clock position and a 9 o'clock position relative to the 12 o'clock position. The concavity can define an aperture therein passing through the first shroud. The mounting plate can define an off-center aperture therethrough between a 9 o'clock position and a 6 o'clock position relative to the 12 o'clock position. The off-center aperture can have a generally lunate shape with a nose extending toward a center axis of the mounting plate from the generally lunate shape. The mounting plate can include a riser tube extending about the aperture and extending in a direction away from the backing plate. [0006] The second shroud can include a first step and a second step extending further from the backing plate than the first step. The first and second steps can meet at a position between the 12 o'clock position and an 11 o'clock position relative to the 12 o'clock position. The second step can extend counter-clock-wise from the first step. A mounting flange with a fastener aperture can extend from the second shroud where the first and second steps meet. [0007] An IDG housing can be included, wherein the mounting flange is engaged to an outer housing wall of the IDG housing. The mounting plate can define a plurality of fastener apertures therethrough. A differential unit can be mounted to the mounting plate by fasteners engaged in the fastener apertures. The mounting plate, first shroud, second shroud, and backing plate can form a first gear shroud portion and an opposed gear shroud portion can be engaged with the first gear shroud portion and with the differential unit to form a complete gear shroud for the differential unit. Each of the mounting plate and backing plate of each of the gear shroud portions can include a concave notch proximate the 12 o'clock position. [0008] These and other features of the systems and methods of the subject disclosure will become more readily apparent to those skilled in the art from the following detailed description of the preferred embodiments taken in conjunction with the drawings. BRIEF DESCRIPTION OF THE DRAWINGS [0009] So that those skilled in the art to which the subject disclosure appertains will readily understand how to make and use the devices and methods of the subject disclosure without undue experimentation, preferred embodiments thereof will be described in detail herein below with reference to certain figures, wherein:Fig. 1 is a perspective view of an exemplary embodiment of a gear shroud portion constructed in accordance with the present disclosure, showing the mounting plate and backing plate; Fig. 2A is a plan view of the gear shroud of Fig. 1, showing the mounting plate; Fig. 2B is a plan view of the gear shroud of Fig. 1, showing the backing plate viewed from the opposite direction from Fig. 2A; Fig. 3 is a side-elevation view of the gear shroud of Fig. 1, showing the step in the second shroud and the aperture through the first shroud; Fig. 4 is a perspective view of the gear shroud of Fig. 1, showing the gear shroud engaged with the outer wall of an IDG housing; Fig. 5 is a perspective view of the gear shroud arrangement of Fig. 4, showing two hydraulic transmission units and a differential unit engaged in the IDG housing; and Fig. 6 is a perspective view of the IDG housing of Fig. 5. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS [0010] Reference will now be made to the drawings wherein like reference numerals identify similar structural features or aspects of the subject disclosure. For purposes of explanation and illustration, and not limitation, a partial view of an exemplary embodiment of a gear shroud arrangement in accordance with the disclosure is shown in Fig. 1 and is designated generally by reference character 100. Other embodiments of gear shrouds in accordance with the disclosure, or aspects thereof, are provided in Figs. 2A-6, as will be described. The systems and methods described herein can be used to shroud gears in IDGs to reduce the amount of oil churning, which improves IDG efficiency and scavenge pump performance, thus improving the IDG oil servicing range. [0011] The gear shroud arrangement 100 includes a mounting plate 102 defining a semi-circular aperture 104 therethrough. A first cylindrical shroud 106 is included having a first end 108 and an opposed second end 110. The first end 108 of the first shroud 106 is connected to an outer periphery of the mounting plate 102 and is aligned with the aperture 108 with respect to the axis A. A backing plate 112 is mounted to the second end 110 of the first shroud 106. A second cylindrical shroud 114 extends from the backing plate 112 in a direction opposite the first shroud 106, i.e. the second shroud 114 extends downward from the plate 102 and the first shroud 106 extends upward from the mounting plate 102 as oriented in Fig. 1. [0012] With reference now to Fig. 2A, the first shroud 106 extends counter-clockwise from a first position between an 11 o'clock position and a 12 o'clock position as viewed toward the mounting plate 102 and a 6 o'clock position relative to the 12 o'clock position. As indicated in Fig. 2B (which is flipped relative to the view of Fig. 2A so that clockwise and counter-clockwise directions are reversed in Fig. 2B), the second shroud 114 extends counter-clockwise from the 12 o'clock position as viewed toward the mounting plate 102 and a position between an 9 o'clock position and a 8 o'clock position relative to the 12 o'clock position. The first shroud 106 is mostly convex, wherein a concavity 116 is defined in the first shroud 106 between a 10 o'clock position and a 9 o'clock position relative to the 12 o'clock position. The concavity 116 defines an aperture 118 therein, identified in Fig. 3, passing through the first shroud 106. The mounting plate 102 defines an off-center aperture 120 therethrough between a 9 o'clock position and a 6 o'clock position relative to the 12 o'clock position. The off-center aperture 120 has a generally lunate shape with a nose 122 extending toward a center axis A of the mounting plate 102 from the generally lunate shape. The mounting plate 102 includes a riser tube 124, identified in Figs. 1 and 2A, extending about the aperture 104 and extending in a direction away (i.e., upward as oriented in Fig. 1) from the backing plate 112. [0013] With reference again to Fig. 3, the second shroud 114 includes a first step 126 and a second step 128 extending further from the backing plate 112 than the first step. The first and second steps 126, 128 meet at a position between the 12 o'clock position and an 11 o'clock position relative to the 12 o'clock position. The second step 128 extends counter-clock-wise from the first step 126. A mounting flange 130 with a fastener aperture 132 extends from the second shroud 114 where the first and second steps 126, 128 meet. [0014] With reference now to Fig. 4, an IDG housing 136 is included. The mounting flange 130, shown in Fig. 2B, is engaged to an outer housing wall 138 of the IDG housing 136 with a fastener 140 passing through the fastener aperture 132, identified in Fig. 2B. The mounting plate 102 defines a plurality of fastener apertures 142 therethrough, which are identified in Fig. 1. A differential unit 164 is mounted to the mounting plate 102 by fasteners 140 engaged in the fastener apertures 142. The mounting plate 102, first shroud 106, second shroud 114, and backing plate 112 form a first gear shroud portion 166. An opposed gear shroud portion 168 is engaged with the first gear shroud portion 166 and with the differential unit 164 to form a complete gear shroud for the differential unit 164. Each of the mounting plate 102 and backing plate 112 of each of the gear shroud portions 166, 168 includes a concave notch 170, identified in Fig. 2A, proximate the 12 o'clock position, exposing the gear 152 of the differential unit 164. As shown in Fig. 4, a portion 158 of a differential shroud portion 166 extends within the aperture 156 of the hydraulic unit shroud 157. In Fig. 5, two hydraulic units 143 and 145 are mounted in parallel with the differential unit 164. As shown in Fig. 6, when fully assembled, the outer housing wall 138 of the IDG housing 136 surrounds the components shown in Figs. 4-5 and forms an IDG 162. [0015] The methods and systems of the present disclosure, as described above and shown in the drawings, provide for gear shrouds with superior properties including reducing the amount of oil churning, which improves IDG efficiency and scavenge pump performance, thus improving the IDG oil servicing range. While the apparatus and methods of the subject disclosure have been shown and described with reference to preferred embodiments, those skilled in the art will readily appreciate that changes and/or modifications may be made thereto without departing from the scope of the invention as defined by the claims.
权利要求:
Claims (15) [0001] A gear shroud arrangement comprising: a mounting plate (102) defining an aperture (104) therethrough; a first cylindrical shroud (106) having a first end (108) and an opposed second end (110), wherein the first end of the first shroud is connected to an outer periphery of the mounting plate and is aligned with the aperture; a backing plate (112) mounted to the second end of the first shroud; and a second cylindrical shroud (114) extending from the backing plate in a direction opposite the first shroud. [0002] The arrangement as recited in claim 1, wherein the first shroud extends counter-clockwise from a first position between an 11 o'clock position and a 12 o'clock position as viewed toward the mounting plate and a 6 o'clock position relative to the 12 o'clock position. [0003] The arrangement as recited in claim 2, wherein the second shroud extends counter-clockwise from the 12 o'clock position as viewed toward the mounting plate and a position between an 9 o'clock position and a 8 o'clock position relative to the 12 o'clock position. [0004] The arrangement as recited in claim 2, wherein the first shroud is mostly convex, wherein a concavity is defined in the first shroud between a 10 o'clock position and a 9 o'clock position relative to the 12 o'clock position. [0005] The arrangement as recited in claim 4, wherein the concavity defines an aperture therein passing through the first shroud. [0006] The arrangement as recited in claim 2, wherein the mounting plate defines an off-center aperture (120) therethrough between a 9 o'clock position and a 6 o'clock position relative to the 12 o'clock position. [0007] The arrangement as recited in claim 6, wherein the off-center aperture has a generally lunate shape with a nose extending toward a center axis of the mounting plate from the generally lunate shape. [0008] The arrangement as recited in any preceding claim, wherein the mounting plate includes a riser tube (124) extending about the aperture and extending in a direction away from the backing plate. [0009] The arrangement as recited in any preceding claim, wherein the second shroud includes a first step (126) and a second step (128) extending further from the backing plate than the first step. [0010] The arrangement as recited in claim 9, wherein the first and second steps meet at a position between the 12 o'clock position and an 11 o'clock position relative to the 12 o'clock position. [0011] The arrangement as recited in claim 10, wherein the second step extends counter-clock-wise from the first step. [0012] The arrangement as recited in claim 10, wherein a mounting flange (130) with a fastener aperture extends from the second shroud where the first and second steps meet. [0013] The arrangement as recited in claim 12, further comprising an IDG housing (136), wherein the mounting flange is engaged to an outer housing wall of the IDG housing. [0014] The arrangement as recited in claim 13, wherein the mounting plate defines a plurality of fastener apertures therethrough, and further comprising a differential unit (164) mounted to the mounting plate by fasteners engaged in the fastener apertures. [0015] The arrangement as recited in claim 14, wherein the mounting plate, first shroud, second shroud, and backing plate form a first gear shroud portion (166) and further comprising an opposed gear shroud portion (168) engaged with the first gear shroud portion and with the differential unit to form a complete gear shroud for the differential unit, and preferably wherein each of the mounting plate and backing plate of each of the gear shroud portions includes a concave notch proximate the 12 o'clock position.
类似技术:
公开号 | 公开日 | 专利标题 US9885242B2|2018-02-06|Turbomachine blade US10138817B2|2018-11-27|Gas turbine engine geared compressor with first and second input rotors CN104246197B|2018-09-18|The damper of the fan drive gear transmission system of gas-turbine unit US8973465B2|2015-03-10|Gearbox for gas turbine engine EP2799674B1|2020-06-03|Lubrication oil system for a reduction gearbox JP6035946B2|2016-11-30|Engine duct and aircraft engine JP4806267B2|2011-11-02|Twin spool turbine engine having power take off means in low and high pressure rotors, power take off module for turbine engine, and method of assembling turbine engine US20140178180A1|2014-06-26|Fundamental gear system architecture EP2586978B1|2020-09-02|Turbine of a turbomachine US10301971B2|2019-05-28|Low pressure ratio fan engine having a dimensional relationship between inlet and fan size US10001059B2|2018-06-19|Accessory gearbox with tower shaft removal capability US8585539B2|2013-11-19|Coupling system for a star gear train in a gas turbine engine US10053989B2|2018-08-21|Cooling circuit for a multi-wall blade US9926849B2|2018-03-27|Transverse mounted accessory gearbox US4194869A|1980-03-25|Stator vane cluster EP2964921B1|2019-10-16|Multi-shaft gas turbine engine EP1458967B1|2012-05-02|Gas turbine engine with offset drive RU2406846C2|2010-12-20|Starter/generator module box integration into gear box of gas turbine US8857192B2|2014-10-14|Accessory gearbox with a starter/generator US8876462B2|2014-11-04|System of contra-rotating propellers driven by a planetary gear train providing a balanced distribution of torque between the two propellers JP6001851B2|2016-10-05|Method and system for powering transportation US9506347B2|2016-11-29|Compressor blade for gas turbine engine EP3282093B1|2020-12-23|Geared turbofan with low spool power extraction EP2535544B1|2020-02-19|Transverse mounted accessory gearbox US20180258955A1|2018-09-13|Multi degree of freedom flutter damper
同族专利:
公开号 | 公开日 CN111692311A|2020-09-22| US20200292069A1|2020-09-17|
引用文献:
公开号 | 申请日 | 公开日 | 申请人 | 专利标题
法律状态:
2020-08-14| PUAI| Public reference made under article 153(3) epc to a published international application that has entered the european phase|Free format text: ORIGINAL CODE: 0009012 | 2020-08-14| STAA| Information on the status of an ep patent application or granted ep patent|Free format text: STATUS: THE APPLICATION HAS BEEN PUBLISHED | 2020-09-16| AK| Designated contracting states|Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR | 2020-09-16| AX| Request for extension of the european patent|Extension state: BA ME | 2021-03-19| STAA| Information on the status of an ep patent application or granted ep patent|Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE | 2021-04-21| 17P| Request for examination filed|Effective date: 20210316 | 2021-04-21| RBV| Designated contracting states (corrected)|Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR | 2022-02-25| STAA| Information on the status of an ep patent application or granted ep patent|Free format text: STATUS: EXAMINATION IS IN PROGRESS |
优先权:
[返回顶部]
申请号 | 申请日 | 专利标题 相关专利
Sulfonates, polymers, resist compositions and patterning process
Washing machine
Washing machine
Device for fixture finishing and tension adjusting of membrane
Structure for Equipping Band in a Plane Cathode Ray Tube
Process for preparation of 7 alpha-carboxyl 9, 11-epoxy steroids and intermediates useful therein an
国家/地区
|