Disconnect shaft for integrated drive generator
10823230 ยท 2020-11-03
Assignee
Inventors
- Derek R. Hochstetler (Rockford, IL, US)
- Ted A. Martin (Byron, IL, US)
- Duane C. Johnson (Beloit, WI, US)
- Glenn C. Lemmers (Loves Park, IL, US)
Cpc classification
F02C7/36
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D1/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D11/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D2023/123
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D2011/008
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C3/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D11/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C7/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H3/728
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T403/7045
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
International classification
F16C3/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D1/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C7/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H3/72
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C7/36
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D11/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D11/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A disconnect shaft for use in an integrated drive generator longitudinally extending between a first end and a second end having a plurality of gear teeth extending longitudinally from a first face disposed at the first end. A cam ledge is at an intermediate location between the first end and the second end. An annular cavity is defined between an inner surface of an inner bore of the disconnect shaft and an outer surface of a radially inner portion of the disconnect shaft. A generator and a method are also disclosed.
Claims
1. A disconnect shaft for use in an integrated drive generator longitudinally extending between a first end and a second end having a plurality of gear teeth extending longitudinally from a first face disposed at the first end, a cam ledge at an intermediate location between said first end and said second end, an annular cavity defined between an inner surface of an inner bore of said disconnect shaft and an outer surface of a radially inner portion of the disconnect shaft; and wherein an outer diameter of said gear teeth is defined at said first end, and an inner diameter is defined to a radially inner surface of a bore at said first face, and a ratio of said outer diameter to said inner diameter being between 1.4 and 2.1.
2. The disconnect shaft as set forth in claim 1, wherein a cam ledge distance is defined between said first face and a beginning point of said cam ledge, and a ratio of said cam ledge distance to an overall distance between said first face and said second end being between 0.25 and 0.45.
3. The disconnect shaft as set forth in claim 2, wherein said cam ledge including a cam face having a cam outer diameter and a ratio of said cam outer diameter to said overall distance being between 0.3 and 0.5.
4. The disconnect shaft as set forth in claim 3, wherein there are four of said gear teeth on said first face.
5. The disconnect shaft as set forth in claim 1, wherein there are four of said gear teeth on said first face.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
(2)
(3)
(4)
(5)
DETAILED DESCRIPTION
(6)
(7) A gas turbine engine 22 may drive an input shaft 23 which selectively drives a disconnect assembly 26. The disconnect assembly 26, in turn, drives a carrier shaft 28, which drives a carrier in a gear differential 30.
(8) As the carrier shaft 28 rotates, planet gears 36 and 38 are caused to rotate. Gears 38 have a gear interface 42 with a first ring gear portion 40. Gears 36 have a gear interface 48 with a second ring gear portion 46.
(9) Ring gear portion 40 has a gear interface 50 with a main generator drive gear 52. When drive gear 52 is driven to rotate, it rotates a rotor 56 associated with a stator 58 of the main generator as well as an exciter rotor 60. Electric power is generated for a use 62, as known.
(10) It is desirable that the frequency of the generated electric power be at a desired frequency. This requires the input speed to gear 52 to be relatively constant and at the desired speed. As such, the speed of the input shaft 23 is added to the speed of the speed trimmer 66 to result in a constant input speed to gear 52.
(11) A gear 15 that is part of the carrier has a gear interface 16 with a gear 13 driving a shaft 14 also within the speed trimmer.
(12) As known, the speed trimmer 66 includes a variable unit 72 and a fixed unit 76. The units 72 and 76 may each be provided with a plurality of pistons and a swash plate arrangement. If the input speed of the gear 13 is too high, the speed of the gear 52 will also be too high, and hence, the speed trimmer 66 acts to lower the speed of the trim gear 46 which will drop the speed of gear 52. On the other hand, if the input speed is too low, the speed trimmer will increase the trim gear speed and the speed seen by gear 52 will increase.
(13) In essence, the variable unit 72 receives an input through gear 13 that is proportional to the speed of the input shaft 23. The variable unit 72 also receives a control input from a control monitoring the speed of the generator rotor 56. The position of the swash plate in the variable unit 72 is changed to in turn change the speed and direction of the fixed unit 76. The fixed unit 76 can change the speed, and direction of rotation of the shaft 70, and this then provides control back through the trim ring gear 46 to change the speed reaching the generator. In this manner, the speed trimmer 66 results in the frequency generated by the generator being closer to constant, and at the desired frequency.
(14) A permanent magnet generator 32 rotates with the ring gear 40.
(15) An accessory drive shaft 29 rotates with the carrier shaft 28 and drives a plurality of accessory gears 31.
(16) The operation of the integrated drive generator 20 is generally as known in the art. A worker of ordinary skill would recognize that the desired frequency and speed at use 62 would dictate a number of design functions.
(17)
(18)
(19)
(20) As shown in
(21) As shown, the cam face 87 has a changing profile across a circumferential dimension, such that the actuator 88 can cause the disconnect shaft 80 to move to the left against the force of a spring 106. The spring 106 sits between an end face of the carrier shaft 28 and a cavity 110. The carrier shaft 28 rides along spline teeth 104 inside the disconnect shaft to drive the carrier shaft when the disconnect shaft rotates. A rear end 102 of the disconnect shaft is also shown.
(22) Cavity 110 houses the spring 106. In embodiments, the cavity 110 is defined by a radially inner portion 111 spaced inwardly from a radially outer portion 113 and providing cavity 110 to receive a forward end 108 of the spring 106. The cavity 110 provides support for the end of the spring 106. Cavity 110 is shown spaced toward rear end 102 relative to cam ledge 86.
(23) An outer diameter d.sub.1 is defined as a diameter to an outer peripheral surface of the front face 92. An inner diameter d.sub.2 is defined to a radially inner surface 95 of a bore at the front face 92. A cam ledge distance d.sub.3 is defined between the front face 92 and a beginning of the cam ledge 86. A diameter d.sub.4 is defined to the outer periphery of the cam surface 87. An overall distance d.sub.5 is defined between rear end 102 and front face 92.
(24) In an embodiment, d.sub.1 is 1.836 inches (4.784 cm). In a prior art disconnect shaft, it was 1.375 inches.
(25) d.sub.2 in one embodiment is 1.230 inches (3.124 cm). In that same prior art embodiment, d.sub.2 was 0.5 inches.
(26) In the embodiments, a ratio of d.sub.1 to d.sub.2 is between 1.4 and 2.1.
(27) In that same prior disconnect shaft, the distance d.sub.3 was much smaller with the cam ledge being effectively directly behind the surface 96. In the disclosed embodiment, d.sub.3 is 1.607 inches. In the prior embodiment, d.sub.3 was 0.257 inch (0.652 cm). In the disclosed embodiment, d.sub.4 is 1.930 inches (4.90 cm). In that same prior embodiment, it was 1.5 inches (3.81 cm). In the disclosed embodiment, d.sub.5 is 4.896 inches (12.43 cm).
(28) In embodiments, a ratio of d.sub.3 to d.sub.5 is between 0.25 and 0.45. In the same disclosed embodiments, a ratio of d.sub.4 to d.sub.5 is between 0.3 and 0.5.
(29) A disconnect shaft, as disclosed here, provides valuable operational benefits.
(30) A method of replacing a disconnect shaft in an integrated drive generator comprising the steps of removing an existing disconnect shaft from an integrated drive generator including a housing enclosing an input shaft. The input shaft has a gear interface with the existing disconnect shaft. The existing disconnect shaft having spline teeth at an inner peripheral bore slideably engaging a carrier shaft and a spring biasing the existing disconnect shaft such that gear teeth on a forward face of the existing disconnect shaft engage the input shaft. An actuator selectively moves the existing disconnect shaft against the spring to move the gear teeth on the existing disconnect shaft out of engagement with the input shaft. The carrier shaft provides a drive input into a gear differential by driving a set of planetary gears to, in turn, drive a ring gear portion. The ring gear portion selectively provides drive input into a main generator.
(31) The method includes the further step of replacing the existing disconnect shaft with a replacement disconnect shaft. The replacement disconnect shaft includes a forward face having a plurality of gear teeth and extending in a direction to a rear end. A cam ledge is at an intermediate location between the forward face and the rear end. There is an inner bore within the disconnect shaft and a cavity in the inner bore receives an end of the spring to bias the replacement disconnect shaft. The cavity is defined by a radially inner portion of the replacement disconnect shaft spaced from a radially outer portion to define the cavity.
(32) Although an embodiment of this invention has been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of this invention. For that reason, the following claims should be studied to determine the true scope and content of this invention.