Modularity of an aircraft turbomachine
US-2024003303-A1 · Jan 4, 2024 · US
US9879731B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9879731-B2 |
| Application number | US-201314649974-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 14, 2013 |
| Priority date | Dec 6, 2012 |
| Publication date | Jan 30, 2018 |
| Grant date | Jan 30, 2018 |
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A gear spindle ( 3 ) obtained by inclining the axis of a spindle inner tube ( 10 ) provided at one end with an external cog inner tube gear section ( 40 ) at 0.6 degrees to 1.6 degrees with respect to the axis of a spindle outer tube ( 20 ) provided with an internal cog outer tube gear section ( 50 ) that meshes the inner tube gear section ( 40 ). On the teeth of the inner tube gear section ( 40 ) having a face width (B), a crowning of radius (Cr) is provided so that the center in the face width direction is expanded and both tooth ends are thin. The face width (B) and the crowning radius (Cr) are set within an area that is enclosed by graphs of (Cr)=1200 [mm], (Cr)=4000 [mm], (B)=0.0272×(Cr)+28 [mm], (B)=59.04×exp (0.0005×(Cr)) [mm], and (B)=32×(Cr) 0.274 [mm].
Opening claim text (preview).
The invention claimed is: 1. A gear spindle in which, an axis of a spindle inner tube and an axis of a spindle outer tube are inclined with respect to each other at 0.6 degrees to 1.6 degrees, the spindle inner tube having an inner-tube gear portion being an external gear on one end side, the spindle outer tube having an outer-tube gear portion being an internal gear configured to be fitted to the inner-tube gear portion, characterized in that teeth of the inner-tube gear portion having a facewidth B are each provided with a crown of a radius Cr such that the tooth is thicker at the center and thinner at opposite tooth ends along a facewidth direction, and the facewidth B and the crown radius Cr are set within a range defined by Cr=1200 [mm], Cr=4000 [mm], B= 0.0272 ×Cr+ 28 [mm], B= 59.04×exp(0.0005 ×Cr ) [mm], and B= 32 ×Cr 0.247 [mm] in a graph. 2. The gear spindle according to claim 1 , characterized in that B=0.0272×Cr+28 [mm] is a straight line obtained by connecting a large number of points each of which is a set of a given crown radius Cr and a minimum facewidth under a condition where the inclination angle is 0.6 degrees, the minimum facewidth being such that the teeth of the inner-tube spindle do not contact at the tooth ends thereof under the condition where the crown radius Cr is given. B=59.04×exp(0.0005×Cr) [mm] is a curved line obtained by connecting a large number of points each of which is a set of a crown radius Cr and 40 [mm] plus a minimum facewidth under a condition where a given inclination angle is set within the range of 0.6 degrees to 1.6 degrees, the crown radius Cr being such that tooth-root bending stress to be applied to the inner-tube gear portion is a maximum allowable value, the minimum facewidth being such that the teeth of the spindle inner tube do not contact at the tooth ends thereof under the condition where the crown radius Cr is given, and B=32×Cr 0.247 [mm] is a curved line obtained by connecting a large number of points each of which is a set of a given crown radius Cr and a facewidth B being 40 [mm] plus a minimum facewidth under a condition where a given inclination angle is set within the range of 0.6 degrees to 1.6 degrees, and a backlash required for the combination of the crown radius Cr and the facewidth B is an allowable maximum backlash between the inner-tube gear portion and the outer-tube gear portion, the minimum facewidth being such that the teeth of the inner-tube spindle do not contact at the tooth ends thereof under the condition where the crown radius Cr is given. 3. A gear spindle in which an axis of a spindle inner tube and an axis of a spindle outer tube are inclined, with respect to each other at 0.6 degrees to 1.6 degrees, the spindle inner tube having an inner-tube gear portion being an external gear on one end side, the spindle outer tube having an outer-tube gear portion being an internal gear configured to be fitted to the inner-tube gear portion, characterized in that teeth of the inner-tube gear portion are each provided with a crown of a radius Cr such that the tooth is thicker at the center and thinner at opposite tooth ends along a facewidth direction, and the facewidth B and the crown radius Cr are set within a range defined by Cr=1200 [mm], Cr=4000 [mm], B= 0.0272 ×Cr+ 28 [mm], B= 18×exp(0.001 ×Cr ) [mm], and B= 19 ×Cr 0.292 [mm] in a graph. 4. The gear spindle according to claim 3 , characterized in that B=0.0272×Cr+28 [mm] is a straight line obtained by connecting a large number of points each of which is a set of a given crown radius Cr and a minimum facewidth under a condition where the inclination angle is 0.6 degrees, the minimum facewidth being such that the teeth of the inner-tube spindle do not contact at the tooth ends thereof under the condition where the crown radius Cr is given. B=18×exp(0.001×Cr) [mm] is a curved, line obtained by connecting a large number of points each of which is a set of a crown radius Cr and a. minimum facewidth under a condition, where a given inclination, angle is set within, the range of 0.6 degrees to 1.6 degrees, the crown radius Cr being such that tooth-root bending stress to be applied to the inner-tube gear portion is a maximum allowable value, the minimum facewidth being such that the teeth of the spindle inner tube do not contact at the tooth ends thereof under the condition where the crown radius Cr is given, and B=19×Cr 0.292 [mm] is a curved line obtained by connecting a large number of points each of which is a set of a given crown radius Cr and a minimum facewidth under a condition where a given inclination angle is sec within the range of 0.6 degrees to 1.6 degrees, and a backlash required for the combination of the crown radius Cr and the facewidth B is an allowable maximum backlash between the inner-tube gear portion and the outer-tube gear portion, the minimum facewidth being such that the teeth of the inner-tube spindle do not contact at the tooth ends thereof under the condition where the crown radius Cr is given. 5. The gear spindle according to claim P characterized in that shot blasting is performed on tooth surfaces. 6. The gear spindle according to claim 1 , characterized in that manganese phosphate coating treatment is performed on tooth surfaces. 7. The gear spindle according to claim 1 , characterized in that molybdenum disulfide coating treatment is performed on tooth surfaces. 8. The gear spindle according to claim 1 , characterized in that tooth surface lubricant and tooth surfaces of the spindle outer tube and the spindle inner tube are forcibly cooled by spraying cooling fluid onto outer surfaces of the spindle outer tube and the spindle inner tube. 9. The gear spindle according to claim 1 , characterized in that given that a pitch circle diameter of the inner-tube gear portion is D P [mm], a gear pressure angle is α [degree], a gear module is Mn [mm], the crown radius is Cr [mm], the facewidth is B [mm], a minimum diameter of a portion from a tooth end portion of the inner-tube spindle to a neck portion thereof is d [mm], and a radius of curvature of an arc shape given at a tooth tip is R=Cr×tan α[mm], d ≥ D P - 2 × [ R - { R 2 - ( B 2 ) 2 } 1
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