Fluid accelerator
US-2024286756-A1 · Aug 29, 2024 · US
US9828945B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9828945-B2 |
| Application number | US-201414280592-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 17, 2014 |
| Priority date | May 17, 2014 |
| Publication date | Nov 28, 2017 |
| Grant date | Nov 28, 2017 |
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A ram air turbine is presented that includes a turbine having a blade and a turbine shaft, a strut removably coupled to the turbine, wherein the strut has a gearbox section and a drive section, a turbine shaft with a bevel gear oriented perpendicularly to the turbine shaft and positioned within the gearbox section of the strut, a driveshaft coupled to the generator and positioned within the drive section of the strut, and a pinion gear that engages with the bevel gear, wherein the pinion gear is secured to the driveshaft by a spanner nut, wherein the pinion gear utilizes a key configured to interact with the keyed joint of the driveshaft. The pinion gear is supported by a pinion bearing that may be press fit onto the pinion gear and by one of the generator bearings.
Opening claim text (preview).
What is claimed: 1. A ram air turbine comprising: a turbine comprising a blade and a turbine shaft; a one-piece strut removably coupled to the turbine, wherein the one-piece strut comprises a gearbox section, a drive section, and a generator adapter section; the turbine shaft comprising a bevel gear oriented perpendicularly to the turbine shaft and positioned within the gearbox section of the one-piece strut; a driveshaft positioned within the drive section of the one-piece strut, wherein the driveshaft comprises a first end and a second end, the driveshaft comprising a keyed joint at the first end, and the driveshaft is removably coupled to a generator at the second end, wherein the first end extends into the gearbox section and the second end extends into the generator adaptor section; a pinion gear that engages with the bevel gear and is removably secured to the driveshaft by an interference fit, wherein the pinion gear includes a key configured to interact with the keyed joint of the driveshaft to maintain a position of pinion gear relative to the driveshaft; a spanner nut coupled to the driveshaft and compressing the pinion gear against a shoulder on the driveshaft; and a pinion bearing coupled to and surrounding the pinion gear, wherein the driveshaft is supported at the first end by the pinion bearing and is supported at the second end by a generator bearing assembly located within the generator adapter section. 2. The ram air turbine of claim 1 , wherein the pinion bearing is press fit onto the pinion gear. 3. The ram air turbine of claim 1 , wherein the driveshaft comprises stainless steel. 4. The ram air turbine of claim 1 , wherein the pinion gear comprises an uncoated metal material. 5. The ram air turbine of claim 1 , further comprising a pinion bearing retainer having a seal, wherein the pinion bearing retainer maintains a position of the pinion bearing in a direction parallel to the driveshaft. 6. The ram air turbine of claim 5 , wherein the pinion bearing retainer is engaged with the strut assembly by a threaded engagement. 7. The ram air turbine of claim 1 , further comprising a cover configured to seal an end of the gearbox section opposite to the turbine. 8. A ram air turbine comprising: a turbine comprising a blade; a one-piece strut removably coupled to the turbine, wherein the one-piece strut comprises a gearbox section and a drive section; a turbine shaft comprising a bevel gear oriented perpendicularly to the turbine shaft and positioned within the gearbox section of the one-piece strut; a driveshaft positioned within the drive section and comprising a first end and a second end; a pinion gear that engages with the bevel gear, wherein the pinion gear is coupled to the first end of the driveshaft; and a generator having a bearing and a generator shaft, wherein the second end of the driveshaft is received into an end of the generator shaft, the second end comprising a spline that is complimentary to the end of the generator shaft. 9. The ram air turbine of claim 8 , wherein a shaft bending frequency of the driveshaft is greater than an operating range frequency of the turbine. 10. The ram air turbine of claim 8 , wherein a drivetrain comprises the turbine, the turbine shaft, the driveshaft, and the generator, and wherein a frequency of rotation of the drivetrain is greater than one revolution per revolution of the turbine. 11. The ram air turbine of claim 10 , wherein the driveshaft is hollow. 12. The ram air turbine of claim 11 , wherein an inner diameter of the driveshaft and an outer diameter of a driveshaft are chosen such that a torsional natural frequency of the drivetrain is less than one per revolution of the turbine. 13. The ram air turbine of claim 8 , wherein the driveshaft is solid. 14. The ram air turbine of claim 8 , wherein the gearbox section further comprises a pinion bearing retainer. 15. The ram air turbine of claim 8 , further comprising a cover configured to seal an end of the gearbox section opposite to the turbine.
in ram-air turbines ("RATS") · CPC title
of the bevel or angled type · CPC title
Preventing, counteracting or reducing vibration or noise · CPC title
Bearings · CPC title
hollow · CPC title
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