Tilting wing rotorcrafts and wing rotation systems
US-2021047022-A1 · Feb 18, 2021 · US
US11892275B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11892275-B2 |
| Application number | US-202217824475-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 25, 2022 |
| Priority date | May 25, 2022 |
| Publication date | Feb 6, 2024 |
| Grant date | Feb 6, 2024 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A drive mechanism for actuating a control surface of a vehicle that moves through a fluid medium. The mechanism directly translates the rotational motion provided by an input drive to a control surface that is used to direct the vehicle. The mechanism provides both weight and space savings as well as limits, if not eliminates, backlash. The angled drive mechanism may be particularly suited for use in applications such as UAV/UUV, munitions, and other relatively small platforms.
Opening claim text (preview).
What is claimed is: 1. A drive mechanism, comprising: an input drive that receives rotational input about a drive axis; an input drive hole provided in the input drive; a control surface; a control surface shaft extending from the control surface; and a control arm extending from the input drive hole; wherein rotation of the input drive about the drive axis is transmitted through the control arm to rotate the control surface shaft about a control surface shaft axis; and wherein the control arm is directly mechanically coupled to the control surface shaft. 2. The drive mechanism of claim 1 , wherein the drive axis and the control surface shaft axis are coplanar. 3. The drive mechanism of claim 1 , wherein the drive axis and the control surface shaft axis are substantially perpendicular. 4. The drive mechanism of claim 1 , wherein the input drive includes a disk with the angled hole therein; and wherein the disk is centered around and rotatable around the drive central axis. 5. The drive mechanism of claim 1 , wherein the control arm is connected to the control surface shaft via a yoke that engages diametrically opposed sides of the control surface shaft. 6. The drive mechanism of claim 1 , wherein the control arm engages a pin that passed through the control surface shaft. 7. The drive mechanism of claim 1 , wherein the control surface is selected from a fin, a rudder, an aileron, an elevator, a spoiler, a flap, a canard, and a slat. 8. The drive mechanism of claim 1 , further comprising a motor that provides rotational motion about the drive axis. 9. The drive mechanism of claim 8 , wherein the motor provides 360° of motion about the drive axis. 10. The drive mechanism of claim 8 , wherein the motor provides 180° of motion about the drive axis. 11. The drive mechanism of claim 8 , further comprising a gearbox interposed between the motor and the coupling. 12. The drive mechanism of claim 1 , wherein the input drive hole is at an angle of 30° to 50° relative to the drive axis. 13. The drive mechanism of claim 1 , further comprising a second control surface extending from the control surface shaft at an opposite end from the control surface. 14. The drive mechanism of claim 1 , further comprising: a second control surface; a second control surface shaft extending from the second control surface; and a mechanical linkage connecting the second control surface shaft to the control surface shaft such that the rotation of the coupling identically rotates the control surface shaft with the second control surface shaft. 15. A drive mechanism, comprising: an input drive that receives rotational input about a drive axis; an input drive hole provided in the input drive; a control surface; a control surface shaft extending from the control surface; and a control arm extending from the input drive hole; wherein rotation of the input drive about the drive axis is transmitted through the control arm to rotate the control surface shaft about a control surface shaft axis; and wherein the control arm rotates within the input drive hole about a control arm axis as the input drive rotates about the drive axis. 16. A drive mechanism, comprising: an input drive that receives rotational input about a drive axis; an input drive hole provided in the input drive; a control surface; a control surface shaft extending from the control surface; and a control arm extending from the input drive hole; wherein rotation of the input drive about the drive axis is transmitted through the control arm to rotate the control surface shaft about a control surface shaft axis; wherein the control arm pivots around a pivot axis through the control surface shaft; and wherein the pivot axis and the drive central axis are substantially co-planar. 17. A vehicle that includes the drive mechanism of claim 1 . 18. The vehicle of claim 17 , wherein the vehicle is a flight vehicle. 19. The vehicle of claim 17 , wherein the vehicle is an underwater vehicle. 20. A method of actuating a control surface, comprising: providing rotational movement from a motor, about a drive axis; rotating an input drive about the drive axis with the rotational movement provided by the motor; and transmitting the rotational motion of the input drive via a control arm to a control surface shaft extending from the control surface so that the control surface shaft rotates about a control surface shaft axis; wherein the control surface shaft axis is substantially perpendicular to the drive axis; and wherein the control arm is directly mechanically coupled to the control surface shaft.
Related publications grouped by family.
Answers are generated from the same data shown on this page.