Conformal pylon/boom prop-rotors

Patent metadata

Field	Value
Publication number	US-11465737-B1
Application number	US-202016818524-A
Country	US
Kind code	B1
Filing date	Mar 13, 2020
Priority date	Mar 13, 2019
Publication date	Oct 11, 2022
Grant date	Oct 11, 2022

Abstract

A vertical lift rotor propulsor assembly comprises a boom having a casing with a casing profile and a first propeller blade having a blade profile that corresponds substantially to at least a portion of the casing profile of the casing of the boom. A drive mechanism is at least partially housed within the boom and at the first propeller blade is rotatably mounted to the drive mechanism to be driven thereby. The drive mechanism is to operationally move the first propeller blade between a stowed position in which the first propeller blade is substantially flush with the casing of the boom, and a deployed position in which the first propeller blade is extended a determined distance from the casing of the boom.

First claim

What is claimed is:

1. A vertical lift rotor propulsor assembly comprising:
a wing-mounted boom having a casing with a casing profile;
a first propeller blade having a blade profile that corresponds substantially to at least a portion of the casing profile of the casing of the boom, the first propeller blade having a vertically-aligned axis of rotation; and
a drive mechanism at least partially housed within the boom and to which the first propeller blade is rotatably mounted, the drive mechanism to operationally translate the first propeller blade vertically between a stowed position in the boom and a deployed position, wherein, when in the stowed position, a lower surface of the first propeller blade conforms to a recess in the boom and an upper surface of the first propeller blade is substantially flush with an upper surface of the casing of the boom, and, wherein, in the deployed position, the first propeller blade is extended a determined distance above the casing of the boom and can be rotated in order to provide vertical lift.

2. The vertical lift rotor propulsor assembly of claim 1 , wherein the casing defines a recess having a shape substantially corresponding to the blade profile of the first propeller blade, the recess operationally to receive the first propeller blade when in the stowed position.

3. The vertical lift rotor propulsor assembly of claim 2 , wherein the recess is defined within a surface of the casing.

4. The vertical lift rotor propulsor assembly of claim 1 , wherein the drive mechanism is to rotate the first propeller blade in the deployed position in order to provide vertical lift to an aircraft.

5. The vertical lift rotor propulsor assembly of claim 1 , including a second propeller blade having a blade profile that also corresponds substantially to at least a portion of the casing profile of the casing of the boom, the first and second propeller blades being rotatably mounted in a diametrically opposite arrangement to the drive mechanism.

6. The vertical lift rotor propulsor assembly of claim 1 , wherein the drive mechanism comprises an electric motor and an extendable driveshaft that is operationally driven by the electric motor, the extendable driveshaft being extendable and retractable relative the boom to move the first propeller blade between the stowed position and the deployed position.

7. The vertical lift rotor propulsor assembly of claim 6 , wherein the extendable driveshaft is operationally to raise the first propeller blade above an upper surface of the casing of the boom when translating the first propeller blade to the deployed position.

8. The vertical lift rotor propulsor assembly of claim 7 , wherein the extendable driveshaft is operationally to lower the first propeller blade below an upper surface of the casing of the boom when translating the first propeller blade to the stowed position.

9. The vertical lift rotor propulsor assembly of claim 1 , wherein the determined distance that the first propulsor blade is raised from the casing is equal to or exceeds a chord length of the first blade.

10. The vertical lift rotor propulsor assembly of claim 1 , wherein the drive mechanism comprises a telescoping driveshaft.

11. A method of manufacturing a conformal prop-rotor assembly,
the method comprising:
providing a wing-mountable boom having a casing having a casing profile;
forming at least one propeller blade to have a blade profile that corresponds substantially to at least a portion of the casing profile of the casing of the boom, the at least one propeller blade having a vertically-aligned axis of rotation in use;
securing the at least one propeller blade to a drive mechanism; and
mounting the drive mechanism within the boom, the drive mechanism operationally to rotate the at least one propeller blade to provide vertical lift to an aerial vehicle, and the drive mechanism further operationally to translate the at least one propeller blade vertically between a stowed position in the boom and a deployed position, wherein, when in the stowed position, a lower surface of the at least one propeller blade conforms to a recess in the boom and an upper surface of the at least one propeller blade is substantially flush with an upper surface of the casing of the boom and, wherein, in the deployed position, the at least one propeller blade is extended a determined distance above the casing of the boom.

12. The method of claim 11 , wherein the forming of the at least one propeller blade comprises modifying at least one of rake, skew, or sweep of the at least one propeller blade to modify the blade profile to correspond substantially to the portion of the casing profile of the casing of the boom.

13. The method of claim 11 , comprising forming a recess within the casing of the boom to operationally receive the at least one propeller blade when in the stowed position, the recess having a shape corresponding substantially to a shape of the at least one propeller blade.

14. The method of claim 11 , including forming a second propeller blade having a blade profile that corresponds to a second portion of the casing profile of the casing of the boom.

15. The method of claim 11 , wherein the drive mechanism comprises an electric motor and an extendable driveshaft, and the method comprises forming the extendable driveshaft to operationally extend the at least one propeller blade a determined distance from an upper surface of the casing of the boom.

16. The method of claim 11 , wherein the drive mechanism comprises a telescoping driveshaft.

Assignees

• Joby Aero Inc

Inventors

• Mcdonald Robert Alan

Classifications

• B64C29/0091

  Accessories not provided for elsewhere · CPC title

• B64C29/0033 Primary

  the propellers being tiltable relative to the fuselage · CPC title

• B64C29/0025

  the propellers being fixed relative to the fuselage · CPC title

• B64C13/18

  using automatic pilot · CPC title

• B64C11/28

  Collapsible or foldable blades · CPC title