Propeller

Patent metadata

Field	Value
Publication number	US-9849968-B2
Application number	US-201414560964-A
Country	US
Kind code	B2
Filing date	Dec 4, 2014
Priority date	Dec 4, 2014
Publication date	Dec 26, 2017
Grant date	Dec 26, 2017

Abstract

A propeller includes a hub coaxially surrounding a longitudinal axis. A ring shroud coaxially surrounds the longitudinal axis and is spaced radially from the hub. At least one propeller blade is fixedly attached to both the hub and ring shroud and extends radially therebetween for mutual rotation therewith. At least one stub blade has a first stub end radially spaced from a second stub end. The first stub end is fixedly attached to a selected one of the hub and ring shroud. The second stub end is cantilevered from the first stub end and is radially interposed between the first stub end and the selected one of the hub and ring shroud.

First claim

We claim:

1. A propeller, comprising:
a hub coaxially surrounding a longitudinal axis;
a ring shroud coaxially surrounding the longitudinal axis and spaced radially from the hub;
at least one propeller blade fixedly attached to both the hub and ring shroud and extending radially therebetween for mutual rotation therewith, each propeller blade being angled in a first twist direction; and
at least one stub blade having a first stub end radially spaced from a second stub end, the first stub end being fixedly attached to a selected one of the hub and ring shroud, and the second stub end being cantilevered from the first stub end and radially interposed between the first stub end and the selected one of the hub and ring shroud, each stub blade being angled in a second twist direction which is substantially opposite the first twist direction.

2. The propeller of claim 1 , including a plurality of propeller blades and a plurality of stub blades, the propeller blades being circumferentially spaced about a perimeter of the hub, and each circumferentially adjacent pair of propeller blades having at least one stub blade interposed circumferentially therebetween.

3. A propeller, comprising:
a hub coaxially surrounding a longitudinal axis;
a ring shroud coaxially surrounding the longitudinal axis and spaced radially from the hub; and
a plurality of motive blades extending radially across at least a portion of the distance between the hub and the ring shroud, each motive blade having a blade root directly attached to a chosen one of the hub and the ring shroud, for rotation about the longitudinal axis due to the attachment to the chosen one of the hub and the ring shroud, and a blade tip extending toward the other one of the hub and the ring shroud, at least one selected motive blade of the plurality of motive blades being angled in a first twist direction, and at least one other motive blade of the plurality of motive blades being angled in a second twist direction which is substantially opposite the first twist direction;
wherein at least one selected blade tip is directly attached to the other one of the hub and the ring shroud; and
wherein at least one other blade tip is cantilevered from the blade root and is radially spaced apart from the other one of the hub and the ring shroud.

4. The propeller of claim 3 , wherein at least one motive blade having a blade tip directly attached to the other one of the hub and the ring shroud is directly circumferentially adjacent to at least one motive blade having a blade tip cantilevered from the blade root and radially spaced apart from the other one of the hub and the ring shroud.

5. The propeller of claim 3 , wherein at least one motive blade of the plurality of motive blades which is angled in the first twist direction is directly circumferentially adjacent to at least one motive blade of the plurality of motive blades which is angled in the second twist direction.

6. An aircraft comprising:
a body;
at least one fixed wing and at least one propeller mount extending from the body;
at least one drive shaft positioned within a corresponding one of the at least one propeller mount and drivable by a motor or gear/clutch system; and
at least one propeller operationally attached to the at least one drive shaft to obtain motive power therefrom, the propeller comprising
a hub coaxially surrounding a longitudinal axis,
a ring shroud coaxially surrounding the longitudinal axis and spaced radially from the hub, and
a plurality of motive blades extending radially across at least a portion of the distance between the hub and the ring shroud, each motive blade having a blade root directly attached to a chosen one of the hub and the ring shroud, for rotation about the longitudinal axis, under motive power from the drive shaft, due to the attachment to the chosen one of the hub and the ring shroud, and a blade tip extending toward the other one of the hub and the ring shroud, at least one selected motive blade of the plurality of motive blades being angled in a first twist direction, and at least one other motive blade of the plurality of motive blades being angled in a second twist direction which is substantially opposite the first twist direction,
wherein at least one selected blade tip is directly attached to the other one of the hub and the ring shroud, and
wherein at least one other blade tip is cantilevered from the blade root and is radially spaced apart from the other one of the hub and the ring shroud.

Assignees

• Linch Jonathon J
• Rahrig Kyle M
• Northrop Grumman Systems Corp

Inventors

• Linch Jonathon J
• Rahrig Kyle M

Classifications

• B64U50/14

  ducted or shrouded · CPC title

• B64C11/001 Primary

  Shrouded propellers · CPC title

• B64C39/10

  All-wing aircraft · CPC title

• B64C2039/105

  of blended wing body type · CPC title

• B64C2220/00

  Active noise reduction systems · CPC title