Aircraft vertical lift device

• US 9,156,549 B2
• Filed: 12/29/2010
• Issued: 10/13/2015
• Est. Priority Date: 12/29/2009
• Status: Active Grant

• Current Assignee: Rolls-Royce North American Technologies, Inc. (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce North American Technologies, Inc. (Rolls-Royce Holdings Plc)
• Inventors: Vetters, Daniel Kent, Barlow, Andrew
• Primary Examiner(s): Dinh, Tien
• Assistant Examiner(s): Woldemaryam, Assres H
• Application Number:
  US12/980,420
• Publication Number:
  US 20110155859A1
• Time in Patent Office: 1,749 Days
• Field of Search: 244/17.23, 244/17.25, 244/17.27, 244/21, 244/7.C, 244/23.D, 244/23.A
• US Class Current: 1/1
• CPC Class Codes: B64C 29/0025 the propellers being fixed relative to the fuselage

Abstract

A lift device is disclosed that can be used to provide vertical lift to an aircraft or other vehicle. The lift device can include a fan that produces an airflow and a vane box that can direct the airflow. In one form the fan can be oriented at an angle relative to a reference plane in the aircraft. In another form the vane box can be oriented at an angle. The vane box can be structured to provide a maximum flow area between an aft flow vector and a forward flow vector.

Claims

1. An apparatus comprising:

an aircraft having an engine operable to provide power;

a lift fan powered by the engine and operable to provide a lift for the aircraft along a vertical axis by producing a lift fan flow stream, the lift fan having a bladed device structured to rotate about a rotational axis, the rotational axis fixed relative to the aircraft such that the rotational axis is immobile relative to an aircraft axis during the entire time of operation of the lift fan when the bladed device is rotated to produce the lift fan flow stream;

a vane box fixed relative to the aircraft such that the vane box is substantially aligned with a reference point on the aircraft and is incapable of moving relative to the aircraft during the entire time of operation of the lift fan when the bladed device is rotated to produce the lift fan flow stream, the vane box positioned downstream of the lift fan and housing a vane assembly structured to direct the lift fan flow stream in a downward direction, the vane assembly having a plurality of vanes operable to direct the fan flow stream to a vertical vector for hovering flight, a maximum aft vector for forward flight and a maximum forward vector for rearward flight; and

wherein the vane box has a maximum flow area when the plurality of vanes in the vane assembly are at a position other than the vertical vector, wherein the rotational axis of the lift fan is oriented at an angle relative to the vertical axis.

2. The apparatus of claim 1, wherein the angle of the lift fan is the same as the angle of the vane assembly.

3. The apparatus of claim 1, wherein the maximum aft vector is different than the maximum forward vector.

4. The apparatus of claim 1, wherein the aircraft includes an airflow fairing member operable to smooth the flow around a portion of a lift fan housing protruding beyond an airflow surface.

5. The apparatus of claim 1, wherein the plurality of vanes includes a reference angle that is disposed at an angle relative to the vertical axis when the aircraft is in stationary hovering flight.

6. The apparatus of claim 5, wherein the plurality of vanes are aligned in a common plane.

7. The apparatus of claim 1, wherein the vane box is oriented at an angle relative to the vertical axis, and wherein the maximum flow area of the vane box is between the vertical vector and the maximum aft vector.

8. The apparatus of claim 1, which further includes a diffuser disposed between the lift fan and the vane assembly.

9. An apparatus comprising:

a lift fan structured to be powered by an engine and having a bladed device structured to rotate about a rotational axis, the lift fan sized so that it is operable to provide a lift for an aircraft along a vertical axis of the aircraft through production of a lift fan flow stream;

a vane box fixed at an angle to the vertical axis during the entire time of rotation of the lift fan from spool up to spool down when it is producing a lift fan flow stream such that the angle is constrained from pivoting movement, the vane box positioned downstream of the lift fan and housing a vane assembly structured to direct the lift fan flow stream in a downward direction, the vane assembly having a plurality of vanes operable to direct the fan flow stream to a vertical vector for hovering flight, a maximum aft vector for forward flight and a maximum forward vector for rearward flight; and

wherein the vane box has a maximum flow area when the plurality of vanes in the vane assembly are at a position other than the vertical vector, wherein the rotational axis of the lift fan is oriented at an angle relative to the vertical axis.