Aircraft capable of vertical and short take-off and landing

• US 7,267,300 B2
• Filed: 02/25/2005
• Issued: 09/11/2007
• Est. Priority Date: 02/25/2005
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Gilbert, Ronald E., Hansen, Terrell W., Heath, Gregory F., Slaughter, Stephen C.
• Primary Examiner(s): Holzen; Stephen A
• Application Number:
  US11/065,855
• Publication Number:
  US 20060192046A1
• Time in Patent Office: 928 Days
• Field of Search: 244 121- 23 D, 244/23.R
• US Class Current: 244/12.3
• CPC Class Codes: B64C 15/14 the jets being other than main propulsion jets jet flaps B64C9/38
• CPC Class Codes: B64C 29/0025 the propellers being fixed relative to the fuselage
• CPC Class Codes: B64D 35/04 characterised by the transmission driving a plurality of propellers or rotors
• CPC Class Codes: F16H 1/222 with non-parallel axes

Abstract

Aircraft comprising an airframe having a forward end, an aft end opposite the forward end, a top extending between the forward end and the aft end, and a bottom opposite the top side. The aircraft further includes a power plant mounted on the airframe. In addition, the aircraft includes at least two propellers rotatably mounted on the airframe and powered by the power plant for moving the aircraft in a generally forward direction during operation of the propellers. Also, the aircraft includes at least two counter-rotatable fan sets mounted on the airframe and powered by the power plant for providing upward lift to the aircraft during operation of the fan sets.

Claims

1. An aircraft comprising:

an airframe having a forward end, and an aft end opposite said forward end;

a power plant mounted on the airframe;

at least two propellers rotatably mounted on the airframe and powered by the power plant for moving the aircraft in a generally forward direction during operation of said propellers, each propeller having an axis of rotation that extends approximately parallel with a longitudinal axis extending between the forward and aft ends of the airframe;

at least two counter-rotatable fans sets mounted on the airframe and powered by the power plant for providing upward lift to the aircraft during operation of said fan sets;

wherein the airframe comprising a fuselage and at least two wings extending laterally from the fuselage;

a nose is positioned at the forward end of the airframe;

at least one of said propellers is positioned on each of said wings;

at least one of said counter-rotatable lift fan sets is positioned on each of said wings;

at least one of said counter-rotatable lift fan set is disposed in the nose;

each of said propellers has a plurality of propeller blades; and

each of said fans sets has a plurality of fan blades.

2. The aircraft as set forth in claim 1 further comprising at least one of avionic equipment, navigational equipment, ordinance, and observation equipment mounted on the airframe, and wherein the aircraft is adapted for unmanned flight.

3. The aircraft as set forth in claim 1 further comprising:

a transfer gearbox mounted on the airframe;

a main torque shaft operatively connecting the transfer gear box to the power plant for delivering torque to the gear box from the power plant;

a wing torque shaft operatively connecting the transfer gear box to each of said lift fan sets mounted on the wings for delivering torque to the respective lift fan sets from the gear box;

a nose torque shaft operatively connecting the transfer gear box to said lift fan set mounted in the nose for delivering torque to the respective lift fan set from the gear box; and

a propeller shaft operatively connecting each of said lift fan sets mounted on the wings to the corresponding propeller for delivering torque to the respective propeller.

4. The aircraft as set forth in claim 1 further comprising at least one idler operatively connected to one of the lift fan sets for controlling torque distribution amongst the fan sets and propellers during operation.

5. The aircraft as set forth in claim 4 wherein the power plant is of a type selected from the group consisting of:

an internal combustion engine, an electric motor, and a hybrid motor.

6. The aircraft as set forth in claim 1 further comprising wherein each of said fan blades has an adjustable pitch angle, each of said propeller blades has an adjustable pitch angle, and said aircraft further comprises a control system for controlling the pitch angles of the fan blades and the pitch angles of the propeller blades during operation.

7. The aircraft as set forth in claim 6 wherein the pitch angles of the propeller blades and the fan blades are adjustable between an angle of about 0°

and 45°

during operation.

8. The aircraft as set forth in claim 7 wherein the propeller blades and fan blades each comprise a shape memory alloy and are swept to an inherent pitch angle of between about 21°

and 24°

.

9. The aircraft as set forth in claim 7 wherein each of the propeller blades and each of the fan blades comprises a composite matrix having embedded piezoelectric smart actuator fibers.

10. An aircraft comprising:

an airframe having a forward end, and an aft end opposite said forward end;

a power plant mounted on the airframe;

at least two ducted ring fans mounted on the airframe between the forward end and the aft end for providing lift to the aircraft;

a fan shaft connecting the power plant to at least one of said ducted ring fans to provide lift during use;

at least two propellers mounted on the airframe for providing forward thrust to the aircraft, the propellers having an axis of rotation that extends approximately parallel with a longitudinal axis extending between the forward and aft ends of the airframe;

a propeller shaft connecting the power plant to at one propeller for powering the propeller to provide thrust during use;

wherein the airframe comprising a fuselage and at least two wings extending laterally from the fuselage;

a nose is positioned at the forward end of the airframe;

at least one of said two propellers is positioned on at least one of said wings;

wherein said at least one of said ducted ring fans is a counter-rotatable lift fan, and at least one ducted ring fan is positioned on each of said wings;

at least one of said ducted ring fans is disposed in the nose.