Aircraft having radially extendable tailboom assembly

Patent metadata

Field	Value
Publication number	US-11396374-B2
Application number	US-201916371375-A
Country	US
Kind code	B2
Filing date	Apr 1, 2019
Priority date	Aug 19, 2016
Publication date	Jul 26, 2022
Grant date	Jul 26, 2022

Abstract

A tail sitter aircraft includes a fuselage having a forward portion, an aft portion and a longitudinally extending fuselage axis. At least two wings are supported by the forward portion of the fuselage. A distributed propulsion system includes at least one propulsion assembly operably associated with each fixed wing and is operable to provide forward thrust during forward flight and vertical thrust during vertical takeoff, hover and vertical landing. A tailboom assembly extends from the aft portion of the fuselage and includes a plurality of rotatably mounted tail arms having control surfaces and landing members. In a forward flight configuration, the tail arms are radially retracted to reduce tail surface geometry and provide yaw and pitch control with the control surfaces. In a landing configuration, the tail arms are radially extended relative to the fuselage axis to form a stable ground contact base with the landing members.

First claim

What is claimed is:

1. A tail sitter aircraft comprising:
a fuselage having a forward portion, an aft portion and a longitudinally extending fuselage axis;
first and second fixed wings supported by the forward portion of the fuselage, the fixed wings providing a main lifting surface for the aircraft;
a distributed propulsion system including at least one propulsion assembly operably associated with each fixed wing, the distributed propulsion system operable to provide forward thrust during forward flight and vertical thrust during vertical takeoff, hover and vertical landing; and
a tailboom assembly extending from the aft portion of the fuselage, the tailboom assembly including first, second, third and fourth rotatably mounted tail arms having control surfaces and landing members;
wherein, in a forward flight configuration, the tail arms are radially retracted to reduce tail surface geometry and provide yaw and pitch control with the control surfaces; and
wherein, in a landing configuration, the tail arms are radially extended relative to one another about the fuselage axis to form a stable ground contact base with the landing members.

2. The tail sitter aircraft as recited in claim 1 wherein the first and second fixed wings are generally oppositely disposed relative to the fuselage.

3. The tail sitter aircraft as recited in claim 1 wherein the first and second fixed wings are nonrotatable relative to the fuselage.

4. The tail sitter aircraft as recited in claim 1 wherein each propulsion assembly further comprises a rotor assemblies.

5. The tail sitter aircraft as recited in claim 1 wherein the tailboom assembly further comprises an actuator assembly operable to transition the tail arms between the forward flight configuration and the landing configuration.

6. A tail sitter aircraft comprising:
a fuselage having a forward portion, an aft portion and a longitudinally extending fuselage axis;
first and second fixed wings supported by the forward portion of the fuselage and that are nonrotatable relative to the fuselage, the fixed wings providing a main lifting surface for the aircraft;
a distributed propulsion system including first and second rotor assemblies attached respectively to the first and second fixed wings, the distributed propulsion system operable to provide forward thrust during forward flight and vertical thrust during vertical takeoff, hover and vertical landing; and
a tailboom assembly extending from the aft portion of the fuselage, the tailboom assembly including first, second, third and fourth rotatably mounted tail arms having control surfaces and landing members;
wherein, in a forward flight configuration, the tail arms are radially retracted to reduce tail surface geometry and provide yaw and pitch control with the control surfaces; and
wherein, in a landing configuration, the tail arms are radially extended relative to one another about the fuselage axis to form a stable ground contact base with the landing members.

7. The tail sitter aircraft as recited in claim 6 wherein the first and second fixed wing are generally oppositely disposed relative to the fuselage.

8. The tail sitter aircraft as recited in claim 6 wherein the tailboom assembly further comprises an actuator assembly operable to transition the tail arms between the forward flight configuration and the landing configuration.

Assignees

• Textron Innovations Inc

Inventors

• Robertson Daniel Bryan
• Groninga Kirk Landon
• Fenny Carlos Alexander

Classifications

• B64U70/80

  Vertical take-off or landing, e.g. using rockets (rotorcrafts B64U10/10; VTOL aircraft B64U10/20) · CPC title

• B64U50/14

  ducted or shrouded · CPC title

• B64C25/24

  electric · CPC title

• B64C11/006

  Paddle wheels · CPC title

• B64C25/52

  Skis or runners · CPC title