Variable geometry inlet for a ducted fan and method of assembling same

• US 9,297,333 B2
• Filed: 08/26/2014
• Issued: 03/29/2016
• Est. Priority Date: 08/26/2014
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Filter, Evan J.
• Primary Examiner(s): Dinh, Tien
• Assistant Examiner(s): Green, Richard R
• Application Number:
  US14/468,406
• Publication Number:
  US 20160061144A1
• Time in Patent Office: 581 Days
• US Class Current: 1/1
• CPC Class Codes: B64C 11/001 Shrouded propellers
• CPC Class Codes: B64D 2033/0286 for turbofan engines
• CPC Class Codes: B64D 33/02 of combustion air intakes air intakes for gas-turbine plants or jet-propulsion plants per se F02C7/04; air intakes for combustion engines in general F02M35/00
• CPC Class Codes: B64U 50/14 ducted or shrouded
• CPC Class Codes: F01D 25/005 Selecting particular materials
• CPC Class Codes: F01D 25/24 Casings modified for heating or cooling F01D25/14; Casing parts, e.g. diaphragms, casing fastenings casings for rotary machines or engines in general F16M ; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045
• CPC Class Codes: F02C 7/042 having variable geometry
• CPC Class Codes: F02K 1/06 Varying effective area of jet pipe or nozzle by using fluid jets to influence the jet flow F02K1/30

Abstract

A variable geometry inlet for a ducted fan is selectively transitionable between a first and second mode. The inlet includes a retractable ring that extends circumferentially about the inlet and is selectively movable between an axially extended position in the first mode and an axially retracted position in the second mode. A tube extends circumferentially proximate the retractable ring, and is pressurizable to a relatively deflated state in the first mode and to a relatively inflated state in the second mode. A stretchable skin extends circumferentially proximate the retractable ring, and is elastically deformable in at least a circumferential direction about a longitudinal axis of the fan. A leading edge of the inlet in the first mode is defined by the stretchable skin disposed against a forward edge of the retractable ring, and in the second mode by the stretchable skin disposed against at least a portion of the tube.

Claims

1. A variable geometry inlet for a ducted fan, said variable geometry inlet is selectively transitionable between a first mode and a second mode, said variable geometry inlet comprising:

a retractable ring that extends circumferentially about said variable geometry inlet, said retractable ring is selectively movable between an axially extended position in the first mode and an axially retracted position in the second mode;

a tube that extends circumferentially proximate said retractable ring, said tube is pressurizable to a relatively deflated state in the first mode and to a relatively inflated state in the second mode; and

a stretchable skin that extends circumferentially proximate said retractable ring, said stretchable skin is elastically deformable in at least a circumferential direction about a longitudinal axis of the ducted fan, wherein a leading edge of said variable geometry inlet in the first mode is defined by said stretchable skin disposed against a forward edge of said retractable ring, and said leading edge in the second mode is defined by said stretchable skin disposed against at least a portion of said tube.

2. The variable geometry inlet according to claim 1, further comprising at least one actuator that is operable to selectively axially extend and retract said retractable ring.

3. The variable geometry inlet according to claim 2, further comprising:

a track ring that is configured to be received in a plurality of slots defined in a plurality of stringers of the ducted fan; and

a plurality of circumferentially spaced struts that each extend axially between said retractable ring and said track ring, wherein said at least one actuator is coupled to said track ring.

4. The variable geometry inlet according to claim 1, wherein said stretchable skin is formed from a material that is not substantially elastically deformable parallel to the longitudinal axis of the ducted fan.

5. The variable geometry inlet according to claim 4, wherein said material from which stretchable skin is formed comprises:

an elastic base material; and

a plurality of circumferentially spaced embedded fibers that each extend along said stretchable skin in a plane in which the longitudinal axis lies.

6. The variable geometry inlet according to claim 1, wherein said relatively deflated state of said tube is an at least partially folded state.

7. The variable geometry inlet according to claim 1, wherein said leading edge is located at a first radial distance from the longitudinal axis in the first mode, and at a second radial distance from the longitudinal axis in the second mode, wherein the second radial distance differs from the first radial distance.

8. The variable geometry inlet according to claim 1, wherein said stretchable skin defines a radially inner surface and a radially outer surface of said variable geometry inlet.

9. The ducted fan according to claim 1, wherein said stretchable skin is formed from a material that is not substantially elastically deformable parallel to said longitudinal axis of said ducted fan.

10. The ducted fan according to claim 9, wherein said material from which stretchable skin is formed comprises:

an elastic base material; and

a plurality of circumferentially spaced embedded fibers that each extend along said stretchable skin in a plane in which said longitudinal axis lies.

11. A ducted fan comprising:

a generally annular body; and

a variable geometry inlet coupled to said body, said variable geometry inlet is selectively transitionable between a first mode and a second mode, said variable geometry inlet comprises;

a retractable ring that extends circumferentially about said variable geometry inlet, said retractable ring is selectively movable between an axially extended position in the first mode and an axially retracted position in the second mode;

a tube that extends circumferentially proximate said retractable ring, said tube is pressurizable to a relatively deflated state in the first mode and to a relatively inflated state in the second mode; and

a stretchable skin that extends circumferentially proximate said retractable ring, said stretchable skin is elastically deformable in at least a circumferential direction about a longitudinal axis of said ducted fan, wherein a leading edge of said variable geometry inlet in the first mode is defined by said stretchable skin disposed against a forward edge of said retractable ring, and said leading edge in the second mode is defined by said stretchable skin disposed against at least a portion of said tube.

12. The ducted fan according to claim 11, further comprising at least one actuator that is operable to selectively axially extend and retract said retractable ring.

13. The ducted fan according to claim 12, wherein said variable geometry inlet further comprises:

a track ring that is configured to be received in a plurality of slots defined in a plurality of stringers of said body; and

a plurality of circumferentially spaced struts that each extend axially between said retractable ring and said track ring, wherein said at least one actuator is coupled to said track ring.

14. The ducted fan according to claim 11, wherein said relatively deflated state of said tube is an at least partially folded state.

15. The ducted fan according to claim 11, wherein said leading edge is located at a first radial distance from said longitudinal axis in the first mode, and at a second radial distance from said longitudinal axis in the second mode, wherein the second radial distance differs from the first radial distance.

16. The ducted fan according to claim 11, wherein said stretchable skin defines a radially inner surface and a radially outer surface of said variable geometry inlet.

17. A method of assembling a ducted fan having a variable geometry inlet, wherein the variable geometry inlet is selectively transitionable between a first mode and a second mode, said method comprising:

coupling a retractable ring to a body of the ducted fan, wherein the retractable ring extends circumferentially about the variable geometry inlet and is selectively movable between an axially extended position in the first mode and an axially retracted position in the second mode;

positioning a tube to extend circumferentially proximate the retractable ring, wherein the tube is pressurizable to a relatively deflated state in the first mode and to a relatively inflated state in the second mode; and

coupling a stretchable skin to the body, wherein the stretchable skin extends circumferentially proximate the retractable ring and is elastically deformable in at least a circumferential direction about a longitudinal axis of the ducted fan, such that a leading edge of the variable geometry inlet in the first mode is defined by the stretchable skin disposed against a forward edge of the retractable ring, and the leading edge in the second mode is defined by the stretchable skin disposed against at least a portion of the tube.

18. The method according to claim 17, further comprising coupling at least one actuator to the retractable ring, wherein the at least one actuator is operable to selectively axially extend and retract said retractable ring.

19. The method according to claim 17, wherein coupling the stretchable skin to the body comprises coupling the stretchable skin formed from a material that is not substantially elastically deformable parallel to the longitudinal axis.

20. The method according to claim 17, wherein coupling the stretchable skin to the body comprises coupling the stretchable skin such that it defines a radially inner surface and a radially outer surface of the variable geometry inlet.