Utilizing an air flow assembly with intermittent thruster capabilities

Patent metadata

Field	Value
Publication number	US-11697407-B2
Application number	US-202117399477-A
Country	US
Kind code	B2
Filing date	Aug 11, 2021
Priority date	Aug 12, 2020
Publication date	Jul 11, 2023
Grant date	Jul 11, 2023

Abstract

Techniques involve an air flow assembly to provide pressurized air, e.g., for use by an air-cushion vehicle (ACV) or other craft. The air flow assembly includes a volute having a central chamber, a lift duct, and a thruster duct. The air flow assembly further includes a set of guide members disposed between the central chamber and the thruster duct, and linkage coupled to the set of guide members. The linkage is constructed and arranged to transition the set of guide members between a closed configuration in which the set of guide members closes an opening between the central chamber and the thruster duct, and an opened configuration in which the set of guide members opens the opening between the central chamber and the thruster duct.

First claim

What is claimed is:

1. An air-cushion vehicle (ACV), comprising:
a vehicle frame;
a fan supported by the vehicle frame; and
an air flow assembly supported by the vehicle frame, the air flow assembly being constructed and arranged to control air flow provided by the fan, the air flow assembly including:
a volute having a central chamber, a vehicle lift duct, and a vehicle thruster duct,
a set of guide members disposed between the central chamber and the vehicle thruster duct, and
linkage coupled to the set of guide members, the linkage being constructed and arranged to transition the set of guide members between a closed configuration in which the set of guide members closes an opening between the central chamber and the vehicle thruster duct and an opened configuration in which the set of guide members opens the opening between the central chamber and the vehicle thruster duct;

wherein the volute includes a first curved periphery portion and a second curved periphery portion which define a spiral; and
wherein the set of guide members, when in the closed configuration, defines an arc that connects the first curved periphery portion and the second curved periphery portion to further define the spiral for laminar air flow from the central chamber into the vehicle lift duct.

2. An ACV as in claim 1 wherein the central chamber of the volute is constructed and arranged to guide air flow from the fan to the vehicle lift duct;
wherein the set of guide members, when in the closed configuration, blocks air flow between the central chamber and the vehicle thruster duct; and
wherein the set of guide members, when in the opened configuration, promotes air flow between the central chamber and the vehicle thruster duct.

3. An ACV as in claim 2 wherein the set of guide members, when in the opened configuration, defines a louvered structure that impinges within the central chamber to deflect air flow from the central chamber into the vehicle thruster duct.

4. An ACV as in claim 3 wherein the fan is constructed and arranged to rotate about a central fan axis; and
wherein each guide member of the set of guide members is constructed and arranged to pivot about a respective guide axis that is parallel to the central fan axis.

5. An ACV as in claim 3 wherein the set of guide members includes a first guide member constructed and arranged to pivot about a first guide axis, and a second guide member constructed and arranged to pivot about a second guide axis which is parallel to the first guide axis; and
wherein the linkage is constructed and arranged to pivot the first guide member in a clockwise direction about the first guide axis while concurrently pivoting the second guide member in a counterclockwise direction about the second guide axis, the counterclockwise direction being opposite the clockwise direction.

6. An ACV as in claim 3 wherein each guide member of the set of guide members has an arc-shaped cross section.

7. An ACV as in claim 3 wherein each guide member of the set of guide members has a front edge and a rear edge;
wherein, when the set of guide members is in the closed configuration, (i) the front edge of a second guide member of the set of guide members is covered by the rear edge of a first guide member of the set of guide members, (ii) the front edge of a third guide member of the set of guide members is covered by the rear edge of the second guide member of the set of guide members, (iii) the front edge of a fourth guide member of the set of guide members is covered by the rear edge of the third guide member of the set of guide members; and
wherein the first, second, third, and fourth guide members are ordered in series.

8. An ACV as in claim 7 wherein the front end of the first guide member is uncovered when the set of guide members is in the closed configuration.

9. An ACV as in claim 3 , further comprising:
a controller that moves the linkage from a first position in which the linkage holds the set of guide members in the closed configuration and a second position in which the linkage holds the set of guide members in the opened configuration.

10. An ACV as in claim 3 wherein the vehicle thruster duct has a first end adjacent to the central chamber and a second end distal from the central chamber;
wherein the first end of the vehicle thruster duct has a rectangular cross section; and
wherein the second end of the vehicle thruster duct has a circular cross section.

11. An ACV as in claim 10 , further comprising:
a nozzle coupled to the second end of the vehicle thruster duct to direct air flow from the vehicle thruster duct to provide horizontal thrust.

12. An ACV as in claim 11 wherein the nozzle is constructed and arranged to rotate 360 degrees about a vertical axis.

13. An ACV as in claim 11 wherein the nozzle is constructed and arranged to deflect air flow from a vertical direction by at least 75 degrees.

14. An air flow assembly to provide pressurized air for use by an air-cushion vehicle (ACV), comprising:
a volute having a central chamber, a vehicle lift duct, and a vehicle thruster duct,
a set of guide members disposed between the central chamber and the vehicle thruster duct, and
linkage coupled to the set of guide members, the linkage being constructed and arranged to transition the set of guide members between a closed configuration in which the set of guide members closes an opening between the central chamber and the vehicle thruster duct and an opened configuration in which the set of guide members opens the opening between the central chamber and the vehicle thruster duct;
wherein the volute includes a first curved periphery portion and a second curved periphery portion which define a spiral; and
wherein the set of guide members, when in the closed configuration, defines an arc that connects the first curved periphery portion and the second curved periphery portion to further define the spiral for laminar air flow from the central chamber into the vehicle lift duct.

15. An air flow assembly as in claim 14 wherein the central chamber of the volute is constructed and arranged to guide air flow from a fan to the vehicle lift duct;
wherein the set of guide members, when in the closed configuration, blocks air flow between the central chamber and the vehicle thruster duct; and
wherein the set of guide members, when in the opened configuration, promotes air flow between the central chamber and the vehicle thruster duct.

16. An air flow assembly as in claim 14 wherein the set of guide members, when in the opened configuration, defines a louvered structure that impinges within the central chamber to deflect air flow from the central chamber into the vehicle thruster duct.

17. An air flow assembly as in claim 14 wherein each guide member of the set of guide members has a front edge and a rear edge;
wherein, when the set of guide members is in the closed configuration, (i) the front edge of a second guide member of the set of guide members is covered by the rear edge of a first guide member of the set of guide members, (ii) the front edge of a third guide member of the set of guide members is covered by the rear edge of the second guide member of the set of guide members, (iii) the front edge of a fourth guide member of the set of guide members is covered by the rear edge of the third guide member of the set of guide members; and
wherein the first, second, third, and fourth guide members are ordered in series.

18. An air flow assembly as in claim 17 wherein the front end of the first guide member is un

Assignees

• Textron Systems Corp

Inventors

• Dubose William Keith
• Devalcourt Richard Kent
• Stringer Robert Austin
• Moore Robert

Classifications

• B60V1/15 Primary

  using part of the cushion-forming fluid · CPC title

• B60V3/06 Primary

  Waterborne vessels · CPC title