Power modules with regenerative compressor wheels

Patent metadata

Field	Value
Publication number	US-11359635-B2
Application number	US-201916383628-A
Country	US
Kind code	B2
Filing date	Apr 14, 2019
Priority date	Apr 14, 2019
Publication date	Jun 14, 2022
Grant date	Jun 14, 2022

Abstract

A power module includes a turbine arranged along a rotation axis, an interconnect shaft fixed in rotation relative to the turbine, and a compressor with a regenerative compressor wheel. The regenerative compressor wheel is fixed in rotation relative to the interconnect shaft supported for rotation with the turbine about the rotation axis. Generator arrangements, unmanned aerial vehicles, and methods of generating electrical power are also described.

First claim

What is claimed is:

1. An unmanned aerial vehicle, comprising:
an airframe carrying an electrical load;
a power module, comprising:
a turbine arranged along a rotation axis;
an interconnect shaft fixed in rotation relative to the turbine; and
a compressor with a compressor wheel fixed in rotation relative to the interconnect shaft supported for rotation with the turbine about the rotation axis,
wherein
the power module is carried by the unmanned aerial vehicle and is electrically connected to the electrical load;
a fuel module in fluid communication with the power module, wherein the fuel module is a blowdown fuel module;
wherein the turbine is an impulse turbine;
an air bearing arranged axially between the turbine and the compressor wheel, the air bearing supporting the turbine and the compressor wheel for rotation about the rotation axis;
a radial compressor in fluid communication with the compressor wheel, the radial compressor arranged on a side of the compressor wheel axially opposite the turbine
a gas generator fluidly coupling the compressor wheel to the turbine;
an outlet port in fluid communication with the compressor wheel, the outlet port defined by the power module between the compressor wheel and the turbine.

2. The vehicle as recited in claim 1 , further comprising a permanent magnet generator operably connected to the turbine and arranged axially between the turbine and the compressor wheel.

3. The vehicle as recited in claim 2 , further comprising one or more permanent magnet fixed relative to the interconnect shaft.

4. The vehicle as recited in claim 2 , further comprising a stator coil or winding arranged radially outward of the interconnect shaft and in fluid communication with the compressor wheel to receive coolant therefrom.

5. The vehicle as recited in claim 1 , wherein the air bearing is in fluid communication with the compressor wheel to receive a flow of compressed air from the compressor wheel.

6. The vehicle as recited in claim 1 , wherein the air bearing is a first air bearing and further comprising:
a second air bearing supporting the turbine and the compressor wheel for rotation about the rotation axis; and
a permanent magnet generator arranged axially between the first air bearing and the second air bearing, wherein the second air bearing is in fluid communication with the compressor wheel through both the first air bearing and the permanent magnet generator.

7. The vehicle as recited in claim 1 , further comprising a diffuser arranged axially between the radial compressor and the compressor wheel.

8. The vehicle power module as recited in claim 1 , the fuel module in fluid communication with the gas generator, the fuel module comprising:
a charge of liquid fuel contained within a fuel pressure vessel; and
a charge of compressed gas in fluid communication with the turbine through the fuel pressure vessel, the charge of compressed gas pressurizing the charge of liquid fuel.

9. The vehicle as recited in claim 1 , wherein the turbine includes a single turbine stage.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Himmelmann Richard A

Classifications

• B64U50/14

  ducted or shrouded · CPC title

• B64U10/10

  Rotorcrafts · CPC title

• B64U50/19

  using electrically powered motors · CPC title

• B64U50/34

  In-flight charging (photovoltaics B64U50/31) · CPC title

• B64U30/20

  Rotors; Rotor supports · CPC title