Ram air turbine overspeed protection

Patent metadata

Field	Value
Publication number	US-9725185-B2
Application number	US-201313951515-A
Country	US
Kind code	B2
Filing date	Jul 26, 2013
Priority date	Aug 1, 2012
Publication date	Aug 8, 2017
Grant date	Aug 8, 2017

Abstract

A power generation system includes a ram air turbine that is connected to a generator. The power generation system may be located in a pod, for example a pod for mounting on an aircraft. The ram air turbine receives air that passes through an air path through the pod, going in through an air inlet, through the turbine to turn the turbine, and out through an air outlet. The system includes a deployable flow obstruction, such as one or more airbags, that are deployable to suddenly obstruct the flow through the air path. The obstruction may be used to cut off flow (or greatly reduce flow), when overspeed of the ram air turbine is detected. The obstruction deploys (for example, airbags deploy in an air inlet of the system) to prevent continuation of the overspeed operation of the turbine, which may damage parts of the system.

First claim

What is claimed is:

1. A power generation system comprising:
a ram air turbine;
a turbine air inlet that provides air to the ram air turbine;
a turbine air outlet that expels air that has passed through the ram air turbine, wherein the air inlet and the air outlet together define an air path that passes air through the ram air turbine; and
a deployable flow obstruction that is deployable to block at least part of the air flow through the air path;
wherein the deployable flow obstruction includes one or more airbags that inflate to obstruct the air path; and
wherein the deployable flow obstruction fully deploys in no more than on the order of 1 millisecond.

2. The power generation system of claim 1 , wherein the one or more airbags include at least one airbag that obstructs flow in the air inlet.

3. The power generation system of claim 1 , wherein the one or more airbags include at least one airbag that obstructs flow in the air outlet.

4. The power generation system of claim 1 , further comprising one or more squibs that can be fired to create pressurized gases to fill the one or more airbags.

5. The power generation system of claim 1 , wherein the turbine air inlet is part of an inlet door that also includes a cooling air inlet that provides cooling air to a heat exchanger of the power generation system.

6. The power generation system of claim 5 , wherein deployment of the deployable flow obstruction leaves unobstructed the flow of the cooling air to the heat exchanger.

7. The power generation system of claim 6 , further comprising a cooling pump that is operatively coupled to the heat exchanger, and that is powered by the turbine.

8. The power generation system of claim 5 , wherein the inlet door is openable in flight, to allow air to flow to the ram air turbine, with the one or more airbags that inflate to obstruct the air path.

9. The power generation system of claim 1 , further comprising a controller operatively coupled to the deployable flow obstruction, to control deployment of the deployable flow obstruction.

10. The power generation system of claim 9 , wherein the controller is also operatively coupled to the ram air turbine.

11. The power generation system of claim 10 , wherein the controller receives data on the ram air turbine that is provided by a tachometer that measures rotation speed of the ram air turbine.

12. The power generation system of claim 10 , wherein the controller deploys the deployable flow obstruction in response to an overspeed condition in the ram air turbine.

13. The power generation system of claim 1 , wherein the power generation system is part of a pod that is couplable to an aircraft.

14. The power generation system of claim 1 ,
wherein the turbine air inlet includes multiple openable inlet doors;
wherein the turbine air outlet includes multiple openable outlet doors;
wherein opening the inlet doors and the outlet doors creates the air path;
wherein the one or more airbags include multiple airbags that are part of the inlet doors or the outlet doors.

15. The power generation system of claim 14 , wherein the multiple airbags are parts of respective of the inlet doors.

16. The power generation system of claim 15 , wherein the inlet doors each include a cooling air inlet that provides cooling air to a heat exchanger of the power generation system, with deployment of the airbags leaving open the cooling air inlets.

17. The power generation system of claim 1 , wherein the deployable flow obstruction blocks at least 95% of air flow through the air path.

18. A method of controlling a ram air turbine, the method comprising:
monitoring the ram air turbine for occurrence of an overspeed condition in the ram air turbine; and
when an overspeed condition is detected, deploying a deployable flow obstruction in an air path that flows through the ram air turbine, to block at least some of the air flow through the air path;
wherein the deploying includes deploying one or more airbags as the deployable flow obstruction; and
wherein the deploying includes fully deploying the deployable flow obstruction in no more than on the order of 1 millisecond.

19. The method of claim 18 , wherein the deploying includes deploying the deployable flow obstruction to block at least 95% of the air flow through the air path.

Assignees

• Raytheon Co

Inventors

• Weber Richard M
• Johnson Scott E

Classifications

• F02C7/32

  Arrangement, mounting, or driving, of auxiliaries · CPC title

• Y02E10/72

  Wind turbines with rotation axis in wind direction · CPC title

• F05D2220/34

  in ram-air turbines ("RATS") · CPC title

• F03D9/00

  Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations (hybrid wind-photovoltaic energy systems for the generation of electric power H02S10/12) · CPC title

• F01D21/02

  Shutting-down responsive to overspeed · CPC title