Heating device and method for deployable ram air turbine

• US 6,503,056 B2
• Filed: 04/24/2001
• Issued: 01/07/2003
• Est. Priority Date: 04/24/2001
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Eccles, Steven R., Schindler, Wayne G.
• Primary Examiner(s): Look, Edward K.
• Assistant Examiner(s): NGUYEN, NINH H
• Application Number:
  US09/841,996
• Publication Number:
  US 20020154999A1
• Time in Patent Office: 623 Days
• Field of Search: 416/95, 416/142, 416/DIG.4, 416/245.R, 244/134.D, 244/134.E, 244/134.R, 310/154.01, 310/154.02
• US Class Current: 416/95
• CPC Class Codes: B64D 15/12 by electric heating electric heating elements in general H05B
• CPC Class Codes: B64D 41/007 Ram air turbines
• CPC Class Codes: F01D 25/02 De-icing means for engines having icing phenomena
• CPC Class Codes: F05D 2220/34 in ram-air turbines ("RATS")

Abstract

The heating apparatus and method for the nose fairing of a rotating blade assembly has an electrical generator connected to a heating element attached to the interior of the forward end of the nose fairing. The electrical generator has a rotor with conductor windings attached to the aft end of the rotating blade assembly hub housing. The stator of the electrical generator is attached opposite the rotor on the support structure for the hub housing with stator magnets spaced from and opposite the rotor windings. When the hub housing is rotated by for example airflow through the blades of the rotating blade assembly the rotor moves relative to the stator thereby creating an induced current in the windings. This converts the rotational energy to electrical energy to power the heater to heat the nose fairing to inhibit the formation of ice thereon.

Claims

1. In an apparatus for heating a nose fairing of a rotating blade assembly which comprises said nose faring which has a forward portion and which comprises a rotatable hub housing which extends from said nose faring to aft end and which comprises a support structure having a forward end for supporting said hub housing wherein the improvement comprises:

a rotor having an electrical conductor wound thereon, said rotor being attached at said aft end of said rotatable hub housing;

a stator having a forward portion having a magnet attached thereto, said stator being attached to said support structure forward end and wherein said magnet is positioned opposed to said rotor and spaced apart therefrom but in proximity for, in operation, generating electrical energy;

a heating element which is attached to said nose faring forward portion; and

a cable harness which extends between cable harness first and second ends which connect said rotor conductor and said heating element for providing electrical communication between said rotor conductor and said heating element and wherein said aft end of said hub housing further comprises being configured with a hole therein which is configured and positioned so that said cable harness passes through said hole and so that said cable harness traverses said hub housing so that said cable harness is not routed through relatively rotating parts and so that said cable harness first end is attached to said heating element so that said cable harness second end is attached to said conductor of said rotor.

2. The apparatus of claim 1, further comprising a sealing material positioned in said hole with said cable harness to seal said hole.

3. The apparatus of claim 1, wherein said stator forward portion is configured with a plurality of recesses formed therein and further comprises a plurality of said magnets inserted in said recesses and attached thereto.

4. The apparatus of claim 1, wherein said rotor and said stator are spaced apart in an axial direction.

5. The apparatus of claim 1, wherein said rotor and said stator are spaced apart in a radial direction.

6. The apparatus of claim 1, wherein said rotating blade assembly is a ram air turbine (RAT).

7. A method for providing, in a rotating blade assembly, a heated rotatable nose fairing, comprising the steps of:

positioning a generator rotor in a rotatable hub housing located in spaced proximity to a generator stator in a non-rotating support so that said hub is rotatable relative to said support structure;

positioning a heater element internal to the nose fairing; and

providing electrical communication between the generator rotor and the heating element.

8. The method of claim 7, wherein, in operation, an air flow through said rotating blade assembly causes rotation of the hub assembly.

9. The method of claim 7, wherein said rotor and stator are spaced apart in an axial direction.

10. The method of claim 7, wherein said rotor and stator are spaced apart in a radial direction.

11. The method of claim 7, wherein said rotating blade assembly is a ram air turbine (RAT).

12. A method for providing, in a ram air turbine (RAT) rotating blade assembly, a heated rotatable nose fairing, comprising the steps of:

positioning a generator rotor in a rotatable hub housing located in spaced proximity to a generator stator in a non-rotating support so that said hub is rotatable relative to said support structure;

positioning a heater element internal to the nose fairing; and

providing electrical communication between the generator rotor and the heating element.

13. The method of claim 12, wherein, in operation, an air flow through said rotating blade assembly causes rotation of the hub assembly.

14. The method of claim 12, wherein said rotor and stator are spaced apart in an axial direction.

15. The method of claim 12, wherein said rotor and stator are spaced apart in a radial direction.

16. In an apparatus for heating a nose fairing of a ram air turbine (RAT) rotating blade assembly which comprises said nose faring which has a forward portion and which comprises a rotatable hub housing which extends from said nose faring to an aft end and which comprises a support structure having a forward end for supporting said hub housing wherein the improvement comprises:

a rotor having an electrical conductor wound thereon, said rotor being attached at said aft end of said rotatable hub housing;

a stator having a forward portion configured with a plurality of recesses formed therein and having a plurality of magnets inserted in said recesses and attached thereto, said stator being attached to said support structure forward end and wherein said magnets are positioned opposed to said rotor and spaced apart therefrom but in proximity for, in operation, generating electrical energy;

a heating element which is attached to said nose faring forward portion;

a cable harness which extends between cable harness first and second ends which connect said rotor conductor and said heating element for providing electrical communication between said rotor conductor and said heating element and wherein said aft end of said hub housing further comprises being configured with a hole therein which is configured and positioned so that said cable harness passes through said hole and so that said cable harness traverses said hub housing so that said cable harness is not routed through relatively rotating parts and so that said cable harness first end is attached to said heating element so that said cable harness second end is attached to said conductor of said rotor; and

a sealing material positioned in said hole with said cable harness to seal said hole.

17. The apparatus of claim 16, wherein said rotor and stator are spaced apart in an axial direction.

18. The method of claim 16, wherein said rotor and stator are spaced apart in a radial direction.