Rotating sealing systems

Patent metadata

Field	Value
Publication number	US-10322797-B2
Application number	US-201514636896-A
Country	US
Kind code	B2
Filing date	Mar 3, 2015
Priority date	Mar 3, 2015
Publication date	Jun 18, 2019
Grant date	Jun 18, 2019

Abstract

A rotating sealing system includes a non-metallic rotating seal configured to be attached to a rotating shaft. The rotating seal is configured to rotate with the rotating shaft about an axis. The rotating sealing system includes a stationary sealing surface configured to be attached to a stationary housing positioned around the rotating shaft. The stationary sealing surface is substantially parallel to the axis. The rotating seal is configured to seal with the stationary sealing surface as the rotating shaft rotates.

First claim

The invention claimed is:

1. A rotating sealing system for a rotorcraft comprising:
a stationary vertical housing having an open end;
a vertical rotor mast configured to rotate within the stationary vertical housing about a vertical axis, wherein the vertical rotor mast has a first end extending through the open end of the stationary vertical housing and a second end coupled to a gearbox;
a cover removably attached to the open end of the stationary vertical housing, wherein the cover has a central hole that forms a gap between the vertical rotor mast and the cover;
an L-shaped seal holder having a first portion attached to the vertical rotor mast within the stationary vertical housing below the cover and the gap, and a second portion extending outwards from the vertical rotor mast;
a rotating seal attached to and held in place by the L-shaped seal holder, the rotating seal comprising an elastomeric part having one or more protruded portions, and an L-shaped metallic part inserted in the elastomeric part;
the L-shaped metallic part configured to increase a stiffness or rigidness of the rotating seal, and the L-shaped metallic part having a first portion substantially parallel to the vertical rotor mast and having a second portion extending outward beyond the L-shaped seal holder towards a stationary seal, and wherein the first portion of the L-shaped metallic part is positioned between the second portion of the L-shaped metallic part and the second portion of the L-shaped seal holder; and
the stationary seal attached to an interior of the stationary vertical housing, the stationary seal having a substantially cylindrical shape with a stationary sealing surface substantially parallel to the vertical axis, wherein the one or more protruded portions of the rotating seal is configured to seal with the stationary sealing surface as the vertical rotor mast rotates.

2. The system of claim 1 , wherein:
the vertical rotor mast has a first end coupled to a rotor and a second end coupled to a gearbox.

3. The system of claim 1 , wherein the vertical rotor mast is configured to rotate at approximately 400 rpm or less.

4. The system of claim 1 , wherein the stationary seal comprises a metallic material, a composite material, or an elastomeric material.

5. A method for sealing a vertical rotor mast of a rotorcraft, the method comprising:
providing a stationary vertical housing having an open end, and the vertical rotor mast configured to rotate within the stationary vertical housing about a vertical axis, wherein the vertical rotor mast has a first end extending through the open end of the stationary vertical housing and a second end coupled to a gearbox;
providing a cover having a central hole configured to form a gap between the vertical rotor mast and the cover when attached to the open end of the stationary vertical housing;
attaching a first portion of an L-shaped seal holder to the vertical rotor mast within the stationary vertical housing below where the cover and the gap will be when attached, the L-shaped seal holder configured to rotate with the vertical rotor mast and having a second portion extending outwards from the vertical rotor mast;
attaching a rotating seal to the L-shaped seal holder, the rotating seal configured to rotate with the vertical rotor mast about the vertical axis, wherein the rotating seal comprises an elastomeric part and an L-shaped metallic part inserted in the elastomeric part, the elastomeric part configured to be attached to the L-shaped seal holder and having one or more protruded portions, the L-shaped metallic part configured to increase a stiffness or rigidness of the rotating seal, and the L-shaped metallic part having a first portion substantially parallel to the vertical rotor mast and having a second portion extending outward beyond the L-shaped seal holder towards a stationary seal, and wherein the first portion of the L-shaped metallic part is positioned between the second portion of the L-shaped metallic part and the second portion of the L-shaped seal holder;
attaching the stationary seal to an interior of the stationary vertical housing, the stationary seal having a substantially cylindrical shape with a stationary sealing surface being substantially parallel to the vertical axis, wherein the one or more protruded portions of the rotating seal is configured to seal with the stationary sealing surface as the vertical rotor mast rotates; and
attaching the cover to the open end of the stationary vertical housing.

6. The method of claim 5 , wherein attaching the rotating seal to the L-shaped seal holder comprises placing the rotating seal without tooling.

7. The method of claim 5 , further comprising aligning the rotating seal to the stationary sealing surface.

8. The method of claim 5 , further comprising removing the rotating seal without tooling.

9. The method of claim 5 , wherein the stationary seal comprises a metallic material, a composite material, or an elastomeric material.

10. A rotorcraft comprising:
a stationary vertical housing having an open end;
a stationary seal attached to an interior of the stationary vertical housing proximate to the open end of the stationary vertical housing;
a cover removably attached to the open end of the stationary vertical housing, the cover having a central hole;
a vertical rotor mast configured to rotate within the stationary vertical housing about a vertical axis, the vertical rotor mast having a first end coupled to a rotorcraft rotor and extending through the central hole of the cover, with a gap between the vertical rotor mast and the cover, and the vertical rotor mast having a second end coupled to a gearbox;
a single L-shaped seal holder having a first portion attached to the vertical rotor mast within the stationary vertical housing below the cover and the gap, the first portion configured to rotate with the vertical rotor mast, and the L-shaped seal holder having a second portion extending outward from the vertical rotor mast, the L-shaped seal holder holding a rotating seal in place and aligned with the stationary seal;
the rotating seal attached to the L-shaped seal holder to rotate with the vertical rotor mast, the rotating seal comprising an elastomeric part attached to the L-shaped seal holder and having one or more protruded portions, and an L-shaped metallic part disposed within the elastomeric part and configured to increase a stiffness or rigidness of the rotating seal, and the L-shaped metallic part having a first portion substantially parallel to the vertical rotor mast, and having a second portion extending outward beyond the L-shaped seal holder towards the stationary seal, and wherein the first portion of the L-shaped metallic part is positioned between the second portion of the L-shaped metallic part and the second portion of the L-shaped seal holder; and
the stationary seal having a substantially cylindrical shape with a stationary sealing surface substantially parallel to the vertical axis, and the one or more protruded portions of the rotating seal configured to seal with the stationary sealing surface as the vertical rotor mast rotates.

11. The rotorcraft of claim 10 , wherein the vertical rotor mast is configured to rotate at approximately 400 rpm or less.

12. The rotorcraft of claim 10 , wherein the stationary seal comprises a metallic material, a composite material, or an elastomeric material.

13. The rotorcraft of claim 10 , wherein the one or more protruded portions comprise two protruded portions that seal with the stationary sealing surface as the vertical rotor mast rotates.

14. The rotorcraft of claim 10 , wherein

Assignees

• Bell Helicopter Textron Inc

Inventors

• Jurrell Travis
• Cecil Timothy
• Poster Scott
• Porter Wesley

Classifications

• B64C27/32 Primary

  Rotors · CPC title

• B64C27/12

  Rotor drives · CPC title

• F16J15/3232

  having two or more lips · CPC title

• F16J15/164

  the sealing action depending on movements; pressure difference, temperature or presence of leaking fluid · CPC title

• F16J15/3256

  comprising two casing or support elements, one attached to each surface, e.g. cartridge or cassette seals · CPC title