Floating ducts

Patent metadata

Field	Value
Publication number	US-10823289-B2
Application number	US-201715816516-A
Country	US
Kind code	B2
Filing date	Nov 17, 2017
Priority date	Nov 17, 2017
Publication date	Nov 3, 2020
Grant date	Nov 3, 2020

Abstract

A duct interface system and method includes a duct having a first end and a second end; a first receptacle for the first end of the duct and/or a second receptacle for the second end of the duct; and one or more first seals between the first end of the duct and the first receptacle and/or one or more second seals between the second end of the duct and the second receptacle.

First claim

What is claimed is:

1. A duct interface system for a rotorcraft, comprising:
a floating duct having a first end and a second end;
a first port having a first receptacle for the first end of the floating duct;
a second port having a second receptacle for the second end of the floating duct;
one or more first seals between an interior of the first end of the floating duct and an exterior of the first receptacle;
one or more second seals between an exterior of the second end of the floating duct and an interior of the second receptacle; and
wherein the first end of the floating duct is coupled to the first receptacle of the first port without any fasteners or clamps, and the second end of the floating duct is coupled to the second receptacle of the second port without any fasteners or clamps.

2. The system of claim 1 , wherein the one or more first seals are operable to allow a first motion of the first end of the floating duct relative to the first receptacle and the one or more second seals are configured to allow a second motion of the second end of the floating duct relative to the second receptacle.

3. The system of claim 2 , wherein the first motion does not substantially break a first seal formed by the one or more first seals and the second motion does not substantially break a second seal formed by the one or more second seals.

4. The system of claim 1 , wherein the first port comprises an inlet port having the first receptacle or the second port comprises an outlet port having the second receptacle.

5. The system of claim 1 , wherein the first seal is the only device coupling the interior of the first end of the floating duct to the exterior of the first receptacle and the second seal is the only device coupling the exterior of the second end of the floating duct to the interior of the second receptacle.

6. The system of claim 1 , wherein the first receptacle is coupled to the first port comprising an inlet port.

7. The system of claim 1 , wherein the second receptacle is coupled to the second port comprising an outlet port.

8. The system of claim 1 , wherein the first seal(s) comprise a bulb seal, a compressible seal or a gasket and the second seal(s) comprise a bulb seal, a compressible seal or a gasket.

9. A method of interfacing a floating duct for a rotorcraft, comprising:
providing a floating duct having a first end and a second end, and a first port having a first receptacle for the first end of the floating duct and a second port having a second receptacle for the second end of the floating duct;
using one or more first seals to substantially seal an interior of the first end of the floating duct at an exterior of the first receptacle of the first port without any fasteners or clamps; and
using one or more second seals to substantially seal an exterior of the second end of the floating duct at an interior of the second receptacle of the second port without any fasteners or clamps.

10. The method of claim 9 , further comprising configuring the one or more first seals to substantially seal the first end of the floating duct at the first receptacle to allow a first motion of the first end of the floating duct relative to the first receptacle and configuring the one or more second seals to substantially seal the second end of the floating duct at the second receptacle to allow a second motion of the second end of the floating duct relative to the second receptacle.

11. The method of claim 10 , further comprising configuring the one or more first seals such that the first motion of the first end of the floating duct relative to the first receptacle does not substantially break a first seal formed by the one or more first seals and configuring the one or more second seals such that the second motion of the second end of the floating duct relative to the second receptacle does not substantially break a second seal formed by the one or more second seals.

12. The method of claim 9 , wherein the first port comprises an inlet port having the first receptacle or the second port comprises an output port having the second receptacle.

13. The method of claim 9 , wherein the one or more first seals are the only devices securing the interior of the first end of the floating duct to the exterior of the first receptacle and the one or more second seals are the only devices securing the exterior of the second end of the floating duct to the interior of the second receptacle.

14. The method of claim 9 , wherein the first receptacle is coupled to the first port comprising an inlet port.

15. The method of claim 9 , wherein the second receptacle is coupled to the second port comprising an outlet port.

16. The method of claim 9 , wherein the first seal(s) comprise a bulb seal, a compressible seal or a gasket and the second seal(s) comprise a bulb seal, a compressible seal or a gasket.

17. A rotorcraft, comprising:
a fuselage;
an engine compartment coupled to the fuselage;
an engine coupled to the engine compartment and disposed within the engine compartment;
an inlet port disposed within the fuselage, the inlet port having a first receptacle;
an outlet port disposed within the fuselage, the outlet port having a second receptacle;
a floating duct having a first end and a second end;
one or more first seals between an interior of the first end of the floating duct and an exterior of the first receptacle;
one or more second seals between an exterior of the second end of the floating duct and an interior of the second receptacle; and
wherein the first end of the floating duct is coupled to the first receptacle of the inlet port without any fasteners or clamps, and the second end of the floating duct is coupled to the second receptacle of the outlet port without any fasteners or clamps.

18. The rotorcraft of claim 17 , wherein the one or more first seals are operable to allow a first motion of the first end of the floating duct relative to the first receptacle and the one or more second seals are configured to allow a second motion of the second end of the floating duct relative to the second receptacle.

19. The rotorcraft of claim 17 , wherein the first seal is the only device coupling the interior of the first end of the floating duct to the exterior of the first receptacle and the second seal is the only device coupling the exterior of the second end of the floating duct to the interior of the second receptacle.

20. The rotorcraft of claim 17 , wherein the first seal(s) comprise a bulb seal, a compressible seal or a gasket and the second seal(s) comprise a bulb seal, a compressible seal or a gasket.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Weaver Keith David
• Angell David
• Plagianos Nicholas
• Mast Thomas

Classifications

• B64D33/04 Primary

  of exhaust outlets or jet pipes · CPC title

• F01N13/185

  the connection being realised by deforming housing, tube, baffle, plate, or parts thereof · CPC title

• F01N13/1827

  Sealings specially adapted for exhaust systems (sealings in general F16J15/00) · CPC title

• F01N2470/10

  Tubes having non-circular cross section · CPC title

• F01N13/1811

  with means permitting relative movement, e.g. compensation of thermal expansion or vibration · CPC title