Engine exhaust duct mounting assembly

Patent metadata

Field	Value
Publication number	US-10279924-B2
Application number	US-201715593956-A
Country	US
Kind code	B2
Filing date	May 12, 2017
Priority date	May 12, 2017
Publication date	May 7, 2019
Grant date	May 7, 2019

Abstract

A mounting assembly for mounting a portion of an engine exhaust duct in an opening of an airframe panel aircraft, including a peripheral flange disposed on the portion of the exhaust duct, and at least one mounting member having an outer peripheral flange portion for connection to the airframe panel and having an inner peripheral flange portion with at least one compliant isolator member to receive the peripheral flange of the exhaust duct in a manner that suspends the exhaust duct in the opening away from the airframe panel and accommodates thermal expansion and contraction of the exhaust duct relative to the airframe panel. Embodiments include a method of mounting an engine exhaust duct in an opening of an outer airframe panel of an aircraft.

First claim

What is claimed is:

1. A mounting assembly for mounting a portion of an engine exhaust duct in an opening of an airframe panel aircraft, comprising:
an exhaust duct flange disposed on the portion of the exhaust duct, and
at least one mounting member comprising a first mounting plate and a second mounting plate connected to the first mounting plate with at least one compliant isolator member disposed therebetween; the first mounting plate having an outer peripheral flange portion for connection to the airframe panel and the first mounting plate and the second mounting plate with the at least one compliant isolator member having an inner peripheral flange portion configured to receive the exhaust duct flange in a manner that suspends the exhaust duct in the opening away from the airframe panel and accommodates thermal expansion and contraction of the exhaust duct relative to the airframe panel.

2. The assembly of claim 1 , wherein the at least one compliant isolator member includes a peripheral slot into which at least an outermost portion of the exhaust duct flange is received.

3. The assembly of claim 2 , wherein the slot comprises an inner portion for receiving the exhaust duct flange and an outer portion opposite from the inner portion.

4. The assembly of claim 3 , wherein the slot further comprises a clearance space in the outer portion.

5. The assembly of claim 1 , wherein the first mounting plate and the second mounting plate each includes a respective first planar surface and a second planar surface between which the at least one compliant isolator member is disposed.

6. The assembly of claim 1 , wherein the at least one compliant isolator member comprises a first compliant isolator ring connected to the first mounting plate and a second compliant isolator ring connected to the second mounting plate to define a slot therebetween in which the exhaust duct flange is received.

7. The assembly of claim 6 , wherein the slot comprises an inner portion for receiving the exhaust duct flange and an outer portion opposite from the inner portion.

8. The assembly of claim 7 , wherein the slot further comprises a clearance space in the outer portion.

9. The assembly of claim 1 , wherein the at least one compliant isolator member comprises a metallic encapsulated insulation material.

10. The assembly of claim 1 , wherein the at least one mounting member comprises an aluminum alloy.

11. A combination of a composite outer airframe panel and the mounting assembly of claim 1 including mounting the portion of the exhaust duct of a power unit in the opening of the outer airframe panel.

12. The combination of claim 11 , wherein the airframe panel comprises a carbon-carbon composite.

13. The combination of claim 11 , wherein the power unit comprises an auxiliary power unit.

14. A method of mounting an engine exhaust duct in an opening of an outer airframe panel of an aircraft, comprising:
connecting a flange to the outer periphery of the exhaust duct;
connecting an outer peripheral flange portion of at least one mounting member to the outer airframe panel; and
suspending the flange of the exhaust duct on at least one compliant isolator member disposed on an inner peripheral flange portion of the at least one mounting member to space the exhaust duct in the opening away from the airframe panel and to accommodate thermal expansion and contraction of the exhaust duct relative to the airframe panel.

15. The method of claim 14 , wherein the at least one compliant isolator member comprises a first compliant isolator member connected to a first mounting plate and a second compliant isolator member connected to a second mounting plate to define a peripheral slot therebetween in which a portion of the flange of the exhaust duct is received.

16. The method of claim 15 , wherein the slot comprises an inner portion for receiving the peripheral flange and an outer portion opposite from the inner portion.

17. The method of claim 16 , wherein the slot further comprises a clearance space in the outer portion.

18. The method of claim 14 , wherein the at least one compliant isolator member comprises a metallic encapsulated insulation material.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Rosado Angel David

Classifications

• B64C2001/0072

  from composite materials · CPC title

• F05D2260/30

  Retaining components in desired mutual position · CPC title

• B64D2041/002

  Mounting arrangements for auxiliary power units (APU's) · CPC title

• B64D33/04 Primary

  of exhaust outlets or jet pipes · CPC title

• F02C7/20

  Mounting or supporting of plant; Accommodating heat expansion or creep · CPC title