IP Library Granted Patent US 7,188,477
Granted Patent B2
US 7,188,477 · App. 10/830,272 · Granted Mar 13, 2007

High temperature dynamic seal for scramjet variable geometry

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Quick Facts
Patent No.
US 7,188,477
App. No.
10/830,272
Granted
Mar 13, 2007
Kind
B2
Abstract

A seal assembly for use in an engine, such as a scramjet engine, having a movable element, such as inlet cowl flap, is provided. The movable element has an outboard structural member which requires thermal protection. The seal assembly includes a sealing element and a support block for thermally isolating the outboard structural member and for supporting the sealing element. In a preferred embodiment, the sealing element comprises a rope seal having a tadpole construction.

Claims (56)

1. An engine comprising:

a movable element;

said movable element having a pair of sides and a cavity in each of said sides;

a seal assembly adjacent each of said sides; and

each said seal assembly comprising a support block which fits into said cavity and a sealing member supported by said support block.

2. An engine comprising:

a movable element;

said movable element having a pair of sides and a cavity in each of said sides;

a seal assembly adjacent each of said sides;

each said seal assembly comprising a support block which fits into said cavity and a sealing member supported by said support block; and

said sealing member comprising a rope seal which sits on a shelf portion of said support block.

3. An engine according to claim 2 , wherein said rope seal has a tadpole construction.

4. An engine according to claim 2 , wherein said rope seal has means for retaining said rope seal in position.

5. An engine according to claim 4 , wherein said retaining means comprises a tail on said rope seal.

6. An engine according to claim 2 , wherein said rope seal has a fiber core and a cloth like overbraid surrounding said fiber core.

7. An engine comprising:

a movable element;

said movable element having a pair of sides and a cavity in each of said sides;

a seal assembly adjacent each of said sides;

each said seal assembly comprising a support block which fits into said cavity and a sealing member supported by said support block; and

said movable element having an inner heat exchange panel and an outer heat exchange panel and an outboard structural member.

8. An engine according to claim 7 , further comprising an engine sidewall and said sealing member being sandwiched between said inner and outer heat exchange panels and the engine sidewall.

9. An engine according to claim 7 , wherein said support block extends out past edges of said inner and outer heat exchange panels.

10. An engine comprising:

a movable element;

said movable element having a pair of sides and a cavity in each of said sides;

a seal assembly adjacent each of said sides;

each said seal assembly comprising a support block which fits into said cavity and a sealing member supported by said support block; and

said support block being formed from an insulating material so as to thermally insulate an outboard structural member of said movable element.

11. An engine comprising:

a movable element;

said movable element having a pair of sides and a cavity in each of said sides;

a seal assembly adjacent each of said sides;

each said seal assembly comprising a support block which fits into said cavity and a sealing member supported by said support block; and

said engine being a scramjet engine and said movable element is a movable cowl inlet flap.

12. A seal assembly for use in an engine with a movable element and an outboard structural member, said seal assembly comprising:

a sealing element; and

means for thermally isolating said outboard structural member and for supporting said sealing element, said thermally isolating means being formed from a material selected from the group consisting of a ceramic matrix composite material and a monolithic ceramic material.

13. A seal assembly for use in an engine with a movable element and an outboard structural member, said seal assembly comprising:

a sealing element;

means for thermally isolating said outboard structural member and for supporting said sealing element, said thermally isolating and supporting means being formed from a material selected from the group consisting of a ceramic matrix composite material and a monolithic ceramic material; and

said sealing element comprising a rope seal which surrounds said thermally isolating and supporting means.

14. A seal assembly for use in an engine with a movable element and an outboard structural member, said seal assembly comprising:

a sealing element;

means for thermally isolating said outboard structural member and for supporting said sealing element, said thermally isolating and supporting means being formed from a material selected from the group consisting of a ceramic matrix composite material and a monolithic ceramic material; and

said sealing element comprising a rope seal which surrounds said thermally isolating and supporting means,

wherein said rope seal has a tail structure for retaining said rope seal in position.

15. A seal assembly according to claim 14 , wherein said rope seal has a fiber core and an overbraid material surrounding said fiber core.

16. A seal assembly according to claim 15 , wherein said tail structure is formed from said overbraid material.

17. A seal assembly for use in an engine with a movable element and an outboard structural member, said seal assembly comprising:

a sealing element;

means for thermally isolating said outboard structural member and for supporting said sealing element;

said means for thermally isolating said outboard structural member and for supporting said sealing element comprising a support block formed from an insulating material; and

said outboard structural member having a cavity and said support block being sized to fit within said cavity.

18. A seal assembly according to claim 17 , wherein said support block has a shelf for supporting said sealing element.

19. A support block for use in a seal assembly to support a rope seal, said support block being formed from an insulating material and having a shelf means for supporting said rope seal, and said insulating material being selected from the group consisting of a ceramic matrix composite material and a monolithic ceramic material.

Assignments (9)
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT (AS SUCCESSOR AGENT TO WELLS FARGO BANK, NATIONAL ASSOCIATION (AS SUCCESSOR-IN-INTEREST TO WACHOVIA BANK, N.A.), AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE, INC. (AS SUCCESSOR-BY-MERGER TO AEROJET-GENERAL CORPORATION)
Reel/Frame 064424/0087 →
RELEASE OF SECURITY INTEREST Recorded Aug 5, 2016
From: U.S. BANK NATIONAL ASSOCIATION
To: AEROJET ROCKETDYNE, INC. (F/K/A AEROJET-GENERAL CORPORATION)
Reel/Frame 039594/0887 →
NOTICE OF SUCCESSION OF AGENCY (INTELLECTUAL PROPERTY) Recorded Jun 20, 2016
From: WELLS FARGO BANK, NATIONAL ASSOCIATION, AS THE RESIGNING AGENT
To: BANK OF AMERICA, N.A., AS THE SUCCESSOR AGENT
Reel/Frame 039079/0857 →
MERGER/CHANGE OF NAME Recorded Jul 8, 2013
From: RPW ACQUISITION LLC
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 030754/0248 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 8, 2013
From: UNITED TECHNOLOGIES CORPORATION
To: RPW ACQUISITION LLC
Reel/Frame 030750/0283 →
SECURITY AGREEMENT Recorded Jun 21, 2013
From: AEROJET-GENERAL CORPORATION
To: U.S. BANK NATIONAL ASSOCIATION
Reel/Frame 030656/0667 →
SECURITY AGREEMENT Recorded Jun 17, 2013
From: AEROJET-GENERAL CORPORATION
To: WELLS FARGO BANK, NATIONAL ASSOCIATION
Reel/Frame 030628/0319 →
CONFIRMATORY LICENSE Recorded Sep 20, 2004
From: UNITED TECHNOLOGIES CORP
To: AIR FORCE, UNITED STATES
Reel/Frame 015799/0521 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 21, 2004
From: CUVA, WILLIAM J.
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 015284/0670 →