Infrared radiation screening device

• US 4,876,851 A
• Filed: 03/24/1988
• Issued: 10/31/1989
• Est. Priority Date: 04/11/1987
• Status: Expired due to Fees

• Current Assignee: Messerschmitt-Boelkow-Blohm GmbH (Mercedes-Benz Group AG)
• Original Assignee: Messerschmitt-Boelkow-Blohm GmbH (Mercedes-Benz Group AG)
• Inventors: Mueller, Werner
• Primary Examiner(s): Casaregola, Louis J.
• Application Number:
  US07/173,193
• Time in Patent Office: 586 Days
• Field of Search: 60/39.5, 60/262, 60/264, 239/127.3, 239/265.17, 239/DIG. 19
• US Class Current: 60/264
• CPC Class Codes: F02K 1/825 Infrared radiation suppressors
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

An infrared radiation screening arrangement includes a special core structure and an outer gas guiding ring which together serve to block the direct view of a hot engine exhaust gas outlet and associated hot engine parts in order to hinder IR-detection of the engine. The gas guiding ring and the core structure define a cooling air guide channel with cooling air inlets for cooling the components of the arrangement and for cooling the exhaust gas stream which is ejected in an essentially unaltered direction.

Claims

1. An apparatus for shielding infrared emissions of an operating engine for hindering IR-detection, comprising an outer gas guiding ring (11), pivotable link means (10a) for adjustably attaching said gas guiding ring to an exhaust outlet (100) of said engine, a conical core structure (12) arranged essentially in a concentrical position within said gas guiding ring (11) for forming a cooling air channel (14, 14'"'"') with an ejector effect between said exhaust outlet and said gas guiding ring and between said gas guiding ring and said conical core structure, a cover plate (13) secured to a large downstream directed end of said conical core structure for covering said large downstream directed end of said conical core structure, said engine exhaust outlet forming with an upstream end of said outer gas guiding ring a ring inlet for feeding cooling air into said cooling air channel having said ejector effect, strut means (17) for supporting said conical core structure and said cover plate in said concentrical position within said gas guiding ring, said gas guiding ring, said conical core structure, said cover plate, and said strut means being made of a carbon-fiber-carbon composite material having a high temperature resistance to form an integral unit which is position adjustable.

2. The arrangement of claim 1, wherein said cover plate of said conical core structure has a given diameter forming a surface area (F1) which is equal to or slightly greater than a corresponding inner diameter of said engine exhaust outlet forming a further surface area (F3), whereby a direct view of hot exhaust outlet components of said engine is blocked.

3. The apparatus of claim 1, further comprising a thermally insulating gap between said large end of said conical core structure and said cover plate, said gap permitting a flow of cooling air through said core structure.

4. The apparatus of claim 1, further comprising a layer of thermally insulating material arranged on at least one side of said cover plate.

5. The apparatus of claim 3, further comprising a plurality of spacer struts (18) for attaching said cover plate to said conical core structure with a spacing between said large end of said conical core structure and said cover plate for forming said thermally insulating gap.

6. The apparatus of claim 5, wherein said core structure support struts (17) comprise cooling air ducts (21) therein, wherein said conical core structure has cooling air inlets connected to said coling air ducts (21), said spacer struts (18) providing cooling air outflow passages from said conical core structure (12) through said thermally insulating gap, whereby cooling air can cool said support struts (21), said conical core structure (12), said spacer struts (18), and said cover plate (13).