Passive infrared reduction device

Patent metadata

Field	Value
Publication number	US-11725609-B2
Application number	US-201916705623-A
Country	US
Kind code	B2
Filing date	Dec 6, 2019
Priority date	Dec 6, 2019
Publication date	Aug 15, 2023
Grant date	Aug 15, 2023

Abstract

A line of sight blocker including a cover defining a duct bounded by the cover and a heated surface when the cover is fastened over the heated surface. The cover blocks transmission of infrared radiation emitted from the heated surface; the cover comprises a material having a lower thermal conductivity than the heated surface; and the duct comprises a vent and a path for latent heat from the heated surface to escape through the vent.

First claim

What is claimed is:

1. A line of sight blocker, comprising:
a cover defining a duct bounded by the cover and a heated surface when the cover is fastened over the heated surface, wherein:
the duct comprises a first sidewall and a second sidewall,
the cover comprises the first sidewall and the second sidewall comprises the heated surface,
the duct comprises a width comprising a spacing between the first sidewall and the heated surface when the first sidewall is facing the heated surface, the cover blocks transmission of infrared radiation emitted from the heated surface,
the cover comprises a material having a lower thermal conductivity than the heated surface, and
the duct comprises a vent and a path for heat from the heated surface to escape through the vent.

2. The line of sight blocker of claim 1 , wherein the duct comprises air forming an insulation layer and the cover comprises one or more materials including plastic or carbon fiber.

3. The line of sight blocker of claim 1 , further comprising:
a part extending outward from the first sidewall, whereinthe part has a length defining the width of the duct.

4. The line of sight blocker of claim 3 , wherein the duct has the width (W) wherein ⅜ inch≤W≤1 inch.

5. The line of sight blocker of claim 3 , wherein the duct has the width allowing a flow of air into the duct through natural convection.

6. The line of sight blocker of claim 3 , wherein the cover includes the part comprising a top wall, a flange, a lip, a rim, or an arm.

7. The line of sight blocker of claim 6 , wherein the top wall includes a plurality of holes allowing flow of air out of the duct.

8. The line of sight blocker of claim 1 , wherein the cover is conformal with the heated surface.

9. The line of sight blocker of claim 1 , wherein the cover has a first circular cross-section or a cross-section including a segment of a circle, the heated surface has a second circular cross-section, and the cover is co-axial with the heated surface when the cover is fastened over the heated surface.

10. The line of sight blocker of claim 1 , wherein the cover is conformal with the heated surface and defines the duct when fastened to a device:
including an engine drain line having the heated surface,
a hydraulic line having the heated surface, or
a screen on a device vent having the heated surface.

11. The line of sight blocker of claim 1 , wherein the cover is conformal with the heated surface and defines the duct when fastened:
to an electronic circuit including the heated surface, or
a box housing the electronic circuit and the box includes the heated surface.

12. The line of sight blocker of claim 1 , wherein the cover defines the duct when fastened to a housing including bearings, the housing including the heated surface.

13. An apparatus, comprising:
a device including a heated surface emitting infrared radiation when the device is in operation;
a cover disposed over the heated surface; and
a gap between the cover and the heated surface, wherein the gap comprises a path for latent heat from the heated surface to escape from between the cover and the heated surface, wherein:
the cover is conformal with the heated surface and defines a duct when fastened to the device including an engine drain line having the heated surface, a hydraulic line having the heated surface, an electronic circuit including the heated surface, or a box housing the electronic circuit and the box includes the heated surface; or
the device comprises a first surface and a second surface, the second surface frictionally engaging the first surface during the operation so as to heat the first surface into the heated surface through friction, or
the apparatus comprises a de-rotation unit including the heated surface, an inner can, an outer can, and bearings between the inner can and the outer can.

14. The device of claim 13 , further comprising a fan coupled to the gap, the fan blowing air into the gap.

15. The device of claim 13 , wherein the cover is retrofittably disposed over the heated surface.

16. The device of claim 13 , wherein the cover is conformal with the heated surface and defines the duct when fastened to the device including:
the engine drain line having the heated surface,
the hydraulic line having the heated surface,
the electronic circuit including the heated surface, or
the box housing the electronic circuit and the box includes the heated surface.

17. The device of claim 13 , wherein the device comprises the first surface and the second surface, the second surface frictionally engaging the first surface during the operation so as to heat the first surface into the heated surface through the friction.

18. The device of claim 13 , further comprising the duct bounded by the cover and the heated surface, the duct having the gap at a first end of the cover and a second opening at a second end of the cover, wherein the path through the duct is perpendicular to a line of sight through the cover to the heated surface.

19. The device of claim 13 , wherein:
the apparatus comprises the de-rotation unit including the inner can, the outer can, and the bearings between the inner can and the outer can,
wherein:
the bearings rotate so as to decouple a rotation of the inner can from the outer can when the outer can is coupled to a stand pipe and the stand pipe is coupled to a fixed point, so that one or more components mounted on the outer can do not rotate with the inner can;
the de-rotation unit further includes seals sealing lubricant within a space between the inner can and the outer can; and
the de-rotation unit includes the heated surface emitting infrared radiation when the de-rotation unit is decoupling the rotation of the outer can from the rotation of the inner can with a drive shaft driving a plurality of rotors on a helicopter.

20. An apparatus comprising:
a shroud that removably and retrofittably couples to a mast, wherein the shroud is sized and shaped to draw air in a gap between the shroud and the mast, and
the gap forms an insulation layer and provides a path for latent heat from the mast to escape.

Assignees

• Boeing Co

Inventors

• King Carl
• Geiler Kal V

Classifications

• F02K1/825 Primary

  Infrared radiation suppressors · CPC title

• G01J5/06

  Arrangements for eliminating effects of disturbing radiation; Arrangements for compensating changes in sensitivity (for adjusting of solid angle of collected radiation G01J5/07; means for wavelength selection G01J5/0801) · CPC title

• G01J2005/065

  by shielding · CPC title

• F05D2220/329

  in helicopters · CPC title

• B64D2033/045

  comprising infrared suppressors · CPC title