U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Lightweight reflective panels for solar-thermal power plants and methods of forming such panels

Patent 3959056 Issued on May 25, 1976. Estimated Expiration Date: Icon_subject May 25, 1993. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

1946184

2731379

2742387

2988809

3136674

3286270

3385726

3595216

3616140

3700522

Inventor

Application

No. 484662 filed on 07/01/1974

US Classes:

156/197, By separating laminae between spaced secured areas (e.g., honeycomb expanding)126/690, Parabolic126/696, Reflector support156/201, Prior to or during assembly with additional lamina156/214, With preshaping of lamina156/280, Subsequent to bonding156/324, Running or continuous webs of indefinite length156/495, By driven web feeding means29/469, Assembling a subassembly, then assembling with a second subassembly29/890.033, Solar energy device making428/116, Honeycomb-like493/379, Comprising bringing two members together493/966HONEYCOMB STRUCTURE

Examiners

Primary: Powell, William A.
Assistant: Gallagher, John J.

Attorney, Agent or Firm

Abstract

An inexpensive, lightweight reflective panel for solar-thermal collector modules of the type including a parabolic reflector for reflecting incident solar radiation onto a fluid carrying conduit positioned along the focal axis of the reflector. A rigid, waterproof, honeycomb panel formed from paper and having a uniform thickness of parabolic shape supports a reflective material. Glass fiber cloth adhered to the outer panel surfaces adds to the panel's strength and rigidity. An adjustable support system suspends the reflective panel from the fluid carrying conduit and provides a means of adjusting panel curvature to precisely obtain the required parabolic shape.Methods of forming the panels are described which permit the panels to be formed at or near the site of their installation to obviate shipping problems and expense. The methods include the steps of forming an expanded honeycomb core, conforming the core to the required parabolic shape, adhering sheets of skin material to top and bottom surfaces of the core, and adhering a reflective material to the top panel surface.

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