US4512069A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method of manufacturing hollow flow profiles
Assignee: MOTOREN-UND TURBINEN-UNION MUNCHEN A CORP OF WEST GERMANY GmbH
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Filing: 1983-02-04
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Granted: 1985-04-23
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Expires: 2003-02-04
Abstract
Abstract A method of manufacturing hollow flow profiles having optimum aerodynamic configurations in conformance with a commensurate application, about the respective outer skin of which there flows a first work medium during operation, such as hot gas, whereas ducts which are arranged within the interior of the flow profiles are concurrently streamed through by a second work medium, such as compressed air. The method of the present invention employs suitable deformation techniques (drawing, circular swaging or rolling) at preselected locations to particularly produce web-like aggregations of material. When appropriate materials are used for this purpose, contoured profiles of that type can also be formed through extruding. The webs, depending upon the demands of preceding or successive process steps, can be formed externally, internally or on both sides of the conduit material. The actual deformation for producing the flow profile can then be effected through drawing or rolling, possibly with several intermediate processing steps as required.
Inventors
- 👤 Klaus Hagemeister
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 22:04
CPC Classifications
B; B21; B21C; B21C37/00; B21C37/06; B21C37/15; B21C37/20; B21C37/151; B21K; B21K3/00; B21K3/04; B23; B23P; B23P15/00; B23P15/02; B23P15/26; F; F28; F28F; F28F1/00; F28F1/02; F28F1/022; Y; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/49316; Y10T29/49336; Y10T29/49339; Y10T29/49341
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
219 words
A method for manufacturing hollow heat exchanger matrix flow profiles of aerodynamic configurations, said profiles each having an outer skin streamed about during operation by a first working medium, and internal passages in the flow profiles simultaneously streamed through by a second working medium; comprising the steps of forming material accumulations at predetermined locations spaced over the circumference of a conduit of an initially predetermined sectional configuration; deforming said conduit so that one of the material accumulations produces a side thickening of the wall being formed proximate the area of the leading and trailing edges of the flow profile, and further deforming said conduit so that other material accumulations produce inner webs superimposed in the meridian plane ultimately to provide at least two separate compressed air passages, said forming step further including providing two diametrically opposite material accumulations on the circumference of the conduit of the same web-like configuration before the final forming of the profile and a projectile structure on the conduit wall; inserting turbulence-inducing metal means between the adjacent ends of the inner webs of the finish-formed flow profiles, and fastening said turbulence-inducing metal means together with the ends of the inner webs, as an internal structural component of the flow profile; effecting the final finish forming through pressing the inner webs together and welding them together.
Claim 2
Independent Claim
219 words
A method for manufacturing hollow heat exchanger matrix flow profiles of aerodynamic configurations, said profiles each having an outer skin streamed about during operation by a first working medium, and internal passages in the flow profiles simultaneously streamed through by a second working medium; comprising the steps of forming material accumulations at predetermined locations spaced over the circumference of a conduit of an initially predetermined sectional configuration; deforming said conduit so that one of the material accumulations produces a side thickening of the wall being formed proximate the area of the leading and trailing edges of the flow profile, and further deforming said conduit so that other material accumulations produce inner webs superimposed in the meridian plane ultimately to provide at least two separate compressed air passages, said forming step further including providing two diametrically opposite material accumulations on the circumference of the conduit of the same web-like configuration before the final forming of the profile and a projectile structure on the conduit wall; inserting turbulence-inducing metal means between the adjacent ends of the inner webs of the finish-formed flow profiles, and fastening said turbulence-inducing metal means together with the ends of the inner webs, as an internal structural component of the flow profile; effecting the final finish forming through pressing the inner webs together and welding them together.
Claim 3
Dependent Claim
22 words
Method as claimed in claim 1, comprising utilizing an internal tool for forming the final inner contour of the compressed air duct.
Claim 4
Dependent Claim
68 words
Method as claimed in claim 1, wherein prior to the intermediate webs of the flow profile being welded together, shaping at least one extreme portion of the profile into a circular or polygonal connecting member; and prior or subsequent to joining together along the remaining web ends, imparting at least said one connection piece with coaxially, helically extending or threaded grooves in the inner or outer wall thereof.
Claim 5
Dependent Claim
106 words
A method as claimed in claim 1, wherein said hollow profiled sections for the matrix of a heat exchanger are lancet-shaped; comprising fastening said hollow profiled sections to a first stationary conduit for directing compressed air into the matrix, and to a second stationary conduit in which the compressed air heated during its passage through the matrix is directed to a consumer, and connecting the two separate pipe conduits into a common manifold formed by mutually parallel individual conduits, whereby the heat exchanger matrix formed by the hollow profile sections projects laterally relative to the manifold or relative to the individual conduits in a U-shaped configuration.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1988-04-22 | 1988-10-22 | 1989-04-23 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1992-04-22 | 1992-10-22 | 1993-04-23 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1996-04-22 | 1996-10-22 | 1997-04-23 | $7700.00 | Window Closed / Lapsed |