FIELD: manufacture of heat control systems of communication, TV broadcasting and retransmission systems.
SUBSTANCE: proposed method includes manufacture of at least three similar thermal load simulators 2 at width of contact surface equal to width of web of heat-transfer agent collector. Heat transfer factors (K1,K2, K3) are determined at similar forces of pressing the contact plate of simulators 2 to skin surface of panel 1. Heat-transfer temperature at collector inlet is maintained equal to surrounding temperature. Said heat transfer factors are determined as follows: for simulator (K1) separately mounted on panel; for simulator (K2) mounted between two adjacent simulators in way of motion of heat-transfer agent; for simulator under conditions when other simulators (K3) are mounted opposite web of adjacent turns symmetrically relative to it. Quality of construction and technology of manufacture is judged from the following relationship: K2+K3-K1-ΔKj ≥ [K], where ΔKj is factor of influence of thermal resistance of joint between simulator contact surfaces and skin on heat-transfer factor; [K] is permissible magnitude of heat-transfer factor.
EFFECT: simplified procedure of check of honeycomb panel quality; low cost of manufacture of panels.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
COMMUNICATION, TV BROADCASTING AND REPEATER SATELLITE | 2003 |
|
RU2227108C1 |
SPACECRAFT TEMPERATURE CONTROL SYSTEM | 2002 |
|
RU2237600C2 |
SPACESHIP THERMAL SIMULATOR | 2011 |
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RU2481254C2 |
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RU2286290C1 |
SPACESHIP THERMAL MODULE | 2010 |
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RU2447003C1 |
METHOD OF CONSTRUCTING SPACECRAFT | 2013 |
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RU2542797C2 |
METHOD OF CONSTRUCTING SPACECRAFT | 2013 |
|
RU2541598C2 |
METHOD OF MANUFACTURING THREE-LAYERED PANEL | 2005 |
|
RU2287435C2 |
HONEYCOMB PANEL | 2007 |
|
RU2346860C2 |
SPACE VEHICLE LAYOUT DESIGN METHOD | 2007 |
|
RU2362713C2 |
Authors
Dates
2005-06-10—Published
2003-01-31—Filed