A water trough support apparatus for supporting a water trough on a flight of stairs, in particular. The water trough support apparatus includes an adjustable leg assembly; and also includes a platform support member being adjustably mounted upon the leg assembly; and further includes a platform bei
A water trough support apparatus for supporting a water trough on a flight of stairs, in particular. The water trough support apparatus includes an adjustable leg assembly; and also includes a platform support member being adjustably mounted upon the leg assembly; and further includes a platform being securely mounted upon the platform support member.
대표청구항▼
A water trough support apparatus for supporting a water trough on a flight of stairs, in particular. The water trough support apparatus includes an adjustable leg assembly; and also includes a platform support member being adjustably mounted upon the leg assembly; and further includes a platform bei
A water trough support apparatus for supporting a water trough on a flight of stairs, in particular. The water trough support apparatus includes an adjustable leg assembly; and also includes a platform support member being adjustably mounted upon the leg assembly; and further includes a platform being securely mounted upon the platform support member. in claim 8, wherein: a first portion of each of said plurality of solar panels remains disposed between said first and second structural members in said deployed position, while a second portion of each of said plurality of solar panels extends beyond said first and second structural members in said deployed position. 14. A satellite assembly, as claimed in claim 1, further comprising: means for biasing each of said plurality of solar panels toward said deployed position. 15. A satellite assembly, as claimed in claim 14, wherein: said means for biasing comprises a separate spring for each of said plurality of solar panels. 16. A satellite assembly, as claimed in claim 1, further comprising: a separate deployment spring for each of said plurality of solar panels. 17. A satellite assembly, as claimed in claim 1, further comprising: means for pivoting each of said plurality of solar panels from said stored position to said deployed position while maintaining each of said plurality of solar panels in parallel relation to each other throughout movement from said stored position to said deployed position. 18. A method for operating a satellite assembly comprising a first solar panel, a second solar panel, a third solar panel, and a fourth solar panel, said method comprising the steps of: maintaining said plurality of solar panels in a stored position; moving said plurality of solar panels from said stored position to a deployed position, wherein said moving step comprises pivoting said first and second solar panels about a first axis, in opposite directions, and in first and second reference planes, and pivoting said third and fourth solar panels about a second axis, in opposite directions, and in third and fourth reference planes, wherein said first and second reference planes are vertically offset and parallel to each other, and wherein said third and fourth reference planes are vertically offset and parallel to each other. 19. A satellite assembly, as claimed in claim 18, wherein: said maintaining step comprises disposing said plurality of solar panels in parallel relation. 20. A satellite assembly, as claimed in claim 18, wherein: said maintaining step comprises disposing said plurality of solar panels in stacked relation. 21. A satellite assembly, as claimed in claim 18, wherein: said maintaining step comprises disposing said plurality of solar panels in both a parallel and stacked relation. 22. A satellite assembly, as claimed in claim 18, wherein: said first and second axes are parallel to each other. 23. A satellite assembly, as claimed in claim 18, wherein: said first, second, third, and fourth reference planes are vertically offset and parallel to each other. 24. A satellite assembly, as claimed in claim 18, wherein: said first and second axes are parallel to each other, and wherein said first, second, third, and fourth reference planes are vertically offset and parallel to each other. 25. A satellite assembly, as claimed in claim 18, wherein: said moving step comprises pivoting said first, second, third, and fourth, solar panels along parallel paths throughout said moving step. 26. A satellite assembly, as claimed in claim 18, wherein: said first and second axes are 180 degrees apart. 27. A satellite assembly, as claimed in claim 18, further comprising: means for pivoting said first and second solar panels about said first connector in opposite directions from said stored position to said deployed position; and means for pivoting said third and fourth solar panels about said second connector in opposite directions from said stored position to said deployed position, wherein said first and second connectors are parallel to each other. 28. A method for operating a satellite assembly comprising a plurality of solar panels, said method comprising the steps of: disposing said plurality of solar panels in a store position, wherein said disposing ste
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이 특허에 인용된 특허 (14)
Chang Pek S. (Flat No. 509 ; Lai Kit Lau ; 38 ; Lai Tak Tsuen Tai Hang HKX), Adjustable-height support apparatus.
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