US2011017198A1PendingUtilityA1
Carrier system for a trackable solar energy plant and a kit
Est. expiryMay 10, 2027(~0.7 yrs left)· nominal 20-yr term from priority
Y02E10/47F24S 25/617F24S 2030/19F24S 2030/133H02S 20/10F24S 25/12H02S 20/32F24S 30/40Y02E10/50
45
PatentIndex Score
0
Cited by
0
References
0
Claims
Abstract
The invention relates to a carrier system for a trackable solar energy plant, in particular a ground supported solar energy system, comprising a support system and a solar module retainer, which is configured to receive a plurality of solar energy modules in a flat arrangement for the automatic tracking around a swivelling axis between settings, installed pivoting on the support system, where the solar energy module retainer is received at support points of the support system resting at the base on a respective three-point arrangement of bearings by means of allocated support elements.
Claims
exact text as granted — not AI-modified1 . A carrier system for a trackable solar energy plant, in particular a ground-supported solar energy plant, comprising a support system ( 1 ) and a solar energy module retainer ( 2 ), which is configured to receive a plurality of solar energy modules in a flat arrangement and is installed on the support system ( 1 ), for tracking automatically pivoting between settings around a swivelling axis, where the solar energy module ( 2 ) is taken in at support points ( 3 , 4 ) of the support system ( 1 ) resting at the base on a three-point arrangement of bearings by means of allocated support elements ( 30 a , 30 b , 30 c ; 31 a , 31 b , 31 c ), wherein one of the following versions has been shaped for the allocated support elements ( 30 a , 30 b , 30 c ; 31 a , 31 b , 31 c ): (i) the bases of the allocated support elements ( 30 a , 30 b , 30 c ; 31 a , 31 b , 31 c ) of the respective three-point arrangement of bearings run together in joint support areas ( 33 , 34 , 35 ), and (ii) at least one allocated support element ( 30 c ) of one of the separated supported points ( 3 ) runs to a different separated support unit ( 4 ) and rests on the three-point arrangement of bearings of the different support point ( 4 ).
2 . The carrier system in accordance with claim 1 , wherein the support points ( 3 , 4 ) enclose an upper and a lower support point that support the solar energy module retainer ( 2 ) in an upper and a lower section.
3 . The carrier system in accordance with claim 1 wherein the allocated support elements ( 30 a , 30 b , 30 c ; 31 a , 31 b , 31 c ) stretch continuously from the respective the three-point arrangement of bearings to the support points ( 3 , 4 ).
4 . The carrier system in accordance with claim 1 , wherein the allocated support elements ( 30 a , 30 b , 30 c ; 31 a , 31 b , 31 c ) are each executed as a one-piece profile element.
5 . The carrier system in accordance with claim 1 , wherein the swivelling axis is formed adjacent the back surface of the solar energy module retainer ( 2 ).
6 . The carrier system in accordance with claim 1 , wherein the base of the support system ( 1 ) rests on several ground anchors ( 36 , 37 , 38 ).
7 . The carrier system in accordance with claim 1 , further comprising an engine-driven traction cable system ( 5 , . . . , 12 ) that is configured to pivot the solar energy module retainer ( 2 ) around the swivelling axis between the end settings.
8 . The carrier system in accordance with claim 7 , wherein the engine-driven traction cable system ( 5 , . . . , 12 ) is formed optionally with a traction cable ( 6 ), executed continuously and with a retained length, is fixed in attachment areas distanced from each other ( 7 , 8 ) of the solar energy module retainer ( 2 ) respectively and runs coupled by friction through an engine-driven driving roller ( 11 ).
9 . The carrier system in accordance with claim 7 , wherein a drive engine ( 5 ) of the traction cable system ( 5 , . . . , 12 ) is arranged on the solar energy module retainer ( 2 ) in the essential centre in the line of sight from the front.
10 . The carrier system in accordance with claim 1 , wherein the solar energy module retainer ( 2 ) is executed as hinged.
11 . The carrier system in accordance with claim 1 , wherein carrying mounting elements ( 20 ) of the solar energy module retainer ( 2 ) are formed as mounting elements ( 20 ) forming a cable channel ( 25 ).
12 . The carrier system in accordance with claim 11 , wherein mounting elements forming the cable channel ( 25 ) are executed as closed cable channels in accordance with an installation of the solar energy modules in the solar energy module retainer ( 2 ) that are provided optionally with openings for taking cable through.
13 . The carrier system in accordance with claim 11 , wherein the mounting elements forming the cable channel ( 25 ) are formed by means of top hat profile elements.
14 . The carrier system in accordance with claim 1 , wherein the solar modules are secured in the solar energy module retainer ( 2 ) by means of not non-destructive detachable connections ( 21 ) optionally executed as a threaded joint.
15 . The carrier system in accordance with claim 1 , wherein by braking fittings ( 52 ) in the end settings configured to brake a movement of the solar energy module retainer ( 2 ) during pivoting, optionally by means of a friction brake, allocated respectively to the end settings.
16 . The carrier system in accordance with claim 17 , wherein the braking fittings ( 52 ) with friction braking are each formed with a guide section ( 53 ) that takes in an allocated inserted element ( 54 ) formed on the solar energy module retainer ( 2 ).
17 . The carrier system in accordance with claim 1 , further comprising means of stopping ( 55 ) that are configured to stop the solar energy module retainer ( 2 ) at the respective end settings.
18 . A kit for the installation of a carrier system for a trackable solar energy plant in accordance with claim 1 , with installable module elements for a support system ( 1 ) and a solar energy module retainer ( 2 ) that is configured to receive a plurality of solar energy modules in a flat arrangement and is installed pivoting on the support system ( 1 ) for automatic tracking between end settings on a swivelling axis, where the solar energy module retainer ( 2 ) is accepted by the support system ( 1 ) at separated support points ( 3 , 4 ) the bases of which rest on each three-point arrangement of bearings by means of allocated support elements ( 30 a , 30 b , 30 c ; 31 a , 31 b , 31 c ), wherein one of the following versions has been formed for the allocated support elements ( 30 a , 30 b , 30 c ; 31 a , 31 b , 31 c ): (i) The bases of the allocated support elements ( 30 a , 30 b , 30 c ; 31 a , 31 b , 31 c ) of the respective three-point arrangement of bearings run together in joint footing areas ( 33 , 34 , 35 ), and (ii) at least one of the allocated support elements ( 30 c ) of one of the separated support points ( 3 ) runs to a different separated support point ( 4 ) and rests on the three-point arrangement of bearings of the other support point ( 4 ).Join the waitlist — get patent alerts
Track US2011017198A1 — get alerts on status changes and closely related new filings.
We store only your email — no account needed. See our privacy policy.