[發明所欲解決之課題] [0009] 該等放熱元件之製造步驟中,放熱板、散熱板係以焊接、焊料之步驟加熱至200~700℃左右。管狀熱管、平面狀熱管係使用燒結、脫氣、磷銅焊料(BCuP-2等)予以焊接、擴散接合、熔接等之步驟加熱至800~1000℃左右。 例如使用純銅板作為熱管的原材料時,加熱至600℃以上溫度時之軟化劇烈。又急遽產生結晶粒的粗大化。因此,對熱片、半導體裝置之安裝或對PC框體之組裝等時,所製造之熱管易變形,熱管內部之構造產生變化或表面凹凸變大,而有無法發揮期望放熱性能之問題。又,為避免此等變形只要增厚純銅板厚度即可,但若如此則熱管的質量及厚度增大。厚度增大時,有使PC框體內部之間隙變小,對流傳熱性能降低之問題。 [0010] 又,專利文獻1、2中記載之銅合金板(Cu-Fe-P系合金)於600℃以上之溫度加熱時亦會軟化,進而與純銅相比導電率大為降低。因此,經過燒結、脫氣、焊接、擴散接合、熔接等步驟製造例如平面狀熱管時,容易於該熱管的運送及處理、對基板的組裝步驟等中變形。且因導電率降低,而有無法發揮作為熱管的期望性能。 [0011] 本發明之實施形態係鑑於在自純銅或銅合金板製造放熱元件之製程的一部分中包含加熱至600℃以上溫度之製程時的上述問題點者,目的在於提供可使經過加熱至600℃以上溫度之製程而製造之放熱元件具有充分強度與放熱性能之銅合金板。 [用以解決課題之手段] [0012] 析出硬化型銅合金藉由進行熔體化處理後、老化處理而提高強度及導電率。然而,析出硬化型銅合金於熔體化處理後,藉由施加冷塑性加工而將成為析出部位之塑性變形導入合金中之後,若進行老化處理,則有因老化處理使強度及導電率提高效果降低之情況。 經過焊接、擴散接合、熔接等之加熱步驟而製作之均熱板等之放熱元件時,於前述加熱步驟後並未施加塑性加工。因此,自析出硬化型銅合金之板材製作前述放熱元件時,即使於相當於熔體化處理之上述加熱步驟後實施老化處理,仍有強度及導電率未充分提高之情況。 另一方面,本發明人等發現於析出硬化型銅合金中之Cu-Co-P系合金中,藉由限定Co、P的組成範圍及Co/P比,於上述加熱步驟後,即使未施加塑性加工而進行老化處理時,亦可大為提高放熱元件之強度及導電率,因而完成本發明之實施形態。 [0013] 本發明實施形態之放熱元件用銅合金板係於包含加熱至600℃以上之製程與老化處理作為製造放熱元件之製程之一部分時使用,其係由Co:0.05~0.9質量%,P:0.01~0.25質量%,其餘部分由Cu及不可避免雜質所成,將Co含量(質量%)設為[Co],P含量(質量%)設為[P]時,[Co]/[P]為2~6,0.2%耐力為100MPa以上,伸長度為3%以上,具有優異之彎曲加工性。而且,該銅合金板於850℃加熱30分鐘後水冷,其次於500℃加熱2小時之老化處理後之0.2%耐力為150MPa以上,導電率為70%IACS以上。又,銅合金板之0.2%耐力為150MPa以上若換算為硬度係相當於Hv75以上。藉由拉伸試驗難以測定0.2%耐力時,藉由根據JISZ2244(2009)之規定測定維卡硬度,可推測0.2%耐力是否為150MPa以上。 [0014] 上述放熱元件用銅合金板可根據需要進而含有1.0質量%以下(不含0質量%)之Zn作為合金元素。且,本實施形態之放熱元件用銅合金板可根據需要進而以合計0.005~0.5質量%以下含有Fe、Ni、Si、Al、Mn、Cr、Sn、Ti、Zr、Ag、Mg中之1種或2種以上。上述銅合金板可進而與Zn同時含有Fe、Ni、Si、Al、Mn、Cr、Sn、Ti、Zr、Ag、Mg中之1種或2種以上。 [發明效果] [0015] 本發明實施形態之銅合金板係於包含加熱至600℃以上之製程與老化處理作為製造放熱元件之製程之一部分時使用。亦即,使用本發明實施形態之銅合金板製造之放熱元件高溫加熱至600℃以上後,不接受塑性加工進行老化處理,而提高強度。 本發明實施形態之銅合金板由於具有100MPa以上之高強度(0.2%耐力),故將銅合金板加工為放熱元件時之搬運及處理中不容易變形。且由於具有3%以上之伸長度及優異彎曲加工性,故可無阻礙地實行前述加工。 [0016] 本發明實施形態之銅合金板於850℃加熱30分鐘,其次進行老化處理時,0.2%耐力為150MPa以上,導電率為70%IACS以上。本發明實施形態之銅合金板由於老化處理後之強度高,故使用該銅合金板製造之熱管等之散熱元件安裝於熱片、半導體裝置、或組裝於PC框體等時,該放熱元件不易變形。且,本發明實施形態之銅合金板之導電率比純銅板低,但由於老化處理後之強度高故可薄片化,就放熱性能方面可彌補導電率之降低量。[Problems to be Solved by the Invention] [0009] In the manufacturing steps of the heat radiation element, the heat radiation plate and the heat dissipation plate are heated to about 200 to 700 ° C by soldering or soldering. The tubular heat pipe and the planar heat pipe are heated to about 800 to 1000 ° C by a step of welding, diffusion bonding, welding, etc. using sintering, degassing, phosphor bronze solder (BCuP-2, etc.). For example, when a pure copper plate is used as a raw material of the heat pipe, the softening is intense when heated to a temperature of 600 ° C or higher. The crystallization of the crystal grains is also rushed. Therefore, when the heat sheet, the semiconductor device is mounted, or the PC frame is assembled, the heat pipe to be manufactured is easily deformed, the structure inside the heat pipe is changed, or the surface unevenness is increased, and there is a problem that the desired heat radiation performance cannot be exhibited. Further, in order to avoid such deformation, it is only necessary to increase the thickness of the pure copper plate, but if so, the quality and thickness of the heat pipe are increased. When the thickness is increased, there is a problem in that the gap inside the PC casing is made small and the convective heat transfer performance is lowered. Further, the copper alloy sheets (Cu-Fe-P alloys) described in Patent Documents 1 and 2 are also softened when heated at a temperature of 600 ° C or higher, and further have a lower electrical conductivity than pure copper. Therefore, when a planar heat pipe is produced by a process such as sintering, degassing, welding, diffusion bonding, or welding, it is easy to be deformed during transportation and processing of the heat pipe, assembly steps of the substrate, and the like. Further, since the electrical conductivity is lowered, the desired performance as a heat pipe cannot be exhibited. [0011] Embodiments of the present invention are directed to the above problems when a process for heating a temperature of a temperature of 600 ° C or higher is included in a part of a process for manufacturing a heat releasing element from a pure copper or copper alloy plate, and the object is to provide heating to 600. A heat-dissipating element manufactured by a process of a temperature above °C has a copper alloy plate having sufficient strength and heat release properties. [Means for Solving the Problem] [0012] The precipitation hardening type copper alloy is improved in strength and electrical conductivity by performing a melt treatment and aging treatment. However, after the precipitation hardening type copper alloy is introduced into the alloy by applying cold plastic processing to the plastic deformation of the precipitation portion, the aging treatment causes the strength and electrical conductivity to be improved by the aging treatment. Reduce the situation. When a heat releasing element such as a heat equalizing plate is produced by a heating step such as welding, diffusion bonding, or welding, plastic processing is not applied after the heating step. Therefore, when the heat radiating element is produced from the plate material of the hardened copper alloy, the strength and the electrical conductivity are not sufficiently improved even if the aging treatment is performed after the heating step corresponding to the melt treatment. On the other hand, the present inventors have found that in the Cu-Co-P alloy in the precipitation hardening type copper alloy, by limiting the composition range of Co and P and the Co/P ratio, even after the heating step, even if not applied When the aging treatment is performed by plastic working, the strength and electrical conductivity of the heat radiating element can be greatly improved, and thus the embodiment of the present invention is completed. [0013] The copper alloy sheet for a heat radiation element according to the embodiment of the present invention is used when a process including heating to 600 ° C or higher and an aging treatment is used as a part of a process for manufacturing a heat release element, which is from 0.05 to 0.9% by mass, P. : 0.01 to 0.25 mass%, the remainder is made of Cu and unavoidable impurities, and the Co content (% by mass) is [Co], and the P content (% by mass) is [P], [Co]/[P It is 2 to 6, 0.2% withstand strength of 100 MPa or more, and elongation of 3% or more, and has excellent bending workability. Further, the copper alloy sheet was heated at 850 ° C for 30 minutes, then water-cooled, and secondly heated at 500 ° C for 2 hours, the 0.2% proof stress after the aging treatment was 150 MPa or more, and the electrical conductivity was 70% IACS or more. Further, the 0.2% proof stress of the copper alloy sheet is 150 MPa or more, and the hardness is equivalent to Hv75 or more. When it is difficult to measure 0.2% of the endurance by the tensile test, it is estimated that the 0.2% proof stress is 150 MPa or more by measuring the Vicat hardness according to the regulation of JIS Z2244 (2009). [0014] The copper alloy sheet for a heat releasing element may further contain 1.0% by mass or less (excluding 0% by mass) of Zn as an alloying element, if necessary. In addition, the copper alloy sheet for a heat radiating element of the present embodiment may contain one of Fe, Ni, Si, Al, Mn, Cr, Sn, Ti, Zr, Ag, and Mg in a total amount of 0.005 to 0.5% by mass or less, as needed. Or two or more. The copper alloy sheet may further contain one or more of Fe, Ni, Si, Al, Mn, Cr, Sn, Ti, Zr, Ag, and Mg together with Zn. [Effect of the Invention] The copper alloy sheet according to the embodiment of the present invention is used when a process including heating to 600 ° C or higher and an aging treatment are used as a part of a process for manufacturing a heat releasing element. In other words, the heat-dissipating element produced by using the copper alloy sheet according to the embodiment of the present invention is heated to 600 ° C or higher at a high temperature, and is subjected to aging treatment without plastic processing to improve strength. Since the copper alloy sheet according to the embodiment of the present invention has a high strength (0.2% proof) of 100 MPa or more, the copper alloy sheet is not easily deformed during handling and handling when it is processed into a heat releasing element. Further, since it has an elongation of 3% or more and excellent bending workability, the above processing can be carried out without hindrance. [0016] The copper alloy sheet according to the embodiment of the present invention is heated at 850 ° C for 30 minutes, and when subjected to the aging treatment, the 0.2% proof stress is 150 MPa or more, and the electric conductivity is 70% IACS or more. Since the copper alloy sheet according to the embodiment of the present invention has high strength after the aging treatment, the heat radiating element such as the heat pipe manufactured using the copper alloy sheet is attached to the hot sheet, the semiconductor device, or the PC frame, etc., and the heat radiating element is not easily used. Deformation. Further, the copper alloy sheet according to the embodiment of the present invention has a lower electrical conductivity than a pure copper plate, but can be flaky due to the high strength after the aging treatment, and the amount of decrease in electrical conductivity can be compensated for in terms of heat release performance.
[0017] 以下針對本發明實施形態之放熱元件用銅合金板更詳細說明。 本發明實施形態之銅合金板係藉由加壓成形、沖壓加工、切削、蝕刻等加工為特定形狀,經過高溫加熱(用以脫氣、接合(焊接,擴散接合、熔接)、燒結等之加熱),精加工為放熱元件。前述高溫加熱之加熱條件係根據放熱元件之種類及製造方法而異,但本發明之實施形態,假定為前述高溫加熱係以600℃~1050℃左右進行之情況。本發明實施形態之銅合金板由後述組成之Co-P系銅合金所成,於前述溫度範圍內加熱時,加熱前於母材析出之Co-P化合物之至少一部分固熔於母材,使結晶粒成長,產生軟化及導電率降低。 [0018] 本發明實施形態之銅合金板於850℃加熱30分鐘後水冷,其次老化處理後之強度(0.2%耐力)為150MPa以上,導電率為70%IACS以上。於850℃加熱30分鐘後係假定放熱元件之製造中的前述高溫加熱製程的加熱條件。本發明實施形態之銅合金板於該條件下高溫加熱時,加熱前於母材析出之Co-P化合物固熔於母材,使結晶粒成長,產生軟化及導電率降低。其次使前述銅合金板老化處理時,析出微細之Co-P化合物。藉此,藉由前述高溫加熱而顯著改善強度及導電率。 [0019] 前述老化處理可藉由例如如下等方法實施:(a)高溫加熱後之冷卻步驟中於析出溫度範圍保持一段時間,(b)高溫加熱後冷卻至室溫,隨後再加熱至析出溫度範圍並保持一段時間,(c)於前述(a)之步驟後,再加熱至析出溫度範圍並保持一段時間。 作為具體之老化處理條件,舉例為在300~580℃之溫度範圍保持5分鐘~10小時之條件。以強度提高為優先時,只要適當選擇生成微細Co-P化合物之溫度-時間條件即可,以導電率提高為優先時,只要適當選擇使固熔於母材之Co-P減少的過度老化處理溫度-時間條件即可。 [0020] 老化處理後之銅合金板雖與高溫加熱後之純銅板相比,導電率較低,但強度與純銅板相比顯著變高。為了獲得此效果,使用本發明實施形態之銅合金板製造之熱管等之放熱元件高溫加熱後經老化處理。老化處理條件係如前述。老化處理後之放熱元件(銅合金板)強度高,朝熱片、半導體裝置安裝或組裝於PC框體等時,可防止該放熱元件之變形。又,本發明實施形態之銅合金板(老化處理後),與純銅板相比強度較高,故可薄片化(0.1~1.0mm厚),藉此,放熱元件之放熱性能提高,可彌補與純銅板相比時之導電率降低量。 又,本發明實施形態之銅合金板即使高溫加熱之溫度未達850℃(600℃以上)或超過850℃(1050℃以下),於老化處理後,亦可達成150MPa以上之0.2%耐力及70%IACS以上之導電率。 [0021] 本發明實施形態之銅合金板於600℃以上之溫度高溫加熱前,藉由加壓成形、沖壓加工、切削、蝕刻等,而加工為放熱元件。銅合金板較好具有前述加工時之運送及處理中不容易變形的強度,可無障礙地實行前述加工之機械特性。更具體而言,本發明實施形態之銅合金板具有0.2%耐力為100MPa以上,伸長度為3%以上之優異彎曲加工性。若滿足以上特性,則銅合金板之調質無問題。例如熔體化處理材、老化處理結束、老化處理完成材進行冷壓延者等均可使用。伸長度較好為6%以上。 [0022] 針對前述彎曲加工性,要求於彎曲部不發生龜裂。再者,於曲線及其附近較好不發生表面粗糙。即使為相同材質之銅合金板,因彎曲所致之龜裂及表面粗糙之發生容易性依存於彎曲半徑R與板厚t的比率R/t。使用銅合金板製造均熱板等之放熱元件時,作為銅合金板之彎曲加工性通常要求彎曲線方向為壓延平行方向及直角方向同時進行R/t≦2之彎曲時不發生龜裂。作為銅合金板之彎曲加工性,較好於R/t≦1.5之彎曲時不發生龜裂,更好於R/t≦1.0之彎曲時不發生龜裂。銅合金板之彎曲加工性一般係對板寬10mm之試驗片進行試驗(參考後述實施例之彎曲加工性試驗)。使銅合金板材彎曲加工時,彎曲寬度越大越易發生龜裂,因此作為放熱元件彎曲寬度特別大時,較好於R/t=1.0之彎曲不發生龜裂,更好於R/t=0.5之彎曲不發生龜裂。又,為了不於彎曲線及其附近發生表面粗糙,針對銅合金板之表面的板寬方向測定之平均結晶粒徑(切斷法)較好為20μm以下,更好為15μm以下,又更好為10μm以下。 [0023] 如前述,加工本發明實施形態之銅合金板而製造之放熱元件於600℃以上之溫度高溫加熱時軟化。高溫加熱後之放熱元件較好進一步具有於實施老化處理時之運送及處理中不容易變形之強度。因此於850℃加熱30分鐘後水冷之階段,較好具有50MPa以上之0.2%耐力。 [0024] 使用本發明實施形態之銅合金板製造之放熱元件於接受老化處理後,基於提高耐腐蝕性及焊接性為主要目的,可根據需要至少於外表面之一部分形成Sn被覆層。Sn被覆層包含於電鍍、無電解鍍敷、或該等鍍敷後,加熱至Sn之熔點以下或熔點以上而形成者。Sn被覆層包含Sn金屬與Sn合金,作為Sn合金舉例為以合計5質量%以下含有Bi、Ag、Cu、Ni、In、Zn中之1種以上作為Sn以外之合金元素者。 [0025] 於Sn被覆層下,可形成Ni、Co、Fe等之基底鍍敷。該等基底鍍敷具有防止Cu及合金元素自母材擴散的障壁功能,及因放熱元件之表面硬度增大而具有防止損傷的功能。亦可於前述基底鍍敷上鍍敷Cu,進而鍍敷Sn後,進行加熱至Sn之熔點以下或熔點以上的熱處理而形成Cu-Sn合金層,而成為基底鍍敷、Cu-Sn合金層及Sn被覆層之3層構成。Cu-Sn合金層具有防止Cu及合金元素自母材擴散的障壁功能,及因放熱元件之表面硬度增大而具有防止損傷的功能。 [0026] 且,使用本發明實施形態之銅合金板製造之放熱元件於接受老化處理後,可根據需要至少於外表面之一部分形成Ni被覆層。Ni被覆層具有防止Cu及合金元素自母材擴散的障壁功能,因放熱元件之表面硬度增大而具有防止損傷的功能及提高耐腐蝕性之功能。 [0027] 其次針對本發明實施形態之銅合金板組成加以說明。 本發明實施形態之銅合金板組成係由Co:0.05~0.9質量%,P:0.01~0.25質量%,其餘部分由Cu及不可避免雜質所成,將Co含量(質量%)設為[Co],P含量(質量%)設為[P]時,[Co]/[P]為2~6。 Co係於與P之間生成P化合物(Co-P化合物),提高銅合金板之強度及耐應力緩和特性。該P化合物使固熔溫度提高,即使銅合金板加熱至600℃以上之高溫(例如850℃)亦一部分比較安定存在,而防止結晶粒徑之粗大化。另一方面,銅合金板之加熱溫度越高,水冷後之凍結空孔濃度越變高,析出物之核生成部位增加,故因持續進行之老化處理,可使析出物之數密度增加,此有助於老化處理後之強度提高。Co含量未達0.05質量%或P含量未達0.01質量%時,P化合物之析出量少,無法提高銅合金之強度及耐應力緩和特性。另一方面,Co含量超過0.9質量%或P含量超過0.25質量%時,老化處理後之銅合金中,無法達成70%IACS以上之導電率。且,生成粗大氧化物、晶析物、析出物等,而使熱加工性降低且銅合金板之強度、耐應力緩和特性及彎曲加工性降低。因此,Co設為0.05~0.9質量%,P含量設為0.01~0.25質量%。Co含量之下限值較好為0.10質量%,更好為0.15質量%,上限值較好為0.75質量%,更好為0.60質量%。P含量之下限值較好為0.02質量%,更好為0.03質量%,上限值較好為0.23質量%,更好為0.22質量%。 [0028] 為了上述作用,P含量有必要為上述範圍內,但另一方面,無助於析出的P含量,於可防止氫脆性之範圍較好儘可能少。基於此點,Co與P的含量比[Co]/[P]成為2~6之範圍內。[Co]/[P]未達2時,無助於Co-P化合物形成之固熔於母材的P量變多,[Co]/[P]超過6時,同樣固熔於母材之Co量變多,任一者均無法使老化處理後之銅合金板導電率為70%IACS以上。且,[Co]/[P]未達2或超過6時,無助於Co-P化合物形成之Co或P變多,無法充分提高銅合金板之老化處理後之強度。[Co]/[P]之下限值較好為2.2,更好為2.5,又更好為3.0,[Co]/[P]之上限值較好為5.0,更好為4.5。 [0029] 上述銅合金亦可根據需要進而含有Zn:1.0質量%以下(不包含0質量%)或/及以合計0.005~0.5質量%含有Fe、Ni、Sn、Si、Al、Mn、Cr、Ti、Zr、Ag、Mg中之1種或2種以上。但,藉由添加該等元素,必須避免使老化處理後之銅合金板導電率低於70%IACS。 Zn具有改善銅合金板之焊料的耐熱剝離性及Sn鍍敷之耐熱剝離性的作用。放熱元件組裝於半導體裝置時,有需要焊接之情況,且製造放熱元件後,有為了改善耐腐蝕性而進行Sn鍍敷之情況。製造此等放熱元件時,較好使用含有Zn之銅合金板。然而,Zn含量超過1.0質量%時,為了降低焊料濡濕性,而含有Zn時,Zn含量設為1.0質量%以下(不包含0質量%)。Zn含量較好為0.7質量%以下,更好為0.5質量%以下。另一方面,Zn含量未達0.01質量%時,對於耐熱剝離性之改善助益較小,Zn含量較好為0.01質量%以上。Zn含量更好為0.05質量%以上,進而較好為0.1質量%以上。 又,本發明實施形態之銅合金板包含Zn時,於500℃以上之溫度加熱時,則有因加熱環境使Zn氣化,使銅合金板之表面性狀降低,汙染加熱爐之情況。基於防止Zn氣化之觀點,Zn含量較好為0.5質量%以下,更好為0.4質量%以下,又更好為0.3質量%以下,再更好為0.2質量%以下。 [0030] 由於Fe、Ni、Sn、Si、Al、Mn、Cr、Ti、Zr、Ag、Mg具有提高銅合金之強度及耐熱性之作用,故根據需要添加該等元素中之1種或2種以上。然而,該等元素之含量多時,銅合金板之導電率降低,故添加該等元素中之1種或2種以上時,其合計含量設為0.005~0.5質量%之範圍。 上述元素中Fe、Ni與Co同樣,與P之間形成磷化合物((Ni, Fe)-P化合物)。因磷化物之形成而提高銅合金板強度之效果係Co最大,其次依序為Fe、Ni。Fe、Ni具有與未與Co形成磷化物之P形成磷化物(固熔於母材的P減少),而提高銅合金板強度之效果。且Fe具有抑制高溫加熱時之結晶粒粗大化之效果。為了獲得該等效果,Fe含量較好為0.01質量%以上,Ni含量較好為0.02質量%以上。另一方面,為了抑制導電率降低,Fe含量較好為0.05質量%以下,Ni含量較好為0.1質量%以下。 [0031] Sn、Mg具有固熔於銅合金母相,提高銅合金板的強度及耐應力緩和特性之效果。放熱元件之溫度或使用環境為80℃或其以上時,產生蠕變變形,與CPU等熱源的接觸面積變小,使放熱性降低,但藉由提高耐應力緩和特性,可抑制該現象。為了獲得該效果,Sn含量較好為0.02質量%以上,Mg含量較好為0.01質量%以上。另一方面,基於防止銅合金板之導電率降低之觀點,Sn含量較好為0.2質量%以下,Mg含量較好為0.2質量%以下。 Si、Al、Mn具有提高銅合金之強度及耐熱性之效果。為了獲得該效果,Si、Al、Mn之含量較好均為0.01質量%以上。另一方面,基於防止銅合金板之導電率降低之觀點,Si含量較好為0.2質量%以下,Al含量較好為0.2質量%以下,Mn含量較好為0.1質量%以下。 [0032] Cr、Ti、Zr具有提高銅合金之強度及耐熱性,抑制高溫加熱時之結晶粒粗大化之效果。為了獲得該效果,Cr含量與Ti含量較好均為0.01質量%以上,Zr含量較好為0.005質量%以上。另一方面,基於防止銅合金板之導電率降低之觀點,Cr含量較好為0.2質量%以下,Ti含量較好為0.1質量%以下,Zr含量較好為0.05質量%以下。又,該等元素容易形成數μm~數10μm左右之氧化物系、硫化物系等之介隔物,於表面存在前述介隔物時,銅合金板之耐腐蝕性降低,但該等元素含量為上述範圍時,不會產生特別問題。 Ag有提高銅合金之強度及耐熱性的效果。Ag含量較好為0.005~ 0.02質量%之範圍。 [0033] 不可避免雜質的H、O、S、Pb、Bi、Sb、Se、As於銅合金板長時間加熱至600℃以上之溫度時聚集於粒界,有於加熱中及加熱後引起粒界龜裂及粒界脆化之可能性,故較好減低該等元素含量。H由於於加熱中聚集於粒界、介隔物與母材之界面,而產生膨脹,故較好設為未達1.5ppm(質量ppm,以下同),更好未達1ppm。O較好設為未達20ppm,更好未達15ppm。S、Pb、Bi、Sb、Se、As較好合計設為未達30ppm,更好未達20ppm。尤其關於Bi、Sb、Se、As,較好該等元素之合計含量未達10ppm,更好未達5ppm。 [0034] 本發明實施形態之銅合金板可使鑄塊均熱處理後,藉由(1)熱壓延-冷壓延-燒鈍,(2)熱壓延-冷壓延-燒鈍-冷壓延,(3)熱壓延-冷壓延-燒鈍-冷壓延-低溫燒鈍等之步驟製造。上述(1)~(3)中,冷壓延-燒鈍之步驟可進行複數次。 前述燒鈍包含軟化燒鈍、再結晶燒鈍或析出燒鈍(老化處理)。軟化燒鈍或再結晶燒鈍時,加熱溫度可自600~950℃之範圍選擇,加熱時間可自5秒~1小時之範圍選擇。軟化燒鈍或再結晶燒鈍兼具熔體化處理時,宜在600~950℃,較好670~900℃保持3分鐘以下進行連續燒鈍。老化處理時,宜以350~580℃左右之溫度範圍保持0.5~10小時之條件進行。軟化燒鈍或再結晶燒鈍於兼具熔體化處理時,於後步驟可進行該老化處理。 [0035] 最終冷壓延宜配合目標的0.2%耐力與彎曲加工性,自加工率5~80%之範圍選擇。 低溫燒鈍係為了恢復銅合金板之延展性而不使銅合金板再結晶而軟化者,故宜根據連續燒鈍之情況而決定為在300~650℃之環境下保持1秒~5分鐘左右。又,批式燒鈍之情況宜決定為使銅合金板之實體溫度為250℃~400℃保持5分鐘~1小時左右。 藉由以上製造方法,可製造0.2%耐力為100MPa以上,伸長度為3%以上之具有優異彎曲加工性之銅合金板。又,該銅合金板於850℃加熱30分鐘,其次於500℃加熱2小時之老化處理時,具有150MPa以上之0.2%耐力,70%IACS以上之導電率。 又,可於600℃以上之溫度藉由擴散接合、焊接等之方法良好接合(無接合不良,接合強度高等)之銅合金板(製品)的表面粗糙度,以算術平均粗糙度Ra計為0.3μm以下,以最大高度粗糙度Rz計為1.5μm以下,內部氧化深度為0.5μm以下,期望為0.3μm以下。 欲使銅合金板(製品)之表面粗糙度為Ra:0.3μm,Rz:1.5μm以下時,最終冷壓延所用之壓延輥之輥軸方向的表面粗糙度為例如Ra:0.15μm,Rz:1.0μm以下,或對最終冷壓延後之銅合金板進行拋光研磨、電解研磨等之研磨即可。又,欲使銅合金板(製品)之內部氧化深度為0.5μm以下時,藉由使燒鈍環境設為還原性且露點設為-5℃以下,或對燒鈍後之銅合金板進行機械研磨(拋光,刷子等)或電解研磨,而去除生成之內部氧化層或減薄即可。 [0036] 本發明實施形態之銅合金板,作為標準的製造方法,係使鑄塊均熱處理,進行熱壓延後,伴隨冷壓延、熔體化而進行再結晶處理、冷壓延(可省略)、老化處理之步驟而製造。伴隨熔體化之再結晶處理後之冷壓延可省略。又,前述老化處理後,亦可進而進行冷壓延。使用前述組成之銅合金,藉由該製造方法製造之銅合金板具有高強度(0.2%耐力為300MPa以上),伸長度為3%以上,具有優異之彎曲加工性。又,該銅合金板於850℃加熱30分鐘,其次於500℃加熱2小時之老化處理時,具有150MPa以上之0.2%耐力,70%IACS以上之導電率。 [0037] 熔解、鑄造可藉由連續鑄造、半連續鑄造等之通常方法進行。又,作為銅熔解原料,較好使用S、Pb、Bi、Se、As含量較少者。又,注意經銅合金熔液被覆之木炭之紅熱化(水分去除)、裸金屬、廢棄原料、鑄造導水管、鑄模之乾燥及熔液之脫氧等,較好減低O、H。 [0038] 均質化處理較好於鑄塊內部到達500℃以上之溫度後,保持30分鐘以上。均質化處理之保持時間更好為1小時以上,更好為2小時以上。 均質化處理後,於800℃以上之溫度開始熱壓延。較好以於熱壓延材中不形成粗大Co-P析出物之方式,使熱壓延於600℃以上之溫度結束,自該溫度藉由水冷等之方法急冷。熱壓延後之急冷開始溫度若低於600℃,則易形成粗大Co-P析出物,使組織變不均一,使銅合金板(製品板)之強度降低。熱壓延之結束溫度較好為600℃以上之溫度,更好為700℃以上之溫度。又,經熱壓延後急冷之熱壓延材的組織成為再結晶組織。伴隨後述之熔體化之再結晶處理可兼進行熱壓延後之急冷。 [0039] 藉由熱壓延後之冷壓延,對銅合金板施加一定應力,繼續在再結晶處理後,獲得具有期望再結晶組織(微細之再結晶組織)之銅合金板。 伴隨熔體化之再結晶處理係以600~950℃,較好670~900℃保持3分鐘以下之條件進行。於銅合金中之Co、P含量較少時,較好於比上述溫度範圍內更低溫區域進行,於Co、P含量較多時,較好於比上述溫度範圍內更高溫區域進行。藉由該再結晶處理,Co、P固熔於銅合金母材,並且可形成彎曲加工性良好之再結晶組織(結晶粒徑為1~20μm)。該再結晶處理溫度低於600℃時,Co、P對母材之固熔量變少,老化處理後之強度降低。另一方面,再結晶處理之溫度超過950℃或處理時間超過3分鐘時,再結晶粒粗大化。 [0040] 伴隨熔體化之再結晶處理後,進行(a)老化處理,(b)冷壓延及老化處理,(c)冷壓延及老化處理後,進而冷壓延至製品厚度,或(d)於前述(c)之後進行低溫燒鈍(延展性回復)。 老化處理係如前述記載,於加熱溫度300~580℃左右保持0.5~10小時之條件進行。該加熱溫度未達300℃時析出量少,超過580℃時析出物易變粗大化。加熱溫度之下限較好為350℃,上限較好為570℃,更好為560℃。老化時間之保持時間係根據加熱溫度適當選擇,而於0.5~10小時之範圍內進行。該保持時間未達0.5小時時,析出變不充分,即使超過10小時析出量已飽和,而使生產性降低。保持時間之下限較好為1小時,更好為2小時。 [實施例1] [0041] 鑄造表1、2所示組成之銅合金,分別製作厚度45mm之鑄塊。該銅合金中,不可避免雜質的H未達1ppm,O未達15ppm,S、Pb、Bi、Sb、Se、As之合計未達20ppm。 對於各鑄塊於965℃進行3小時之均熱處理,接著進行熱壓延作成板厚15mm之熱壓延材,自650℃以上之溫度淬火(水冷)。淬火後之熱壓延材的兩面各研磨掉1mm後,進行冷粗壓延直至目標板厚0.6mm,於800℃保持20秒進行再結晶處理(伴隨熔體化)。其次於500℃進行2小時之析出燒鈍後,施以50%之精加工冷壓延,作成板厚0.3mm,進而於330℃進行20秒之低溫燒鈍(應力消除燒鈍),製造銅合金板。又,對板厚0.3mm之各銅合金板(僅比較例No.2熱壓延龜裂材)分析之組成亦為與表1、2之值相同。且,關於各銅合金板(比較例No.2除外),其表面粗糙度係Ra:0.08~0.15μm,Rz:0.8~1.2μm,研磨板厚剖面並以掃描電子顯微鏡(觀察倍率15000倍)測定之內部氧化深度為0.1μm以下。 [0042][0043][0044] 將所得銅合金板作為供試材,以下述要領,進行導電率、機械特性、彎曲加工性、焊料濡濕性之各測定試驗。其結果示於表3、4。 又,所得銅合金板係於850℃加熱30分鐘後水冷者,進而於500℃加熱2小時(老化析出處理)者分別作為供試材,進行導電率及機械特性之各測定試驗。其結果示於表3、4。 [0045] (導電率之測定) 導電率之測定係依據JIS-H0505規定之非鐵金屬材料導電率測定法,以使用雙橋接之四端子法進行。 (機械特性) 自供試材以使長度方向成為壓延平行方向之方式切出JIS5號拉伸試驗片,依據JIS-Z2241實施拉伸試驗,測定耐力及伸長度。耐力係相當於永久伸長度0.2%之拉伸強度。 [0046] (彎曲加工性) 彎曲加工性之測定係依據伸銅協會標準JBMA-T307規定之W彎曲試驗方法實施。自各供試材切出寬10mm、長30mm之試驗片,使用R/t=1.0之治具,進行G.W.(Good Way(彎曲軸與壓延方向垂直))及B.W.(Bad Way(彎曲軸與壓延方向平行))之彎曲。其次,藉由100倍之光學顯微鏡目視觀察彎曲部有無龜裂,G.W.及B.W.兩者均未發生龜裂者評價為P(P:Pass,合格),G.W.及B.W.之一者或兩者發生龜裂者評價為F(F:Fall,不合格)。 [0047] (焊料濡濕性) 自各供試材以長度方向與壓延方向平行之方式,採取寬10mm、長35mm之短條狀試驗片,於非活性助焊劑(日本αMetallized股份有限公司製α100)中浸漬塗佈1秒後,以弧面狀沾錫試驗法(meniscograph method)測定焊料濡濕時間(依據JISC0053焊接試驗方法(平衡法),RHESCA股份有限公司製SAT5100)。焊料使用於260±5℃保持之Sn-3質量%Ag-0.5質量%Cu,浸漬速度為25mm/sec,浸漬深度5mm,浸漬時間5秒之試驗條件進行。焊料濡濕時間為2秒以下者評價為焊料濡濕性優異。又,比較例5以外,焊料濡濕時間為2秒以下。 [0048][0049][0050] 表1、3中所示之實施例1~18之銅合金板係合金組成滿足本發明實施形態之規定,於850℃加熱30分鐘,其次於500℃加熱2小時之老化處理後之強度(0.2%耐力)為150MPa以上,且導電率為70%IACS以上。又,於850℃加熱前之銅合金板的特性係強度(0.2%耐力)為100MPa以上,伸長度為3%以上,彎曲加工性及焊料濡濕性均優異。於850℃加熱後,大多亦具有50MPa以上之強度(0.2%耐力)。又,實施例6(Co、P之含量接近下限值)之老化處理後之耐力值為162MPa,硬度為Hv83(於試驗力0.49N測定)。 [0051] 相對於此,表2、4所示之比較例1~8之銅合金板如以下所示,某特性差。 比較例1由於Co含量過量,故彎曲加工性差,老化處理後之強度及導電率低。 比較例1由於P含量過量,故熱壓延時發生龜裂,無法進行至熱壓延後之步驟。 比較例3係[Co]/[P]高,老化處理後之強度及導電率低。 比較例4係[Co]/[P]低,老化處理後之強度及導電率低。 比較例5係Zn含量過量,如前述焊料濡濕性差。 比較例6由於主要元素以外之元素(Al、Mn等)之合計過量,故老化處理後之導電率低。 比較例7由於P含量不足,故老化處理後之強度及導電率低。 比較例8由於Co含量不足,故老化處理後之強度低。 [實施例2] [0052] 針對表1、2所示之銅合金板中代表者(實施例2、10、比較例3、4),於1000℃加熱30分鐘後予以水冷,進而於500℃加熱2小時(老化處理),將該銅合金板作為供試材,以實施例1記載之方法進行導電率及機械特性之各測定試驗。其結果示於表5。 [0053][0054] 如表5所示,實施例2、10於1000℃加熱30分鐘,接著老化處理後之強度(0.2%耐力)為150MPa以上,且導電率為70%IACS以上。表5所示之各個數值與在850℃加熱30分鐘,其次老化處理後之測定結果(參考表)比較,則數值並無太大差異。 另一方面,比較例3、4於1000℃加熱30分鐘,接著老化處理後之強度及導電率未達到基準(0.2%耐力為150MPa以上,導電率為70%IACS以上)。 [0055] 本說明書之揭示內容包含以下態樣。 態樣1: 一種放熱元件用銅合金板,其特徵係由Co:0.05~0.9質量%,P:0.01~0.25質量%,其餘部分由Cu及不可避免雜質所成,將Co含量設為[Co],P含量設為[P]時,[Co]/[P]為2~6,0.2%耐力為100MPa以上,伸長度為3%以上,具有優異之彎曲加工性,於850℃加熱30分鐘後水冷,其次於500℃加熱2小時之老化處理後之0.2%耐力為150MPa以上,導電率為70%IACS以上,於製造放熱元件之製程之一部分係包含加熱至600℃以上之製程與老化處理。 態樣2: 如態樣1之放熱元件用銅合金板,其中進而含有1.0質量%以下(不含0質量%)之Zn。 態樣3: 如請求項1或2之放熱元件用銅合金板,其中進而以合計0.005~ 0.5質量%含有Fe、Ni、Sn、Si、Al、Mn、Cr、Ti、Zr、Ag、Mg中之1種或2種以上。 態樣4: 一種放熱元件之製造方法,其特徵係將如態樣1~3中任一項之放熱元件用銅合金板加工成特定形狀後,施以加熱至600℃以上之製程,接著不施加塑性加工而進行老化處理,獲得具有150MPa以上之0.2%耐力及70%IACS以上之導電率之放熱元件。 態樣5: 如態樣4之放熱元件之製造方法,其中於老化處理後,於放熱元件之外表面至少一部分形成Sn被覆層。 態樣6: 如態樣4之放熱元件之製造方法,其中於老化處理後,於放熱元件之外表面至少一部分形成Ni被覆層。 [0056] 本申請案係以申請日為2016年9月26日之日本國專利申請案特願第2016-190664號為申請基礎伴隨主張優先權。特願第2016-190664號藉由參考併入本說明書中。[0017] Hereinafter, a copper alloy sheet for a heat radiation element according to an embodiment of the present invention will be described in more detail. The copper alloy sheet according to the embodiment of the present invention is processed into a specific shape by press molding, press working, cutting, etching, or the like, and is heated by high temperature (for degassing, joining (welding, diffusion bonding, welding), sintering, etc.). ), finishing into an exothermic component. The heating conditions of the high-temperature heating vary depending on the type of the heat-releasing element and the manufacturing method. However, in the embodiment of the present invention, the high-temperature heating system is assumed to be performed at about 600 ° C to 1050 ° C. The copper alloy sheet according to the embodiment of the present invention is formed of a Co—P-based copper alloy having a composition described later, and when heated in the above temperature range, at least a part of the Co—P compound deposited on the base material before heating is solid-melted to the base material. The crystal grains grow, resulting in softening and a decrease in electrical conductivity. [0018] The copper alloy sheet according to the embodiment of the present invention is heated at 850 ° C for 30 minutes, then water-cooled, and the strength (0.2% proof) after the aging treatment is 150 MPa or more, and the electrical conductivity is 70% IACS or more. Heating at 850 ° C for 30 minutes is assumed to be the heating condition of the aforementioned high-temperature heating process in the manufacture of the heat releasing element. When the copper alloy sheet according to the embodiment of the present invention is heated at a high temperature under these conditions, the Co-P compound deposited on the base material before heating is solid-melted to the base material to grow the crystal grains to cause softening and a decrease in electrical conductivity. Next, when the copper alloy sheet is aged, a fine Co-P compound is precipitated. Thereby, the strength and electrical conductivity are remarkably improved by the aforementioned high temperature heating. [0019] The foregoing aging treatment can be carried out by, for example, the following methods: (a) maintaining a temperature range for a period of time in a cooling step after heating at a high temperature, (b) cooling to room temperature after heating at a high temperature, and then heating to a precipitation temperature. The range is maintained for a period of time, and (c) is heated to the precipitation temperature range for a period of time after the step (a). As specific aging treatment conditions, for example, the conditions are maintained in the temperature range of 300 to 580 ° C for 5 minutes to 10 hours. When the strength is increased as a priority, the temperature-time condition for forming the fine Co-P compound may be appropriately selected, and when the conductivity is increased, the excessive aging treatment for reducing the Co-P of the solid solution to the base material is appropriately selected. Temperature-time conditions are sufficient. [0020] Although the copper alloy sheet after the aging treatment has a lower electrical conductivity than the pure copper plate after the high temperature heating, the strength is remarkably higher than that of the pure copper plate. In order to obtain this effect, the heat radiation element such as the heat pipe manufactured by using the copper alloy sheet according to the embodiment of the present invention is heated at a high temperature and then subjected to aging treatment. The aging treatment conditions are as described above. The heat radiation element (copper alloy plate) after the aging treatment has high strength, and deformation of the heat radiation element can be prevented when it is mounted on a heat sheet or a semiconductor device or assembled in a PC frame or the like. Further, since the copper alloy sheet according to the embodiment of the present invention (after the aging treatment) has higher strength than the pure copper sheet, it can be thinned (0.1 to 1.0 mm thick), whereby the heat radiation performance of the heat radiating element is improved, and it is possible to make up for The conductivity is reduced when compared to a pure copper plate. Moreover, even if the temperature of the copper alloy sheet according to the embodiment of the present invention is not higher than 850 ° C (600 ° C or higher) or more than 850 ° C (1050 ° C or lower), after the aging treatment, 0.2% of the endurance of 150 MPa or more and 70 can be achieved. Conductivity above % IACS. [0021] The copper alloy sheet according to the embodiment of the present invention is processed into a heat radiation element by press molding, press working, cutting, etching, or the like before heating at a temperature of 600 ° C or higher. The copper alloy sheet preferably has the strength that is not easily deformed during transportation and handling during the above-described processing, and the mechanical properties of the above processing can be performed without any trouble. More specifically, the copper alloy sheet according to the embodiment of the present invention has an excellent bending workability of 0.2% withstand strength of 100 MPa or more and elongation of 3% or more. If the above characteristics are satisfied, the conditioning of the copper alloy sheet is not problematic. For example, the melt-treated material, the aging treatment, and the aging-treated material can be used for cold rolling. The elongation is preferably 6% or more. [0022] In view of the aforementioned bending workability, it is required that cracks do not occur in the bent portion. Furthermore, surface roughness does not preferably occur in the vicinity of the curve. Even in the case of a copper alloy plate of the same material, the occurrence of cracks and surface roughness due to bending depends on the ratio R/t of the bending radius R to the thickness t. When a copper alloy sheet is used to produce a heat radiating element such as a heat equalizing plate, the bending workability of the copper alloy sheet usually requires no cracking when the bending direction is the parallel direction of the rolling direction and the direction perpendicular to the direction of R/t ≦2. As the bending workability of the copper alloy sheet, it is preferable that cracking does not occur at the time of bending of R/t≦1.5, and it is more preferable that cracking does not occur when bending of R/t≦1.0. The bending workability of the copper alloy sheet is generally tested on a test piece having a plate width of 10 mm (refer to the bending workability test of the example described later). When the copper alloy sheet is bent, the larger the bending width, the more likely the crack occurs. Therefore, when the bending width of the heat releasing element is particularly large, it is preferable that the bending of R/t=1.0 does not occur, and it is better that R/t=0.5. The bending does not occur. Further, in order not to cause surface roughness in the vicinity of the bending line and the vicinity thereof, the average crystal grain size (cutting method) for measuring the width direction of the surface of the copper alloy sheet is preferably 20 μm or less, more preferably 15 μm or less, and more preferably It is 10 μm or less. [0023] As described above, the heat radiation element produced by processing the copper alloy sheet according to the embodiment of the present invention is softened when heated at a high temperature of 600 ° C or higher. The heat-dissipating element after the high-temperature heating preferably further has a strength which is not easily deformed during transportation and handling during the aging treatment. Therefore, the stage of water cooling after heating at 850 ° C for 30 minutes preferably has a resistance of 0.2% or more of 50 MPa or more. [0024] After the heat-treating element manufactured using the copper alloy sheet according to the embodiment of the present invention is subjected to the aging treatment, the Sn coating layer may be formed at least on one of the outer surfaces as needed for the purpose of improving corrosion resistance and weldability. The Sn coating layer is formed by electroplating, electroless plating, or the like, and is heated to a temperature equal to or lower than the melting point of Sn or a melting point or higher. The Sn coating layer contains a Sn metal and a Sn alloy, and the Sn alloy contains, for example, 5% by mass or less, and at least one of Bi, Ag, Cu, Ni, In, and Zn is used as an alloying element other than Sn. [0025] Under the Sn coating layer, a base plating of Ni, Co, Fe, or the like can be formed. These base plating functions as a barrier function for preventing diffusion of Cu and alloying elements from the base material, and have a function of preventing damage due to an increase in surface hardness of the heat radiation element. Cu may be plated on the base plating, and after plating with Sn, heat treatment to a temperature below the melting point of Sn or a melting point or higher may be performed to form a Cu-Sn alloy layer, thereby forming a base plating, a Cu-Sn alloy layer, and The Sn coating layer is composed of three layers. The Cu-Sn alloy layer has a barrier function of preventing diffusion of Cu and alloy elements from the base material, and has a function of preventing damage due to an increase in surface hardness of the heat radiation element. Further, after the heat radiation element manufactured using the copper alloy sheet according to the embodiment of the present invention is subjected to the aging treatment, the Ni coating layer may be formed at least in part of the outer surface as needed. The Ni coating layer has a barrier function of preventing diffusion of Cu and alloying elements from the base material, and has a function of preventing damage and an effect of improving corrosion resistance due to an increase in surface hardness of the heat releasing element. [0027] Next, the composition of the copper alloy sheet according to the embodiment of the present invention will be described. The composition of the copper alloy sheet according to the embodiment of the present invention is from 0.05 to 0.9% by mass, P: 0.01 to 0.25 mass%, and the remainder is formed of Cu and unavoidable impurities, and the Co content (% by mass) is set to [Co]. When the P content (% by mass) is set to [P], [Co]/[P] is 2 to 6. Co is formed between P and P to form a P compound (Co-P compound), which improves the strength and stress relaxation resistance of the copper alloy sheet. The P compound increases the solid solution temperature, and even if the copper alloy sheet is heated to a high temperature of 600 ° C or higher (for example, 850 ° C), it is somewhat stable, and coarsening of the crystal grain size is prevented. On the other hand, the higher the heating temperature of the copper alloy sheet, the higher the concentration of the frozen pores after the water cooling, and the increased nucleation sites of the precipitates, so that the number density of the precipitates can be increased by the continuous aging treatment. Helps increase the strength after aging treatment. When the Co content is less than 0.05% by mass or the P content is less than 0.01% by mass, the amount of precipitation of the P compound is small, and the strength and stress relaxation resistance of the copper alloy cannot be improved. On the other hand, when the Co content exceeds 0.9% by mass or the P content exceeds 0.25 % by mass, the conductivity of 70% IACS or more cannot be achieved in the copper alloy after the aging treatment. Further, coarse oxides, crystallizations, precipitates, and the like are formed, and the hot workability is lowered, and the strength, stress relaxation resistance, and bending workability of the copper alloy sheet are lowered. Therefore, Co is set to 0.05 to 0.9% by mass, and the P content is set to 0.01 to 0.25 mass%. The lower limit of the Co content is preferably 0.10% by mass, more preferably 0.15% by mass, and the upper limit is preferably 0.75% by mass, more preferably 0.60% by mass. The lower limit of the P content is preferably 0.02% by mass, more preferably 0.03% by mass, and the upper limit is preferably 0.23% by mass, more preferably 0.22% by mass. [0028] For the above action, the P content is necessarily in the above range, but on the other hand, the P content which does not contribute to precipitation is preferably as small as possible in the range in which hydrogen embrittlement can be prevented. Based on this, the content ratio of Co to P [Co]/[P] is in the range of 2 to 6. When [Co]/[P] is less than 2, the amount of P which is not solidified in the base material due to the formation of the Co-P compound is increased, and when [Co]/[P] exceeds 6, the Co is solidified in the base material. The amount of the copper alloy plate after the aging treatment cannot be made 70% IACS or more. Further, when [Co]/[P] is less than 2 or more than 6, the amount of Co or P which does not contribute to the formation of the Co-P compound is increased, and the strength after the aging treatment of the copper alloy sheet cannot be sufficiently improved. The lower limit of [Co]/[P] is preferably 2.2, more preferably 2.5, still more preferably 3.0, and the upper limit of [Co]/[P] is preferably 5.0, more preferably 4.5. [0029] The copper alloy may further contain Zn: 1.0% by mass or less (excluding 0% by mass) or/and may contain Fe, Ni, Sn, Si, Al, Mn, Cr, or 0.003 to 0.5% by mass, as needed. One or more of Ti, Zr, Ag, and Mg. However, by adding these elements, it is necessary to avoid the conductivity of the copper alloy sheet after the aging treatment being lower than 70% IACS. Zn has an effect of improving the heat-resistant peeling property of the solder of the copper alloy sheet and the heat-resistant peeling property of the Sn plating. When the heat radiation element is assembled in the semiconductor device, soldering is required, and after the heat radiation element is manufactured, Sn plating may be performed to improve corrosion resistance. When manufacturing such an exothermic element, it is preferred to use a copper alloy plate containing Zn. However, when the Zn content is more than 1.0% by mass, in order to reduce solder wettability, when Zn is contained, the Zn content is 1.0% by mass or less (excluding 0% by mass). The Zn content is preferably 0.7% by mass or less, more preferably 0.5% by mass or less. On the other hand, when the Zn content is less than 0.01% by mass, the improvement of the heat-resistant peeling property is small, and the Zn content is preferably 0.01% by mass or more. The Zn content is more preferably 0.05% by mass or more, further preferably 0.1% by mass or more. When the copper alloy sheet according to the embodiment of the present invention contains Zn, when it is heated at a temperature of 500 ° C or higher, Zn is vaporized by the heating environment, and the surface properties of the copper alloy sheet are lowered to contaminate the heating furnace. The Zn content is preferably 0.5% by mass or less, more preferably 0.4% by mass or less, still more preferably 0.3% by mass or less, and still more preferably 0.2% by mass or less, from the viewpoint of preventing Zn gasification. [0030] Since Fe, Ni, Sn, Si, Al, Mn, Cr, Ti, Zr, Ag, and Mg have an effect of improving the strength and heat resistance of the copper alloy, one or two of the elements are added as needed. More than one species. However, when the content of the elements is large, the electrical conductivity of the copper alloy sheet is lowered. When one or two or more of these elements are added, the total content thereof is in the range of 0.005 to 0.5% by mass. Among the above elements, Fe and Ni form a phosphorus compound ((Ni, Fe)-P compound) with P as well as P. The effect of increasing the strength of the copper alloy sheet due to the formation of the phosphide is Co, which is the largest, followed by Fe and Ni. Fe and Ni have an effect of forming a phosphide with P which does not form a phosphide with Co (a decrease in P which is solid-melted in the base material), and improving the strength of the copper alloy sheet. Further, Fe has an effect of suppressing coarsening of crystal grains at the time of high-temperature heating. In order to obtain such effects, the Fe content is preferably 0.01% by mass or more, and the Ni content is preferably 0.02% by mass or more. On the other hand, in order to suppress a decrease in electrical conductivity, the Fe content is preferably 0.05% by mass or less, and the Ni content is preferably 0.1% by mass or less. [0031] Sn and Mg have an effect of solid-melting in the mother phase of the copper alloy, and improving the strength and stress relaxation resistance of the copper alloy sheet. When the temperature of the heat releasing element or the use environment is 80 ° C or higher, creep deformation occurs, and the contact area with a heat source such as a CPU is small, and the heat radiation property is lowered. However, by suppressing the stress relaxation property, the phenomenon can be suppressed. In order to obtain this effect, the Sn content is preferably 0.02% by mass or more, and the Mg content is preferably 0.01% by mass or more. On the other hand, from the viewpoint of preventing a decrease in the electrical conductivity of the copper alloy sheet, the Sn content is preferably 0.2% by mass or less, and the Mg content is preferably 0.2% by mass or less. Si, Al, and Mn have an effect of improving the strength and heat resistance of the copper alloy. In order to obtain this effect, the content of Si, Al, and Mn is preferably 0.01% by mass or more. On the other hand, from the viewpoint of preventing a decrease in the electrical conductivity of the copper alloy sheet, the Si content is preferably 0.2% by mass or less, the Al content is preferably 0.2% by mass or less, and the Mn content is preferably 0.1% by mass or less. [0032] Cr, Ti, and Zr have an effect of improving the strength and heat resistance of the copper alloy and suppressing coarsening of crystal grains at the time of high-temperature heating. In order to obtain this effect, the Cr content and the Ti content are each preferably 0.01% by mass or more, and the Zr content is preferably 0.005% by mass or more. On the other hand, from the viewpoint of preventing the decrease in the electrical conductivity of the copper alloy sheet, the Cr content is preferably 0.2% by mass or less, the Ti content is preferably 0.1% by mass or less, and the Zr content is preferably 0.05% by mass or less. Moreover, these elements are likely to form a spacer such as an oxide system or a sulfide system of several μm to several 10 μm, and when the above-mentioned spacer is present on the surface, the corrosion resistance of the copper alloy sheet is lowered, but the content of the elements is reduced. When it is in the above range, no particular problem arises. Ag has an effect of improving the strength and heat resistance of the copper alloy. The Ag content is preferably in the range of 0.005 to 0.02% by mass. [0033] H, O, S, Pb, Bi, Sb, Se, and As, which are unavoidable impurities, accumulate at the grain boundary when the copper alloy plate is heated to a temperature of 600 ° C or more for a long time, and causes the particles to be heated and heated. The possibility of cracking and grain boundary embrittlement is good, so it is better to reduce the content of these elements. Since H accumulates at the interface between the grain boundary and the spacer and the base material during heating, it is preferably set to less than 1.5 ppm (mass ppm, the same hereinafter), more preferably less than 1 ppm. O is preferably set to less than 20 ppm, more preferably less than 15 ppm. The total of S, Pb, Bi, Sb, Se, and As is preferably less than 30 ppm, more preferably less than 20 ppm. In particular, in the case of Bi, Sb, Se, and As, the total content of these elements is preferably less than 10 ppm, more preferably less than 5 ppm. [0034] The copper alloy sheet according to the embodiment of the present invention may be subjected to heat treatment of the ingot, by (1) hot calendering-cold calendering-blown, (2) hot calendering-cold calendering-blown-cold calendering, (3) It is produced by the steps of hot rolling, cold rolling, burning, blunt cooling, cold rolling, low temperature burning, and the like. In the above (1) to (3), the step of cold rolling-blowning can be performed plural times. The aforementioned burnt blunt includes softening and blunt, recrystallization blunt or precipitation blunt (aging treatment). When the softening is blunt or the recrystallization is blunt, the heating temperature can be selected from the range of 600 to 950 ° C, and the heating time can be selected from the range of 5 seconds to 1 hour. When the softening or blunt or recrystallization blunt is combined with the melt treatment, it should be continuously blunt at 600~950 °C, preferably 670~900 °C for 3 minutes or less. When aging treatment, it should be carried out under the condition of a temperature range of about 350 to 580 ° C for 0.5 to 10 hours. When the softening is blunt or the recrystallization is blunt and the melt treatment is performed, the aging treatment can be carried out in the subsequent step. [0035] The final cold rolling is suitable to match the target's 0.2% endurance and bending workability, and the self-processing rate is selected from the range of 5 to 80%. In order to restore the ductility of the copper alloy sheet without re-crystallizing the copper alloy sheet and softening it, it is preferable to maintain the temperature in the environment of 300 to 650 ° C for 1 second to 5 minutes depending on the continuous burning. . Moreover, the batch blunt condition should be determined so that the physical temperature of the copper alloy plate is maintained at 250 ° C ~ 400 ° C for 5 minutes ~ 1 hour. According to the above production method, a copper alloy sheet having excellent bending workability of 0.2% withstand strength of 100 MPa or more and elongation of 3% or more can be produced. Further, the copper alloy sheet was heated at 850 ° C for 30 minutes, and then heated at 500 ° C for 2 hours to have an electrical conductivity of 0.2% or more and a conductivity of 70% IACS or more. Further, the surface roughness of the copper alloy sheet (product) which can be joined by a method such as diffusion bonding or welding at a temperature of 600 ° C or higher (with no joint failure and high joint strength) is 0.3 in terms of arithmetic mean roughness Ra. The μm or less is 1.5 μm or less in terms of the maximum height roughness Rz, and the internal oxidation depth is 0.5 μm or less, and desirably 0.3 μm or less. When the surface roughness of the copper alloy sheet (product) is Ra: 0.3 μm and Rz: 1.5 μm or less, the surface roughness of the calender roll for the final cold rolling is, for example, Ra: 0.15 μm, Rz: 1.0. The grinding of the copper alloy sheet after the final cold rolling may be performed by grinding or polishing, electrolytic polishing or the like. Further, when the internal oxidation depth of the copper alloy sheet (product) is 0.5 μm or less, the blunt environment is set to be reductive, and the dew point is set to -5 ° C or lower, or the copper alloy sheet after burning is mechanically machined. Grinding (polishing, brushing, etc.) or electrolytic grinding to remove the resulting internal oxide layer or thinning. [0036] The copper alloy sheet according to the embodiment of the present invention is a standard production method in which the ingot is subjected to heat treatment, and after hot rolling, recrystallization treatment and cold rolling are performed by cold rolling and melt reduction (may be omitted). Manufactured by the steps of aging treatment. The cold rolling after the recrystallization treatment accompanying the melt can be omitted. Further, after the aging treatment, cold rolling may be further performed. The copper alloy sheet produced by the production method has a high strength (0.2% withstand force of 300 MPa or more) and an elongation of 3% or more, and has excellent bending workability. Further, the copper alloy sheet was heated at 850 ° C for 30 minutes, and then heated at 500 ° C for 2 hours to have an electrical conductivity of 0.2% or more and a conductivity of 70% IACS or more. [0037] Melting and casting can be carried out by a usual method such as continuous casting or semi-continuous casting. Further, as the copper melting raw material, those having a small content of S, Pb, Bi, Se, and As are preferably used. In addition, attention is paid to the red heating (moisture removal) of the charcoal coated with the copper alloy melt, the bare metal, the waste material, the casting water conduit, the drying of the mold, and the deoxidation of the melt, etc., and it is preferable to reduce O and H. [0038] The homogenization treatment is preferably carried out for 30 minutes or more after the inside of the ingot reaches a temperature of 500 ° C or higher. The holding time of the homogenization treatment is more preferably 1 hour or more, more preferably 2 hours or more. After the homogenization treatment, hot rolling is started at a temperature of 800 ° C or higher. It is preferred to terminate the hot rolling at a temperature of 600 ° C or higher without forming coarse Co-P precipitates in the hot rolled material, and to quench from the temperature by water cooling or the like. When the quenching start temperature after hot rolling is lower than 600 ° C, coarse Co-P precipitates are easily formed, the structure becomes uneven, and the strength of the copper alloy sheet (product sheet) is lowered. The end temperature of the hot rolling is preferably a temperature of 600 ° C or higher, more preferably 700 ° C or higher. Further, the structure of the hot rolled material which is quenched by hot rolling becomes a recrystallized structure. The recrystallization treatment accompanying the melting described later can also perform rapid cooling after hot rolling. [0039] After the cold rolling after hot rolling, a certain stress is applied to the copper alloy sheet, and after the recrystallization treatment, a copper alloy sheet having a desired recrystallized structure (fine recrystallized structure) is obtained. The recrystallization treatment accompanying the melt is carried out at 600 to 950 ° C, preferably at 670 to 900 ° C for 3 minutes or less. When the content of Co and P in the copper alloy is small, it is preferably carried out in a lower temperature region than in the above temperature range, and when the content of Co and P is large, it is preferably carried out in a higher temperature region than in the above temperature range. By this recrystallization treatment, Co and P are solid-melted in the copper alloy base material, and a recrystallized structure (crystal grain size: 1 to 20 μm) excellent in bending workability can be formed. When the recrystallization treatment temperature is lower than 600 ° C, the amount of solid solution of Co and P to the base material decreases, and the strength after the aging treatment decreases. On the other hand, when the temperature of the recrystallization treatment exceeds 950 ° C or the treatment time exceeds 3 minutes, the recrystallized grains are coarsened. [0040] After the recrystallization treatment with the melt, (a) aging treatment, (b) cold rolling and aging treatment, (c) cold rolling and aging treatment, and then cold calendering to the thickness of the product, or (d) Low temperature burn-off (ductility recovery) was carried out after (c) above. The aging treatment is carried out under the conditions of a heating temperature of about 300 to 580 ° C for 0.5 to 10 hours as described above. When the heating temperature is less than 300 ° C, the amount of precipitation is small, and when it exceeds 580 ° C, the precipitate is liable to become coarse. The lower limit of the heating temperature is preferably 350 ° C, and the upper limit is preferably 570 ° C, more preferably 560 ° C. The retention time of the aging time is appropriately selected depending on the heating temperature, and is carried out in the range of 0.5 to 10 hours. When the retention time was less than 0.5 hours, the precipitation became insufficient, and even if the precipitation amount was saturated over 10 hours, the productivity was lowered. The lower limit of the holding time is preferably 1 hour, more preferably 2 hours. [Example 1] [0041] A copper alloy having a composition shown in Tables 1 and 2 was cast, and an ingot having a thickness of 45 mm was produced. In the copper alloy, H of the unavoidable impurities was less than 1 ppm, O was less than 15 ppm, and the total of S, Pb, Bi, Sb, Se, and As was less than 20 ppm. Each of the ingots was subjected to a soaking treatment at 965 ° C for 3 hours, followed by hot rolling to obtain a hot rolled material having a thickness of 15 mm, and quenched (water-cooled) from a temperature of 650 ° C or higher. After both surfaces of the hot rolled material after quenching were polished to 1 mm, cold-rolling was performed until the target thickness was 0.6 mm, and the film was kept at 800 ° C for 20 seconds for recrystallization treatment (with melt formation). Next, after 500 hours of precipitation at 500 ° C for 2 hours, 50% of the finishing cold rolling was applied to form a plate thickness of 0.3 mm, and further cold burning at 330 ° C for 20 seconds (stress elimination burnt) to produce a copper alloy. board. Further, the composition of each of the copper alloy sheets having a thickness of 0.3 mm (comparative example No. 2 hot-rolled cracked material) was also the same as the values of Tables 1 and 2. Further, regarding each of the copper alloy sheets (excluding Comparative Example No. 2), the surface roughness Ra: 0.08 to 0.15 μm, and Rz: 0.8 to 1.2 μm, and the thickness of the plate was examined by a scanning electron microscope (observation magnification: 15,000 times). The internal oxidation depth measured was 0.1 μm or less. [0042] [0043] [0044] Using the obtained copper alloy sheet as a test material, each measurement test of electrical conductivity, mechanical properties, bending workability, and solder wettability was carried out in the following manner. The results are shown in Tables 3 and 4. Further, the obtained copper alloy sheet was heated at 850 ° C for 30 minutes, and then water-cooled, and further heated at 500 ° C for 2 hours (aging precipitation treatment) as test materials, and each measurement test of electrical conductivity and mechanical properties was carried out. The results are shown in Tables 3 and 4. (Measurement of Conductivity) The conductivity was measured by a four-terminal method using a double bridge in accordance with the conductivity measurement method of a non-ferrous metal material specified in JIS-H0505. (Mechanical characteristics) A JIS No. 5 tensile test piece was cut out from the test piece so that the longitudinal direction thereof became a parallel direction of rolling, and a tensile test was carried out in accordance with JIS-Z2241, and the endurance and elongation were measured. Endurance is equivalent to a tensile strength of 0.2% of permanent elongation. (Bending Processability) The measurement of the bending workability was carried out in accordance with the W bending test method specified in the Copper Bronze Association Standard JBMA-T307. A test piece having a width of 10 mm and a length of 30 mm was cut out from each of the test materials, and a fixture of R/t = 1.0 was used to carry out GW (Good Way (vertical axis and rolling direction)) and BW (Bad Way (bending axis and rolling direction). Parallel))). Next, the crack was observed by visual observation of the bending portion by a 100-fold optical microscope, and those having neither GW nor BW cracked were evaluated as P (P: Pass, qualified), and one of GW and BW or both of them had a turtle. The cracker was evaluated as F (F: Fall, unqualified). (Solder Moisture Resistance) A short strip test piece having a width of 10 mm and a length of 35 mm was used in the longitudinal direction and the rolling direction of each of the test materials, and was used in an inactive flux (α100 manufactured by Japan's αMetallized Co., Ltd.). After dip coating for 1 second, the solder dampening time was measured by a menzograph method (according to JIS C0053 welding test method (balance method), SAT 5100 manufactured by RHESCA Co., Ltd.). The solder was used under the test conditions of Sn-3 mass% Ag-0.5 mass% Cu maintained at 260 ± 5 ° C, impregnation speed of 25 mm/sec, impregnation depth of 5 mm, and immersion time of 5 seconds. When the solder dampening time was 2 seconds or less, it was evaluated that the solder wettability was excellent. Further, in addition to Comparative Example 5, the solder dampening time was 2 seconds or shorter. [0048] [0049] [0050] The copper alloy plate alloy compositions of Examples 1 to 18 shown in Tables 1 and 3 satisfy the requirements of the embodiments of the present invention, and are heated at 850 ° C for 30 minutes, followed by heating at 500 ° C for 2 hours. The strength (0.2% proof) is 150 MPa or more, and the electric conductivity is 70% IACS or more. In addition, the copper alloy sheet before heating at 850 ° C has a characteristic strength (0.2% proof) of 100 MPa or more, an elongation of 3% or more, and excellent bending workability and solder wettability. After heating at 850 ° C, most of them have a strength of 50 MPa or more (0.2% proof). Further, in Example 6, the content of Co and P was close to the lower limit, the endurance value after the aging treatment was 162 MPa, and the hardness was Hv83 (measured at a test force of 0.49 N). On the other hand, in the copper alloy sheets of Comparative Examples 1 to 8 shown in Tables 2 and 4, some characteristics were inferior as shown below. In Comparative Example 1, since the Co content was excessive, the bending workability was poor, and the strength and conductivity after the aging treatment were low. In Comparative Example 1, since the P content was excessive, the hot pressing time was cracked, and the step after the hot rolling could not be performed. Comparative Example 3 was high in [Co]/[P], and the strength and electrical conductivity after the aging treatment were low. In Comparative Example 4, [Co]/[P] was low, and the strength and electrical conductivity after the aging treatment were low. Comparative Example 5 was that the Zn content was excessive, and the solder wettability was poor as described above. In Comparative Example 6, since the total amount of elements other than the main elements (Al, Mn, etc.) was excessive, the electrical conductivity after the aging treatment was low. In Comparative Example 7, since the P content was insufficient, the strength and electrical conductivity after the aging treatment were low. In Comparative Example 8, since the Co content was insufficient, the strength after the aging treatment was low. [Example 2] [0052] The representative of the copper alloy sheets shown in Tables 1 and 2 (Examples 2, 10, Comparative Examples 3 and 4) were heated at 1000 ° C for 30 minutes, then water-cooled, and further at 500 ° C. After heating for 2 hours (aging treatment), the copper alloy sheet was used as a test material, and each measurement test of electrical conductivity and mechanical properties was carried out by the method described in Example 1. The results are shown in Table 5. [0053] As shown in Table 5, Examples 2 and 10 were heated at 1000 ° C for 30 minutes, and then the strength (0.2% proof) after the aging treatment was 150 MPa or more, and the electric conductivity was 70% IACS or more. The values shown in Table 5 were compared with those at 850 ° C for 30 minutes, and the results of the subsequent aging treatment (reference table) were not significantly different. On the other hand, Comparative Examples 3 and 4 were heated at 1000 ° C for 30 minutes, and then the strength and electrical conductivity after the aging treatment were not up to the standard (0.2% proof stress was 150 MPa or more, and electrical conductivity was 70% IACS or more). [0055] The disclosure of the present specification includes the following aspects. Aspect 1: A copper alloy plate for an exothermic element, characterized by Co: 0.05 to 0.9% by mass, P: 0.01 to 0.25 mass%, and the remainder is formed of Cu and inevitable impurities, and the Co content is set to [Co ] When the P content is [P], [Co]/[P] is 2 to 6, 0.2% withstand strength is 100 MPa or more, elongation is 3% or more, and it has excellent bending workability, and is heated at 850 ° C for 30 minutes. After water cooling, followed by heating at 500 ° C for 2 hours, the 0.2% endurance of the aging treatment is 150 MPa or more, and the electrical conductivity is 70% IACS or more. In one part of the process of manufacturing the exothermic element, the process of heating to 600 ° C or more is included. . Aspect 2: A copper alloy plate for a heat releasing element of the aspect 1, which further contains 1.0% by mass or less (excluding 0% by mass) of Zn. Aspect 3: A copper alloy plate for a heat releasing element according to claim 1 or 2, which further contains Fe, Ni, Sn, Si, Al, Mn, Cr, Ti, Zr, Ag, Mg in a total amount of 0.005 to 0.5% by mass One or two or more. Aspect 4: A method for producing an exothermic element, characterized in that the exothermic element according to any one of the aspects 1 to 3 is processed into a specific shape by a copper alloy sheet, and then heated to a temperature of 600 ° C or higher, and then The aging treatment is performed by applying plastic working to obtain a heat releasing element having a resistance of 0.2% or more and a conductivity of 70% IACS or more. Aspect 5: The method for producing a heat releasing member according to Aspect 4, wherein after the aging treatment, at least a portion of the outer surface of the heat releasing member forms a Sn coating layer. Aspect 6: The method for producing a heat releasing member according to aspect 4, wherein after the aging treatment, at least a portion of the outer surface of the heat releasing member forms a Ni coating layer. [0056] The present application claims priority on the basis of the Japanese Patent Application No. 2016-190664, filed on Sep. 26, 2016. Japanese Patent Application No. 2016-190664 is incorporated herein by reference.