JPH0627698B2 - Specimen mounting device for compound environment test equipment - Google Patents
Specimen mounting device for compound environment test equipmentInfo
- Publication number
- JPH0627698B2 JPH0627698B2 JP60072536A JP7253685A JPH0627698B2 JP H0627698 B2 JPH0627698 B2 JP H0627698B2 JP 60072536 A JP60072536 A JP 60072536A JP 7253685 A JP7253685 A JP 7253685A JP H0627698 B2 JPH0627698 B2 JP H0627698B2
- Authority
- JP
- Japan
- Prior art keywords
- test piece
- test
- heat storage
- storage body
- environment
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G7/00—Simulating cosmonautic conditions, e.g. for conditioning crews
- B64G2007/005—Space simulation vacuum chambers
Landscapes
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
- Testing Resistance To Weather, Investigating Materials By Mechanical Methods (AREA)
Description
【発明の詳細な説明】 〔産業上の利用分野〕 この発明は、複合環境試験装置に関し,特に複合環境試
験装置の試験片装着装置に関するものである。Description: TECHNICAL FIELD The present invention relates to a complex environment test apparatus, and more particularly to a test piece mounting apparatus for the complex environment test apparatus.
最近の材料技術の発達はめざましく,特に新しく開発さ
れた素材を使用した新有機材料の開発はめざましいもの
がある。これらの新素材の使用環境は多岐に渡つてお
り,空気中,常温,常圧の通常環境から,宇宙,核融合
装置等の放射線環境,超電導機器の極低温環境等の極限
環境へと使用範囲が拡大されてきている。このような使
用環境の拡大に伴つて,それらの特殊な使用環境での材
料の信頼性の把握,特に材料劣化特性の把握,及び劣化
要因と環境条件との相関性の把握といつた環境試験が重
要な技術として位置ずけられて来ている。The recent development of material technology is remarkable, and in particular, the development of new organic materials using newly developed materials is remarkable. The environment in which these new materials are used is wide-ranging, ranging from the normal environment of air, room temperature, and atmospheric pressure to the extreme environment of radiation environment such as space and fusion devices, and cryogenic environment of superconducting equipment. Is being expanded. With the expansion of such usage environment, the reliability of materials in those special usage environments, especially the material deterioration characteristics, and the correlation between deterioration factors and environmental conditions, and environmental tests Has been positioned as an important technology.
従来の環境試験装置において,特に試料を高温に加熱し
た状態において機械的特性を測定することができる環境
試験装置では,その用途が限定され使用頻度も少なかつ
たこと等から,装置には1個の試料を装着し,目的とす
る環境条件にした後,特性を測定するのが一般的であつ
た。In the conventional environmental test equipment, especially the environmental test equipment that can measure the mechanical characteristics in the state where the sample is heated to a high temperature, one application is available because the application is limited and the usage frequency is low. It was common to attach the sample of (1) to the desired environmental conditions and then measure the characteristics.
第3図は従来の機械特性を測定することができる環境試
験装置の部分断面図である。図において,環境試験装置
(25)は目的とする環境を作るための恒温箱(27)と,恒温
箱(27)の壁を貫通し引張試験機(26)に連結されたプルロ
ツド(3)固定ロツド(4),及びプルロツド(3)固定ロツド
(4)に結合した連結具(7b)とを備えている。恒温箱(27)
は,恒温箱(27)内を高温状態にするための空気加熱供給
装置(33),及び加熱された空気を循環させる為の熱風供
給風路(31)熱風戻り風路(32)とを備えている。また,プ
ルロツド(3)固定ロツド(4)が恒温箱(27)壁を貫通してい
るために,恒温箱(27)内が加熱された時,恒温箱(27)壁
とプルロツド(3)固定ロツド(4)との隙間からの熱放散を
防ぎつつ,機械特性測定時にプルロツド(3)の動きに影
響を及ぼさないように工夫された断熱栓(30)と、試験中
に恒温箱(27)の内部を観察するための窓(28)とを備えて
いる。更に,恒温箱(27)は架台(22)に取りつけられてお
り,この架台(22)とプルロツド(3)固定ロツド(4)とは同
一中心線上に配置されている。FIG. 3 is a partial cross-sectional view of a conventional environment test apparatus capable of measuring mechanical characteristics. In the figure, environmental test equipment
(25) is a constant temperature box (27) for creating a desired environment, a pull rod (3) fixed rod (4) that penetrates the wall of the constant temperature box (27) and is connected to a tensile tester (26), and Pull rod (3) Fixed rod
And a coupling tool (7b) coupled to (4). Constant Temperature Box (27)
Is provided with an air heating supply device (33) for raising the temperature inside the constant temperature box (27), and a hot air supply air passage (31) and a hot air return air passage (32) for circulating the heated air. ing. Further, since the pull rod (3) fixing rod (4) penetrates the constant temperature box (27) wall, when the inside of the constant temperature box (27) is heated, the constant temperature box (27) wall and the pull rod (3) are fixed. A heat insulating plug (30) designed to prevent the heat dissipation from the gap between the rod (4) and the movement of the pull rod (3) during mechanical characteristics measurement, and a constant temperature box (27) during the test. And a window (28) for observing the inside of the. Further, the constant temperature box (27) is attached to the mount (22), and the mount (22) and the pull rod (3) and the fixed rod (4) are arranged on the same center line.
このようにして構成された従来の環境試験装置(25)にお
いて,高温の環境下で機械特性を測定する場合,あらか
じめ試験片(5)に試験片固定具(6b)を取付けておき,恒
温箱(27)の扉(図示せず)を開けた後,プルロツド(3)
固定ロツド(4)双方に結合した連結具(7b)にピン(29)を
用いて,試験片(5)が固定された試験片固定具(6b)を連
結する。その後,恒温箱(27)の扉を閉め,空気加熱供給
装置(33)を用いて恒温箱(27)内を要求温度まで加熱す
る。空気加熱供給装置(33)で加熱された空気は空気加熱
供給装置(33)に内臓したフアンにより送り出され、熱風
供給風路(31)を通り恒温箱(27)内を循環し熱風戻り風路
(32)を通つて空気加熱供給装置(33)に戻る。従つて,試
験片(5)は空気を媒体とした熱伝導により加熱される。
試験片(5)が要求温度に達すると引張試験機械(26)を用
いて高温下での試験片(5)の機械的特性を測定しデータ
を記録する。測定が終ると恒温箱(27)の扉を開け,ピン
(29)を抜いて試験片固定具(6b)と供に試験片(5)を取り
出し、次に試験片(5)を前述した手順で取付け,同様に
して試験片(5)を加熱し,機械的特性の測定を行う。試
験片(5)の数が多い場合は前述した内容を繰返すのであ
る。When measuring the mechanical properties in a high temperature environment in the conventional environment test device (25) configured as described above, the test piece fixture (6b) is attached to the test piece (5) in advance, and the constant temperature box is attached. After opening the door (not shown) of (27), pull rod (3)
The test piece fixture (6b) to which the test piece (5) is fixed is connected using the pin (29) to the connection tool (7b) connected to both the fixed rods (4). After that, the door of the constant temperature box (27) is closed and the inside of the constant temperature box (27) is heated to the required temperature by using the air heating supply device (33). The air heated by the air heating supply device (33) is sent out by a fan incorporated in the air heating supply device (33), circulates in the constant temperature box (27) through the hot air supply air passage (31) and returns to the hot air return air passage.
It returns to the air heating supply device (33) through (32). Therefore, the test piece (5) is heated by heat conduction using air as a medium.
When the test piece (5) reaches the required temperature, the tensile test machine (26) is used to measure the mechanical properties of the test piece (5) at high temperature and record the data. When the measurement is completed, open the constant temperature box (27) door, and
(29) is removed and the test piece (5) is taken out together with the test piece fixture (6b), and then the test piece (5) is attached by the procedure described above, and the test piece (5) is heated in the same manner. Measure the mechanical properties. When the number of test pieces (5) is large, the above-mentioned contents are repeated.
このように従来の機械特性を測定することができる環境
試験装置では,1個の試験片の測定が終了して次の試験
片の測定を行う迄には,試験片の取外し,取付けや,再
び試験片を試験条件まで加熱するのに多くの時間を要す
るという問題点,試験ごとに試験環境条件が同一条件に
なりにくく,データの信頼性が低下するという問題点が
あった。また、最近のように新材料の開発がめざまし
く,また材料の使用環境が多様化して来ている中で,多
くの試験片の特性の把握と信頼性のあるデータが要求さ
れている時に,データの取得に多くの時間がかかりコス
ト的にも非常に高くつくという大きな問題点があつた。
更に,空気を媒体とした試験片加熱方式であるため新材
料の宇宙環境での使用に対して,宇宙環境を模した環境
条件下において機械特性を測定することができないとい
う大きな問題点があつた。As described above, in the conventional environment test apparatus capable of measuring mechanical properties, the test piece is removed, attached, or re-installed before the measurement of one test piece is completed and the measurement of the next test piece is performed. There are problems that it takes a lot of time to heat the test piece to the test conditions, and it is difficult for the test environment conditions to be the same for each test, and the reliability of the data decreases. In addition, with the recent remarkable development of new materials and the diversification of the environment in which the materials are used, it is necessary to grasp the characteristics of many test pieces and obtain reliable data. There was a big problem that it took a lot of time to obtain and the cost was very high.
Furthermore, since the test piece heating method uses air as a medium, there is a big problem that the mechanical properties cannot be measured under the environmental conditions simulating the space environment when the new material is used in the space environment. .
この発明は,上記のような欠点に鑑みてなされたもの
で,複合環境(宇宙環境を模擬することを目的として,
真空,温度,紫外線,放射線等の複数の環境条件を組合
せた状態をいう。以下同じ)の同一環境条件において連
続的に複数試験片の試験を行うことのできる試験片装着
装置を備えた複合環境試験装置を試験片装着装置を得る
ことを目的とする。The present invention has been made in view of the above drawbacks, and aims to simulate a mixed environment (space environment,
A state in which multiple environmental conditions such as vacuum, temperature, ultraviolet rays, and radiation are combined. The same shall apply hereinafter) for the purpose of obtaining a composite environment test apparatus equipped with a test strip mounting apparatus capable of continuously testing a plurality of test strips under the same environmental conditions.
この発明の複合環境試験装置の試験片装着装置は、真空
排気装置を有する真空容器,この真空容器内に複数の試
験片固定具を介して保持される複数の試験片,上記試験
片固定具および試験片のうちの少なくとも一方と接触す
る蓄熱体,この蓄熱体と摺接し上記試験片を加熱・冷却
するヒートシンク,上記試験片に放射線を照射する放射
線照射装置,上記試験片に紫外線を照射する紫外線照射
装置,ベローズを介して上記真空容器内を貫通するロッ
ドを有し上記試験片の機械特性を試験する機械特性試験
機,並びに上記試料の化学的および物理的構造特性を測
定する機器分析装置を備え,取り付けた上記試験片固定
具を移動させ,上記試験片固定具を介して保持された試
験片を上記ロッドに取り付けられた連結具に順次装脱着
して試験に供する試験片装着装置を設けたものである。A test strip mounting apparatus for a composite environment test apparatus according to the present invention includes a vacuum container having an evacuation device, a plurality of test strips held in the vacuum container via a plurality of test strip fixtures, the test strip fixture, and A heat storage body that contacts at least one of the test pieces, a heat sink that slides in contact with the heat storage body to heat and cool the test piece, a radiation irradiation device that irradiates the test piece with radiation, and an ultraviolet ray that irradiates the test piece with ultraviolet light. An irradiation device, a mechanical property tester having a rod penetrating the inside of the vacuum container via a bellows, for testing the mechanical properties of the test piece, and an instrumental analysis device for measuring the chemical and physical structural properties of the sample. The test piece fixture provided and moved is moved, and the test piece held via the test piece fixture is sequentially attached to and detached from the connecting tool attached to the rod for the test. Kenhen is provided with a mounting device.
この発明においては,複数の試験片固定具が試験片装着
装置に取り付けられており,予め複数の試験片を取り付
けておくと試験片装着装置により,試験終了ごとに試験
片が交換装着されるので,同一環境条件において,連続
的に複数試験片の試験を行うことができる。さらに,ヒ
ートシンクにより,急激でしかも温度差の大きな加熱,
冷却が可能となる。In the present invention, a plurality of test piece fixtures are attached to the test piece attaching device, and if a plurality of test pieces are attached in advance, the test piece attaching device replaces and attaches the test pieces after each test. , Multiple test pieces can be continuously tested under the same environmental conditions. In addition, the heat sink allows rapid heating with a large temperature difference,
Cooling becomes possible.
この発明は人工衛星が衛星軌道上で遭遇する宇宙環境と
同じ効果を持つた場を作り出し,人工衛星に使用される
材料の宇宙環境下での材料劣化特性の把握,及び劣化要
因と環境条件との相関性等を把握するための複合環境試
験装置,特にその試験片装着装置についてである。This invention creates a field that has the same effect as the space environment encountered by an artificial satellite in orbit, grasps the material deterioration characteristics of the material used for the artificial satellite in the space environment, and determines the deterioration factors and environmental conditions. It is about a complex environment tester, especially its test piece mounting device, for grasping the correlation and the like.
宇宙環境下においては,人工衛星に使用される繊維強化
複合材料,誘電材料あるいは各種モールド用樹脂等の材
料は,熱真空の為に熱分解しガスが発生する。これらは
材料の性能変化,更には脱ガス成分が他の機器に付着し
材料劣化による衛星の故障原因となる。これらの問題を
正確に把握する為には,宇宙環境に晒された材料を空気
中に取り出すと特性が変化すると考えられるので,宇宙
環境状態のままでの諸特性の変化や劣化,劣化プロセス
およびメカニズムを評価,検討することが最も重要とな
る。In a space environment, materials such as fiber-reinforced composite materials, dielectric materials, and various molding resins used for artificial satellites are thermally decomposed due to thermal vacuum to generate gas. These cause changes in material performance, and degassed components adhere to other equipment, which can cause satellite failure due to material deterioration. In order to accurately understand these problems, it is considered that the characteristics will change if the material exposed to the space environment is taken out into the air. It is most important to evaluate and study the mechanism.
また,現在宇宙開発事業団等で検討が進められている大
規模宇宙構造体開発構想においては,構造体の寿命を3
0年としている。従つて,宇宙環境劣化を地上において
実施するとき,実環境との類似性,相似性,更には,3
0年間に宇宙環境下で受ける材料劣化の加速性等が問題
となる。従つて,宇宙環境を模擬し多数の試料を連続し
てその状態で評価することのできる複合環境試験装置
は,人工衛星材料の信頼性評価技術を確立するためには
今や必要不可欠のものとなつている。In addition, in the large-scale space structure development concept currently being studied by the Japan Space Agency, etc.
It has been 0 years. Therefore, when the space environment deterioration is carried out on the ground, the similarity with the actual environment, the similarity, and 3
There is a problem with the acceleration of material deterioration that occurs in the space environment in 0 years. Therefore, a complex environment tester that can simulate a space environment and continuously evaluate a large number of samples in that state is now indispensable for establishing a reliability evaluation technique for satellite materials. ing.
以下,この発明の複合環境試験装置の一部分の試験片装
着装置を図に基いて説明する。第1図(A)および第1図
(B)はこの試料装着装置の基本的な一実施例を示す断面
構成図である。図において,複合環境試験装置(1)は真
空容器(2),機械特性試験機,この場合は引張試験機
(図示せず)に連結されたプルロツド(3)および固定ロ
ツド(4),試験片(5),試験片(5)の両端に取付けられた
紙片片固定具(6a),継ぎロツド(8)と結合した連結具(7
a),試験片固定具(6a)により保持された試験片(5)を4
個装着することができ,試験片(5)を加熱,冷却するた
めの蓄熱体(11)を備えた回転式の試験片装着部材(10),
試験片装着部材(10)を駆動するための駆動軸(13),試験
片装着部材(10)の回転停止位置を決める位置決め機構(1
4),試験片装着部材(10)の蓄熱体(11)に摺接したヒート
シンク(17),シユラウド(21),真空排気装置(23-1)や紫
外線照射装置(23-2),放射線照射装置(23-3)機器分析装
置(23-4)を接続するための外部機器接続ポート(23)を備
えている。ここで,試験片装着装置は試験片装着部材(1
0),駆動軸(13)及び位置決め機構(14)等から構成され
る。ヒートシンク(17)にはヒートシンク加熱系(18)に接
続されたヒーターやヒートシンク冷却系(19)に接続され
た冷却用導管が埋込まれている。加熱・冷却手段は蓄熱
体(11),ヒートシンク(17),ヒートシンク加熱系(18),
ヒートシンク冷却系(19)等から構成される。試験片装着
部材(10)には上部と下部に熱伝導性が良好で熱容量の大
きい蓄熱体(11)を配置している。この上部の蓄熱体(11)
に試験片固定具(6a)が吊下がる形で固定されており,蓄
熱体(11)と試験片(5)および試験片固定具(6a)とは広範
囲な接触面で接している。更に,上部と下部の蓄熱体(1
1)は同様に上部と下部に設けられたヒートシンク(17)と
摺接面を有しており,固定されたヒートシンク(17)に対
し,試験片装着部材(10)の蓄熱体(11)は回転しながら熱
伝導を受けることができる構造となつている。また,上
部の蓄熱体(11)と下部の蓄熱体(11)の間にはバネ(12)が
設けられており,熱膨張,収縮が生じても蓄熱体(11)は
絶えずヒートシンク(17)の摺接面に接する構造となつて
いる。A test piece mounting device which is a part of the composite environment test device of the present invention will be described below with reference to the drawings. Figure 1 (A) and Figure 1
(B) is a cross-sectional configuration diagram showing a basic embodiment of the sample mounting apparatus. In the figure, the composite environment test device (1) is a vacuum container (2), a mechanical property tester, in this case a pull rod (3) and a fixed rod (4) connected to a tensile tester (not shown), and a test piece. (5), a piece of paper piece fixing device (6a) attached to both ends of the test piece (5), and a connecting device (7) connected to the connecting rod (8).
a), the test piece (5) held by the test piece fixture (6a)
A rotary test piece mounting member (10), which can be individually mounted and has a heat storage body (11) for heating and cooling the test piece (5),
A drive shaft (13) for driving the test piece mounting member (10), and a positioning mechanism (1) for determining the rotation stop position of the test piece mounting member (10)
4), heat sink (17) slidingly contacting heat storage body (11) of test piece mounting member (10), shroud (21), vacuum exhaust device (23-1), ultraviolet irradiation device (23-2), radiation irradiation The device (23-3) is provided with an external device connection port (23) for connecting the device analyzer (23-4). Here, the test piece mounting device is a test piece mounting member (1
0), drive shaft (13), positioning mechanism (14), etc. A heater connected to the heat sink heating system (18) and a cooling conduit connected to the heat sink cooling system (19) are embedded in the heat sink (17). The heating / cooling means is a heat storage body (11), heat sink (17), heat sink heating system (18),
It is composed of a heat sink cooling system (19) and the like. The test piece mounting member (10) is provided with heat storage bodies (11) having good thermal conductivity and large heat capacity at the upper and lower portions. This upper heat storage (11)
The test piece fixture (6a) is fixed in a hanging manner to the heat storage body (11) and the test piece (5) and the test piece fixture (6a) are in contact with each other over a wide range of contact surfaces. In addition, the upper and lower heat storage (1
Similarly, 1) has a sliding contact surface with the heat sinks (17) provided on the upper and lower parts, and the heat storage body (11) of the test piece mounting member (10) is different from the fixed heat sink (17). It has a structure that can receive heat conduction while rotating. Further, a spring (12) is provided between the upper heat storage body (11) and the lower heat storage body (11), and the heat storage body (11) constantly heatsinks (17) even if thermal expansion and contraction occur. The structure is in contact with the sliding surface of.
試験片(5)および試験片固定具(6a)は上部,下部の蓄熱
体(11)に対しては回転、転倒,落下を防止するように固
定されているが,機械特性試験実施時の試験荷重方向に
対しては自由に動く様に設計されている。更に,試験片
装着部材(10)に取付ける試験片固定具(6a)の取付け位置
は,試験片固定具(6a)の公転軌道上に、プルロツド
(3),固定ロツド(4)の中心線が来るように構成されてお
り,試験片固定具(6a)と連結具(7a)の連結は,試験片装
着部材(10)の回転によつて試験片固定具(6a)が連結具(7
a)に装着されるように設計されている。この時の試験片
装着部材(10)の回転停止位置は位置決め機構(14)によつ
て,試験片(5)がプルロツド(3),固定ロツド(4)と同一
中心線上になるように設計されている。また,試験片装
着部材(10)の駆動は,遠隔操作によつて駆動モータ(16)
を動かし,位置決め機構(14),駆動軸(13)を経て,回転
が与えられる構造となつている。The test piece (5) and the test piece fixture (6a) are fixed to the upper and lower heat storage bodies (11) so as to prevent them from rotating, tipping over, and falling. It is designed to move freely in the load direction. Further, the mounting position of the test piece fixture (6a) to be attached to the test piece mounting member (10) should be such that the pull rod is on the orbit of the test piece fixture (6a).
(3), the center line of the fixed rod (4) is arranged to come, and the connection between the test piece fixing tool (6a) and the connecting tool (7a) is performed by the rotation of the test piece mounting member (10). The test piece fixture (6a) is
It is designed to be attached to a). The rotation stop position of the test piece mounting member (10) at this time is designed by the positioning mechanism (14) so that the test piece (5) is on the same center line as the pull rod (3) and the fixed rod (4). ing. The test piece mounting member (10) is driven by a drive motor (16) by remote control.
The structure is such that rotation is given via the positioning mechanism (14) and drive shaft (13) by moving the.
また,プルロツド(3),固定ロツド(4)は真空容器(2)内
の複合環境を外部環境から遮断しつつ,機械的負荷を伝
達させるため,ベローズ(9)によるシール構造となつて
いる。更に,試験片装着部材(10)の駆動軸(13)から真空
容器(2)への熱放散を防止するため,断熱スリーブを内
蔵した断熱軸受(20)を備えている。Further, the pull rod (3) and the fixed rod (4) have a sealing structure by the bellows (9) in order to transmit the mechanical load while blocking the complex environment in the vacuum vessel (2) from the external environment. Further, in order to prevent heat dissipation from the drive shaft (13) of the test piece mounting member (10) to the vacuum vessel (2), a heat insulating bearing (20) having a heat insulating sleeve is provided.
上記のように構成されるこの発明の一実施例において,
複合環境下で機械特性を測定する場合,予め試験片(5)
に試験片固定具(6a)を取付けた状態の試験片(5)を複数
個用意しておき,真空容器(2)の扉(図示せず)を開け
た後,真空容器(2)内に設けた試験片装着部材(10)に,
予め用意された試験片固定具(6a)を取付けた試験片(5)
を4個取付ける。その後,真空容器(2)の扉を閉めた
後,真空容器(2)内を高真空にする。この状態でヒート
シンク(17)を用いて試験片(5)を加熱,あるいは冷却す
る。ヒートシンク(17)からの熱は摺接する蓄熱体(11)を
通じ,蓄熱体(11)に広範囲の面で接触する試験片(5)お
よび試験片固定具(6a)を熱伝導により加熱,冷却する。
更にはこの状態で放射線,紫外線等を照射するなど,一
定の要求複合環境条件にして試験片(5)を劣化させる。
試験片(5)が予定の劣化量に達すると,遠隔操作によつ
て駆動モータ(16)により駆動軸(13)を駆動し,試験片装
着部材(10)を回転させ試験片(5)を連結具(7a)に装着す
る。そこで引張試験機を用いてクロスヘツドを動かし,
プルロツド(3)により試験片(5)を引張り,機械特性の測
定を行う。プルロツド(3)はベローズ(9)を介して連結具
(7a)に連結されているので,複合環境を維持したまま真
空容器(2)の外部から機械的試験を行うことができる。
試験片(5)を一定の要求環境条件下で劣化させた後,機
械特性試験ができる状態になつてから試験片装着部材(1
0)を回転させ連結具(7a)に装着するには,加熱あるいは
冷却された試験片(5)から試験片固定具(6a)を通じて熱
伝導による熱損失を小さくするためである。In one embodiment of the present invention configured as described above,
When measuring mechanical properties in a complex environment, test pieces (5) in advance
Prepare a plurality of test pieces (5) with the test piece fixtures (6a) attached to them, open the door (not shown) of the vacuum vessel (2), and then put them in the vacuum vessel (2). On the provided test piece mounting member (10),
Test piece (5) with the test piece fixture (6a) prepared in advance
Install 4 pieces. Then, after closing the door of the vacuum container (2), the inside of the vacuum container (2) is made into a high vacuum. In this state, the heat sink (17) is used to heat or cool the test piece (5). The heat from the heat sink (17) heats and cools the test piece (5) and the test piece fixture (6a), which come into contact with the heat storage body (11) on a wide range, by heat conduction, through the heat storage body (11) in sliding contact. .
Further, in this state, the test piece (5) is deteriorated by irradiating with radiation, ultraviolet rays, etc. under a certain required complex environmental condition.
When the test piece (5) reaches the expected deterioration amount, the drive shaft (13) is driven by the drive motor (16) by remote control, and the test piece mounting member (10) is rotated to move the test piece (5). Attach it to the connector (7a). Then, using a tensile tester, move the crosshead,
Pull the test piece (5) with the pull rod (3) and measure the mechanical properties. Pull rod (3) is connected via bellows (9)
Since it is connected to (7a), a mechanical test can be performed from the outside of the vacuum vessel (2) while maintaining a complex environment.
After degrading the test piece (5) under certain required environmental conditions, the test piece mounting member (1
The reason why the (0) is rotated and attached to the connecting tool (7a) is to reduce heat loss due to heat conduction from the heated or cooled test piece (5) through the test piece fixing tool (6a).
試験片(5)が破断すると試験片(5)の上半分は試験片装着
部材(10)の上側蓄熱体(11)に吊り下がる形で残り,試験
片(5)の下半分は試験片装着部材(10)の下側蓄熱体(11)
に乗つた形で残る。機械特性の測定データは同時に機械
特性データ処理装置(図示せず)により処理,記録さ
れ,最初の試験片(5)の測定が終了する。そこで遠隔操
作によつて駆動モータ(16)により駆動軸(13)を駆動し,
試験片装着部材(10)を回転させ試験片(5)を連結具(7a)
に装着すると次の試験を行うことができる状態となる。
この操作を繰り返すことによつて,真空容器(2)内を一
度要求環境条件にした後では,その条件下で連続して4
個の試験片(5)の測定を行う事が出来る。When the test piece (5) breaks, the upper half of the test piece (5) remains suspended from the upper heat storage body (11) of the test piece mounting member (10), and the lower half of the test piece (5) is mounted on the test piece. Lower heat storage body (11) of member (10)
It remains in the form of riding. At the same time, the measurement data of the mechanical characteristics is processed and recorded by the mechanical characteristics data processing device (not shown), and the measurement of the first test piece (5) is completed. Therefore, the drive shaft (13) is driven by the drive motor (16) by remote control,
Rotate the test piece mounting member (10) to connect the test piece (5) to the connecting tool (7a)
When it is attached to, the next test can be performed.
By repeating this operation, once the inside of the vacuum vessel (2) has been set to the required environmental conditions, it is possible to continuously perform 4
It is possible to measure individual test pieces (5).
なお,前述した実施例においては,試験片(5)を要求環
境条件下で劣化させた後,試験片装着部材(10)を回転さ
せて試験片(5)を連結具(7a)に装着し機械的特性の測定
を行うと述べたが,予め,試験片(5)を連結具(7a)に装
着した状態にしておき,加熱,冷却,紫外線照射,放射
線照射等を行いつつ機械的特性の測定が実施できること
は言うまでもない。In the above-mentioned embodiment, after the test piece (5) was deteriorated under the required environmental conditions, the test piece mounting member (10) was rotated to mount the test piece (5) on the connector (7a). Although it was stated that the mechanical characteristics were measured, the test piece (5) was attached to the connecting tool (7a) in advance, and the mechanical characteristics of the mechanical characteristics were measured while heating, cooling, UV irradiation, and radiation irradiation were performed. It goes without saying that the measurement can be performed.
更に,試験片装着部材(10)に装着する試験片(5)の個数
は4個とした構成について述べたが真空容器(2)内に設
けることのできる範囲であれば4個に限定されるもので
ない事も言うまでもない。Further, the number of test pieces (5) to be attached to the test piece attachment member (10) is described as four, but it is limited to four as long as it can be provided in the vacuum container (2). It goes without saying that it is not a thing.
また、第1図においては機械特性測定の試験は引張試験
の図について記したが,試験治具を考慮すれば圧縮試
験,曲げ試験等についても同様の効果を奏することは容
易に推定できよう。Further, in FIG. 1, the mechanical characteristic test is described by referring to the drawing of tensile test, but it can be easily estimated that the same effect can be obtained in compression test, bending test, etc. if the test jig is taken into consideration.
更に,試験片装着部材(10)を駆動する駆動軸(13)は駆動
モータ(16)により駆動する構成について述べたが,マグ
ネツト等を用いた駆動機構を用いても同様の効果を奏す
る。Further, although the drive shaft (13) for driving the test piece mounting member (10) is driven by the drive motor (16), the same effect can be obtained by using a drive mechanism using a magnet or the like.
また,試験片装着部材(10)に取付ける試験片固定具(6a)
の取付け位置は,試験片固定具(6a)の公転軌道上に,プ
ルロツド(3),固定ロツド(4)の中心線が来るように構成
されたものについて述べたが,第2図(a)のこの発明の
一部分の試験片装着装置の他の実施例を表わす構成図に
示すように試験片固定具(6a)の取付け中心円が小さく配
置されていて,連結具(7a)に装着する時にアーム(24)に
より,試験片(5)及び試験片固定具(6a)を平行移動させ
て連結具(7a)に装着する機構を備えても同様の効果を奏
する。第2図(b)は第2図(a)における連結具(7a)及び継
ぎロツド(8)のA−A断面図である。Also, a test piece fixture (6a) attached to the test piece mounting member (10).
As for the mounting position of the test piece fixture (6a), the pull rod (3) and the fixed rod (4) were arranged so that their center lines were on the orbit of the test piece fixture (6a). As shown in the block diagram of another embodiment of the test piece attaching device of the present invention, the test piece fixing tool (6a) has a small mounting center circle and is attached to the connecting tool (7a). The same effect can be obtained even if the arm (24) is provided with a mechanism for moving the test piece (5) and the test piece fixture (6a) in parallel and attaching them to the connecting tool (7a). FIG. 2 (b) is a sectional view of the connector (7a) and the connecting rod (8) taken along the line AA in FIG. 2 (a).
以上のように,この発明によれば,真空排気装置を有す
る真空容器,この真空容器内に複数の試験片固定具を介
して保持される複数の試験片,上記試験片固定具および
試験片のうちの少なくとも一方と接触する蓄熱体,この
蓄熱体と摺接し上記試験片を加熱・冷却するヒートシン
ク,上記試験片に放射線を照射する放射線照射装置,上
記試験片に紫外線を照射する紫外線照射装置,ベローズ
を介して上記真空容器内を貫通するロツドを有し上記試
験片の機械特性を試験する機械特性試験機,並びに上記
試料の化学的および物理的構造特性を測定する機器分析
装置を備え,取り付けた上記試験片固定具を移動させ,
上記試験片固定具を介して保持された試験片を上記ロツ
ドに取り付けられた連結具に順次装脱着して試験に供す
る試験片装着装置の試験片装着装置を設けることによ
り,複合環境下で複数個の試験片の機械特性の測定を連
続して同一環境条件において試験が出来ることから,デ
ータのバラツキを少なくすることができデータの信頼性
を向上できる複合環境試験装置が得られる効果がある。
更に,真空容器内を一度要求環境条件にした後では,連
続して複数個の試験片の測定を行う事が出来ることか
ら,試験時間を大きく短縮する事が出来,試験コストを
著しく低減できるという効果を得ることが出来る。さら
に,ヒートシンクにより,急激でしかも温度差の大きな
加熱・冷却が可能となる。As described above, according to the present invention, a vacuum container having an evacuation device, a plurality of test pieces held in the vacuum container via a plurality of test piece fixtures, the test piece fixture and the test piece A heat storage body that is in contact with at least one of them, a heat sink that is in contact with the heat storage body to heat and cool the test piece, a radiation irradiation device that irradiates the test piece with radiation, an ultraviolet irradiation device that irradiates the test piece with ultraviolet rays, A mechanical property tester having a rod penetrating the inside of the vacuum container via a bellows for testing the mechanical properties of the test piece, and an instrumental analyzer for measuring the chemical and physical structural properties of the sample, Move the above test piece fixture,
Multiple test pieces can be installed in a complex environment by installing a test piece mounting device that sequentially mounts and unmounts the test piece held via the test piece fixing device on the connecting tool attached to the rod and provides the test. Since the mechanical characteristics of individual test pieces can be continuously measured under the same environmental conditions, there is an effect that a compound environmental test device can be obtained which can reduce the variation of data and improve the reliability of data.
Furthermore, once the inside of the vacuum container has been set to the required environmental conditions, it is possible to continuously measure multiple test pieces, which can significantly reduce the test time and significantly reduce the test cost. You can get the effect. Furthermore, the heat sink enables rapid heating and cooling with a large temperature difference.
第1図(A)はこの発明の複合環境試験装置の一部分の試
験片装着装置の一実施例を示す断面構成図,第1図(B)
は第1図(A)のI−I断面図,第2図はこの発明の一部
分の試験片装着装置の他の実施例を示す構成図,第3図
は従来の複合環境試験装置の断面構成図である。 図において,(1)は複合環境試験装置,(2)は真空容器,
(3)はプルロツド,(4)は固定ロツド,(5)は試験片,(6
a)(6b)は試験片固定具,(7a)(7b)は連結具,(8)は継ぎ
ロツド,(9)はベローズ,(10)は試験片装着部材,(11)
は蓄熱体,(12)はバネ,(13)は駆動軸,(14)は位置決め
機構,(15)はシール部,(16)は駆動モータ,(17)はヒー
トシンク,(18)はヒートシンク加熱系,(19)はヒートシ
ンク冷却系,(20)は断熱軸受,(21)はシユラウド,(22)
は架台,(23)は外部機器接続ポート,(23-1)は真空排気
装置,(23-2)は紫外線照射装置,(23-3)は放射線照射装
置,(23-4)は機器分析装置,(24)はアーム,(25)は環境
試験装置,(26)は引張試験機,(27)は恒温箱,(28)は
窓,(29)はピン,(30)は熱風供給風路,(32)は熱風戻り
風路,(33)は空気加熱供給装置である。 なお,蓄熱体(11),ヒートシンク(17),ヒートシンク加
熱系(18),及びヒートシンク冷却系(19)から加熱・冷却
手段が構成され,試験片装着部材(10),駆動軸(13),位
置決め機構(14)及び駆動モータ(16)さらにはアーム(24)
から試験片装着装置が構成される。 なお,図中,同一符号は同一又は相当部分を示す。FIG. 1 (A) is a cross-sectional configuration diagram showing an embodiment of a test piece mounting apparatus which is a part of the composite environment test apparatus of the present invention, and FIG. 1 (B).
Is a sectional view taken along the line II of FIG. 1 (A), FIG. 2 is a block diagram showing another embodiment of a test piece mounting apparatus of a part of the present invention, and FIG. 3 is a sectional configuration of a conventional composite environment test apparatus. It is a figure. In the figure, (1) is a compound environment tester, (2) is a vacuum container,
(3) is a pull rod, (4) is a fixed rod, (5) is a test piece, (6
a) (6b) is a test piece fixture, (7a) (7b) is a connecting tool, (8) is a connecting rod, (9) is a bellows, (10) is a test piece mounting member, (11)
Is a heat storage body, (12) is a spring, (13) is a drive shaft, (14) is a positioning mechanism, (15) is a seal part, (16) is a drive motor, (17) is a heat sink, and (18) is a heat sink heating. System, (19) heat sink cooling system, (20) adiabatic bearing, (21) shroud, (22)
Is a stand, (23) is an external device connection port, (23-1) is a vacuum exhaust device, (23-2) is an ultraviolet irradiation device, (23-3) is a radiation irradiation device, and (23-4) is a device analysis. Device, (24) arm, (25) environmental test device, (26) tensile tester, (27) constant temperature box, (28) window, (29) pin, (30) hot air supply air The air passage, (32) is a hot air return air passage, and (33) is an air heating supply device. The heat storage body (11), the heat sink (17), the heat sink heating system (18), and the heat sink cooling system (19) constitute heating and cooling means, and the test piece mounting member (10), drive shaft (13), Positioning mechanism (14), drive motor (16) and arm (24)
The test piece mounting device is composed of In the drawings, the same reference numerals indicate the same or corresponding parts.
───────────────────────────────────────────────────── フロントページの続き (56)参考文献 特開 昭59−3240(JP,A) 特開 昭49−17793(JP,A) 特開 昭56−19433(JP,A) 実開 昭57−72146(JP,U) 鶴 宏「人工衛星」(昭58−4−10)工 学図書 P.255−269 ─────────────────────────────────────────────────── ─── Continuation of the front page (56) References JP 59-3240 (JP, A) JP 49-17793 (JP, A) JP 56-19433 (JP, A) Actual development Sho 57- 72146 (JP, U) Hiroshi Tsuru "Artificial Satellite" (SHO58-4-10) Engineering Book P. 255-269
Claims (1)
容器内に複数の試験片固定具を介して保持される複数の
試験片,上記試験片固定具および試験片のうちの少なく
とも一方と接触する蓄熱体,この蓄熱体と摺接し上記試
験片を加熱・冷却するヒートシンク,上記試験片に放射
線を照射する放射線照射装置,上記試験片に紫外線を照
射する紫外線照射装置,ベローズを介して上記真空容器
内を貫通するロッドを有し上記試験片の機械特性を試験
する機械特性試験機,並びに上記試験片の化学的および
物理的構造特性を測定する機器分析装置を備え,上記試
験片固定具を上記蓄熱体と共に移動させ,上記試験片固
定具を介して保持された試験片を上記ロッドに取り付け
られた連結具に順次装脱着して試験に供する試験片装着
装置を設けたことを特徴とする複合環境試験装置の試験
片装着装置。1. A vacuum container having an evacuation device, a plurality of test pieces held in the vacuum container via a plurality of test piece fixtures, and contact with at least one of the test piece fixtures and the test pieces. Heat storage body, a heat sink that heats and cools the test piece by sliding contact with the heat storage body, a radiation irradiation device that irradiates the test piece with radiation, an ultraviolet irradiation device that irradiates the test piece with ultraviolet rays, and the vacuum through a bellows. A mechanical property tester having a rod penetrating the inside of the container for testing the mechanical properties of the test piece, and an instrumental analysis device for measuring the chemical and physical structural properties of the test piece are provided. A test piece mounting device was provided for moving the heat storage body together with the heat storage body and sequentially attaching and detaching the test piece held through the test piece fixture to and from the connecting tool attached to the rod. Specimen mounting apparatus composite environment test apparatus characterized.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP60072536A JPH0627698B2 (en) | 1985-04-08 | 1985-04-08 | Specimen mounting device for compound environment test equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP60072536A JPH0627698B2 (en) | 1985-04-08 | 1985-04-08 | Specimen mounting device for compound environment test equipment |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS61233000A JPS61233000A (en) | 1986-10-17 |
| JPH0627698B2 true JPH0627698B2 (en) | 1994-04-13 |
Family
ID=13492170
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP60072536A Expired - Lifetime JPH0627698B2 (en) | 1985-04-08 | 1985-04-08 | Specimen mounting device for compound environment test equipment |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0627698B2 (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP6041417B2 (en) * | 2011-12-16 | 2016-12-07 | ユアサシステム機器株式会社 | Constant temperature test equipment |
| WO2025203367A1 (en) * | 2024-03-27 | 2025-10-02 | Ntt株式会社 | Deterioration acceleration apparatus |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS536871B2 (en) * | 1972-06-07 | 1978-03-11 | ||
| JPS5619433A (en) * | 1979-07-26 | 1981-02-24 | Ueshima Seisakusho:Kk | Full-auto continuous tensile tester |
| JPS5933849B2 (en) * | 1982-06-29 | 1984-08-18 | 株式会社島津製作所 | Atmosphere material testing equipment |
-
1985
- 1985-04-08 JP JP60072536A patent/JPH0627698B2/en not_active Expired - Lifetime
Non-Patent Citations (1)
| Title |
|---|
| 鶴宏「人工衛星」(昭58−4−10)工学図書P.255−269 |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS61233000A (en) | 1986-10-17 |
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| Date | Code | Title | Description |
|---|---|---|---|
| EXPY | Cancellation because of completion of term |