TH60970B - Cooling the test system of storage devices - Google Patents

Abstract

DC60 (25/09/60) The storage carrier, including the first and second body transport hulls, the first hulls are shaped so that they are coordinated by a mechanical mechanism. Automatic for moving Storage carrier The second fuselage has been made to accept and accommodate storage devices. The first fuselage is shaped to receive and direct air flow over one or more surfaces. Storage device surface supported in the second fuselage, revised Sept. 25, 2017. The storage device carrier includes the first and second fuselage hulls. It is made in appearance so that it is coordinated by an automatic mechanism for movement. Storage carrier The second fuselage has been made to accept and accommodate storage devices. The first fuselage is shaped to receive and direct air flow over one or more surfaces. The surface of the storage device is supported on the second fuselage. -------------------------------------------------- -------------------------------------------------- The storage device (800, 800 ', 1800) covers the transport body (810, 1810) with the first and second (802, 804, 1802, 1804) torso. The first (802,1802) is configured to work with the automation mechanism in the alignment of the storage carrier (800, 800 ', 1800), the second body (804, 1804). Designed to receive and support the trunk storage device, part one (802, 1802) is configured to receive and direct the airflow (305, 1950) over the surface of the supported storage device. In the second body, one or more surfaces.

Claims (6)

Disclaimer (all) which will not appear on the announcement page: Revised Sep 25, 2017 1. Transport carrier, including A) Carrier body containing i) Body part The first one is made in the appearance so that it is coordinated by a mechanical Automation for moving the transport, storage devices, and ii) a second body part that has been shaped to receive and accommodate the storage device. Where the first fuselage is shaped to receive and direct airflow over it. One or more storage surfaces supported in the second torso. -------------------------------------------------- -------------------------------------------------- 1.Storage carrier (800, 800 \ ', 1800), consisting of: a) carrier body (810, 1810), including: i) part body (802, 1802). That is configured in order to be captured Mechanically to transport the transport, storage device; And ii) the second body part (804, 1804) that was configured to receive and support. A storage device, where one part of the body (802, 1802) is configured to receive and direct direction. The flow of air over one or more surfaces of the storage device is supported in the second trunk. 2. Carrier, the storage device of claim 1, where the first body part. (802, 1802) includes an air direction controller (830, 1830) with one or more air inlets (832a-c, 1832) to take air into the first section (802, 1802) and to direct the direction of the aircraft. Section 2 (804, 1804) 3. Carrier, storage device of Clause 2, where one or more air inlets (832a-c, 1832) are configured. In order to be clamped by an automatic mechanism to transport the conveyor. Storage device (800, 800 \ ', 1800) 4. Carrier, storage device of claim 1, where the second body part (804, 1804) is composed of a side wall, one wall and A second wall (822, 824, 1822, 1824) was set aside for Data storage device in the middle 5. Carrier Device Data acquisition device of claim 1, where the part one (804) consists of one or more vision fiducials (836). 6.The carrier, the storage device of claim 1, is equipped with a clamping mechanism (840, 1840) that can work to clamp the second part of the internal storage device (804, 1804). Claim 1's carrier storage device, where the first body part (802, 1802) is configured to direct the direction of air flowing over the upper and lower surfaces of the carrier. Storage device supported in the second trunk (804, 1804) 8. Carrier Device The storage device of claim 1, where the 1st part of the trunk (802) includes the air direction controller. (830) with one or more air inlets (832a-c) to take air into the first part of the fuselage (802) and direct the air to flow into the second part of the fuselage (804), And by which channel One or more air inlets (832a-c) are aligned with the collector conveyor in X, Y, and rotational directions when the collector conveyor is mechanically clamped. Claim 1's storage device, where the second body (804, 1804) determines the U-shaped opening significantly. Which allows air to flow over the bottom surface of Storage Device Supported in the Storage Carrier 1 0. Test Slot Assembly The attachment includes: a) the storage carrier (800, 800 \ ', 1800), including i) the transport body (810, 1810) that includes: a) the body part One (802, 1802) that is configured to be captured. With automatic mechanisms to move the transport, storage device; And b) the second body (804, 1804) that was configured to receive and support Storage device Where one part of the fuselage was configured to receive and direct the flow of Air goes over one or more surfaces of the storage device supported in the second body b) Test socket (330, 330 \ ', 1330), including: i) Housing (340, 1340) designated: a) test loom for receiving and supporting the storage carrier, and b) open end (346, 1346) that allows access to the test port for insertion and Retractable disk drive carrier 1 1. Test slot assembly of claim 10, where the storage carrier (800, 800 \ ', 1800) can be completely removed from the test compartment 1 2. Clause 10 test slot assembly, where the storage carrier (800 \ ') is connected to the test socket (330 \') in the manner forming the storage drawer 1 3. Storage testing system Which includes a) automatic mechanism; And b) the storage carrier (800,800 \ '1800) that consists of: i) the carrier body (810, 1802) comprising: a) the first part (802, 1802) Instead of configuring them in order to be captured Fastened mechanically to transport the body to a storage device; And b) the second body (804, 1804) that was configured to receive and support Storage device Where one part of the fuselage is configured to receive and direct the flow of Air above one or more surfaces of the storage device supported in the trunk. Part II 1. 4. Clause 13 of the storage device test system, where part one (802 ), As well as an air direction controller with one or more air inlets (832a-c) to get air into the Part one And direct the air to flow to the second part of the body, and by the air inlet One or more compartments are configured so that they are crimped by an automatic mechanism to the transport arms. Storage Device 1 5. Clause 14 of Clause 14 of the Test Storage Device, where the automatic mechanism includes Deployed mechanical actuator (240) holds one or more air inlets (832a-c) 1 6. Acquisition test system of Clause 13, where the trunk part one (802). It consists of one or more indications (836) and by which automatic mechanisms, including optical systems (212), are used to detect that indication. Of claim 13, where the automatic mechanism includes the anchor (244) and where the first body part includes one multiple air inlet (832a-c) for air intake. In the first part of the body And directing the air to flow into the second part of the body The air inlet (832c) is arranged so that it is clamped by the clamp to align the collector conveyor in the X, Y, and rotation directions when the collector conveyor is mechanically clamped. Automation 1 8. Clause 13 of the data acquisition device test system, where the body part one (802) includes a pair of channels (834) and where the automatic mechanism includes a pair of jaws (246a, 246b). That can work Clause 13 of Clause 13 of Clause 13 also includes a clamping mechanism (840, 1840) that can work to clamp the storage device inside the second body (804). , 1804), where the automatic mechanism can act to stimulate the clamping mechanism 2 0. The system of testing the data acquisition device of Clause 13, where the automatic mechanism consists of a robotic arm (200) and Manipulator (210) connected to the motor arm The transporter was Configured to hold the data storage device carrier (800, 800 \ ', 1800) 2 1. Storage test system (100) included: at least one rack ( 300); At least one test slot (330, 330 \ ',) enclosed by each rack, compartment Each test socket, consisting of a test socket enclosure (340) with inlet (346) and outlet (358), is configured to accept a storage device; And at least one evaporator (900) in the form of air contact welding to the socket Test at least one channel. Where at least one airliner is configured to move the air. At least one outside of the racks goes into the inlet of each test socket casing, over the receiving storage device, and exit through the outlet of each test socket casing. Test the storage device of claim 21 where each rack (300) consists of an air duct (304) connecting the test socket. At least one of them, at least one air duct that moves air through the house outlet. Cover each test socket through an air duct. And to the external environment of the rack 2 3. Clause 22 clause 22 storage device testing system where the outlet of the enclosure is Each test plug of every rack is in a pneumatic connection with at least one of the air supplants. ) Are arranged on each shelf (300) in a pneumatic connection with the slots (330) of the respective racks. 2. 5. The storage device test system of Clause 21, where the slot covers Each test (340) has a part one and a second (342, 344), part one (342) of the test socket housing. The inlet (346) is designed and configured to accept the storage device, at least one air evacuation device (900) is in a pneumatic connection to the second (344) of the casing. Test socket 2 6. Storage test system of Clause 25, where the evacuation device (900) includes the air inlet (902) and the air outlet (906), the air emitter that receives the air in the direction specified by One (904) through its air inlet. 2 7. The data acquisition test system of Clause 21, where the inlet is significantly perpendicular to the first direction (908). Of the test compartment casing (346), it is designed to accept the storage carrier transport (800, 800 \ '), the storage device carrier (800,800 \') with the first and the second. , Part one (802) of the carrier Storage devices That includes the air direction controller (830), the second part (804) of the storage conveyor is configured to accept a data acquisition device, a directional air direction controller. Most of the air at the same time flows above, at least the top and bottom of the collection device. Data Received in the Storage Carrier 2 8. Storage Test System of Clause 27, where outside air the rack is Moved into the air direction controller of the receiver carrier, the receiving device into the test socket at Related to the receiving storage device And out through the outlet of the relevant test socket By using at least one of the air movers 2 9. Storage testing system of claim 27, where the air direction controller (830) of the receiving collector carrier (800, 800 \ ') Is defined as one or more air inlets (832a-c), storage devices with top, bottom, front, back, right and left surfaces, front surface of the storage device. With the electrode, the storage device is taken by the back surface. Of the device is significantly facing the part of the storage carrier. Where the air inlet At least one (832a-c) water chamber that controls the air to at least the upper and lower surfaces. Bottom of the receiving storage device 3 0. Storage Test System (100) that includes: at least one rack (300); Air heat exchanger (350) in rack-mounted air contact. At least one floor; And test slots (330,330 \ ') that are enclosed by individual racks, each test socket Composed compartment: Test slot enclosure (340) that defines the inlet (346) and the outlet (348, the inlet is configured to accept the storage device, the inlet and the channel. solution At least one of the chambers is air-welded to the air heat exchanger; And the air motor (900) of the test socket was arranged in a pneumatic contact welding. With test socket housing And was configured to move air into the inlet of the house Cover the test socket, over the receiving storage device, and exit through the test socket cover; Where the air outside the rack is moved into the inlet of the test socket enclosure, over the receiving storage device, via the air motive of the relevant test slot and traveled out through the enclosure outlet. Related slots And off the floor Placed involved, the air is moved through at least outward through the air heat exchanger One of the before and after that passes over the retained storage device 3 1. The storage device test system of Clause 30, where each loop layer (300) is composed of an air duct (304). That causes a connection between each outlet of the house Cover the test socket (340) with the air heat exchanger (350) 3 2. Data acquisition test system of Clause 30 where the air heat exchanger (350) consists of: Of the air (352) that defines the inlet (351), the outlet (353), and the air flow path (304) between them; The cooling section (354) is arranged in the air flow path; And at least one pump (356) and a vent hose to deliver the condensed steam that has accumulated from the Air heat exchanger 3. Air heat exchanger 3 3. Storage test system of Clause 32 where the air heat exchanger (350) also contains the air movers (358) of the air heat exchanger. To move air into the inlet of the housing, cover the air heat exchanger. (Above the heat exchanger and exits through the outlet of the air heat exchanger housing) 3 4. The storage test system of Clause 32, where the air heat exchanger (350) is also joined together. With the evaporator (360), which is placed on the respective shelf. Of air heat exchanger And is in the process of connecting the fluid to at least one pump body (356) and drain hose 3. 5. Test storage device of Clause 30 at the inlet of the test plug housing (346). Configured to accept the storage carrier (800,800 \ '), the storage carrier has a first and second (802, 804), part one (802) of the transport Storage devices This includes the air direction control unit (830), the second part (804) f of the collector carrier. Data that is configured to receive a data acquisition device, air direction controller. Directional Most of the air, at the same time, flows above at least the top and bottom surfaces of the collection device. Data received in the storage carrier 3 6. Storage testing system of claim 35, where air outside the rack (300) is moved into the air direction controller (830) of the collection conveyor. Data (800, 800 \ ') received in the relevant test socket (330, 300 \') over the received data acquisition device by means of air movement (900) of the relevant test socket. And moved out through the exit (348) of the test socket. Through the air heat exchanger (350) and out of the associated racks 3 7. Storage test system of Clause 35, whereby the air direction controller (830) of the collector carrier is Received (800,800 \ ') designates one or more air inlets (832a-c), storage devices with top, bottom, front, back, right and left surfaces, device front surface. Collect data With the power connector, the storage device is taken by the back surface. Of that device is significantly facing the part of the storage carrier. Where the air inlet At least one vent is controlled above at least the top and bottom surfaces of the device. Retain the obtained data. 3 8. Clause 30 of Clause 30 Data Acquisition Device Testing System, where the evacuation device (900) includes the air inlet (902) and the air outlet (906), the air emitter to the air. Follow the first direction (904) through its air inlet and deliver air through the second directional air outlet (908) in a way that is significantly perpendicular to the first direction. Clause 38, where the air emitter (900) consists of a body of an emulator approximately 45 mm wide, approximately 45 mm long and approximately 10 mm high. Article 30 storage device testing system, which also includes a motor arm. At least one arm (200) that is directed to the first axis (205) that is significantly perpendicular to the surface of the floor, a motor arm that can be operated to rotate along a predetermined arc around that axis. one And extended accordingly Radial from the first axis, a rack arranged around the motor arm to be serviced by the motor arm 4 1. Method of temperature control of the data acquisition device received in the storage test system, the method included. : The flow of air flow (305) into the air inlet (346) of the test socket housing (340) of the test socket (330, 330 \ ') received in the rack (300); The flow of air flow (305) over the data acquisition device (500) is placed in the test socket; Air out through the air outlet (348) of the test socket housing of the test socket; 4. 2. The method of claim 41 that also consists of moving most of the air flow (305) in the same time over at least the top surface. And below (512, 514) of the storage device. Data received in the test socket (330, 330 \ ') 4 3. Clause 41 Clause 41 Methodology also includes The movement of air outside the rack (300) into the inlet of the test socket enclosure (346), to the receiving storage device; And airflow from the housing outlet of the test compartment (348) through the air duct (304) and out of the rack (300); Where the air ducts (304) are in the air contact with the outlet holes (348) of each test socket casing of the phases 4 4. Method of Clause 43 is also included. Air exertion through test slots (330,330 \ ') and air ducts (304) by means of an air carrier connected by air to an air duct 4 5. Method of Clause 43 also included. Air movement through the test slot (330,330 \ ') using the exam compartment air movers (900) and into the air ducts (304) to be exported from the rack (300) 4 6. Method of Article Holds Article 41, incorporating airflow outside the rack (300) into the inlet of the test enclosure (346), over the retrieval device, by the air evacuation device. Test socket (900) of the test port, and air travel from the outlet port. Of the test chamber housing (348) through the air heat exchanger (350) 4 7. Method of claim 46, where air is diverted from the outlet of the test chamber housing (348) to the The air heat exchanger (350) consists of air movement through an air duct (304) in a pneumatic connection with the outlet of the test socket housing (348) of each test socket (330,330 \ ') Of the rack and air heat exchanger (350) 4 8. Method of claim 46 that also includes the movement of air through the exchanger. Air heating (350) using the air emitter (358) of the air heat exchanger, the evaporator's evaporator heats the air, which moves air from the air ducts into channel 6 3. Cooling system. Hot test socket of claim 61. Wind to the air inlet (1326) of the test socket housing, air motor (1930) arranged in the casing. Cooling system (1900) and recirculation of the air received through the air inlet (1914) of the enclosure, cooling system out through the air outlet of the cooling housing (1912), moving air. Following a closed loop path through the test socket housing (1340) and the cooling housing (1900), it is configured to produce an air flow rate of approximately 0.122 m 3 / min (4.308 CFM). ) And air pressure up to approximately 20.88 mm water (0.822 in. Water) 6 4. Cooling system Test socket of Clause 54 that also includes an air cooler (1920 ) In the form of a pneumatic connection with an air duct (1930), an air cooler consisting of a fuselage, an air cooler (1922), and at least one fin (1924) arranged on Aircooler body, at least one fin that cools the air flowing above it 6 5. Cooling System Test socket of Clause 64 where Air cooler (1920) Cut into the cooling housing at the source side of the evaporator (1930), Air flow between the test socket casing and the cooling housing in a closed loop path. 6 6. Cooling system Test socket for test venting system Storage device, Cooling system Test socket That includes: a test socket enclosure (1340) to determine the air inlet (1326) and an instrument dash opening (1346) to receive a storage device; Air motive (1930) provided outside the test compartment housing (1340) and in a pneumatic connection with the air inlet (1326) of the test compartment housing (1340) to deliver air to Retained storage device; Where the air movers (1930) include the air inlet (1932) and the air outlet (1936), the air outlet (1936) in a pneumatic connection with the air inlet (1326) of the socket housing. Test (1340), an air carrier that takes air in the first direction (1934), passes through the air inlet (1932) and delivers air out of its air outlet (1936) in its second direction (1938) in an upright manner. Significant perpendicular to the first direction 6 7. Cooling system Test sockets of claim 66, consisting of a casing. Supplied cooling system (1900) adjacent to test mash housing (1340), system housing Cooling vent (1900) with air inlet (1914) located in pneumatic contact welding with air outlet (1348) of test socket housing (1340) and air outlet (1912) in appearance. 6 8. Cooling system Test socket of claim 66, where the air evacuation (1930) consists of an air body with a width of 45 mm. Approx. 45 mm long and approximately 10 mm high. 6 9. Cooling System Test socket of claim 66, where the air mounts (1930) are configured to produce the air flow rate. Air flow up to approximately 0.122 m 3 / min (4.308 CFM) and air pressure up to approximately 20.88 mm water (0.822 in. Water) 7 0. Cooling system, test socket of claim 66, assembled. Includes an air cooler (1920) located in the air-contact connection with an air duct, an air cooler that includes an air cooler (1922) and at least one fin ( 1924) that was arranged on the fuselage, air cooler, at least fins. One that cools the air flowing through the top. 7 1. Data collector carrier (800,800 \ ', 1800) for the storage test system. The storage device carrier (800, 800 \ ', 1800) that consists of: trunk (810, 1810) with first and second (802, 804, 1802, 1804), part body. The first (802, 1802) that includes the air direction controller (830, 1830), the second fuselage (804, 1804) is configured to receive a top-surface storage device. Lower, front, back, right and left side, the data storage device is retained with the rear surface of the device significantly facing the first body part; Where the air direction controller (830, 1830) receives the air flow and controls its direction. Most of the air flow at the same time goes to at least the top and bottom surfaces of the Receiving storage device 7. 2. Storage carrier of claim 71, where the air direction controller (1830) includes the air inlet (1832) and the first and second air outlet. (1834, 1835), air direction controller (1830) that directs the received air through the air inlet (1832) to the air outlet. The first and second compartment (1834, 1835), the first air outlet (1834) that controls the air above the Less, the bottom surface of the storage device is being picked up. And a second air outlet (1835) that directs the air above at least the top surface of the receiving storage device. 7 3. The collector carrier of Clause 71, where the air direction controller (1830) is a defibrillator (1831) that is in the way of connecting the wind connector to the morning air intake (832) and the air outlet (1834, 1835), the air direction controller (1830) that is assembled with the air box. That's right It is supplied in the cavitation (1831), the air box (1836) that controls at least part of the intake air in the cavity (1831) to flow out through the first ventilator (1834). The storage device of Clause 73, where the air box (1836) is assembled with a weighted mass to reduce the displacement of the storage carrier (1800) while being picked up by the device test system. Storage 7 5. The storage carrier of claim 71, where the second body (804, 1804) is equipped with a clamping system (840, 1840) to hold the stored storage device. 7 6. Method for controlling the temperature of the data storage device (500) obtained in the test system, the data acquisition device (100), the methods included: Air (305, 1950) into the air inlet (346, 1326) of the test compartment housing (340, 1340); And control of the air flow direction (305, 1950), mostly at the same time going north. At least the top and bottom surfaces (512,514) of the storage device (500). 7 7. Method of Clause 76 that also includes delivering air flow (305, 1950) to Air direction controller (930, 1930) that will direct the airflow direction above at least the upper and lower surfaces (512,514) of the storage device (500). 7 8. Method of claim. Article 77 also includes support for the storage device (500) in the storage carrier. (800,800 \ ', 1800) received in the test compartment enclosure (340, 1340), the storage carrier (800,800 \', 1800) with the first and second parts (802, 804, 1802. , 1804), part one (802, 1802) that includes air direction controllers (830, 1830), second part (804, 1804) that are configured to accept storage devices (500). Storage device With the top, bottom, front, back, right and left surfaces (512,514,516,518,520,522) and are taken with the back surface (518) of the device facing the part (802, 1802) ) Significantly 7 9. Clause 78's method also incorporates air direction controller weighting (1830) to reduce the body movement of the storage device (1800) while Accepted by the system Test storage device 8 0. Clause 77 method of claim also includes delivering air flow (1950) to air inlet (1832) of air direction controller (1830), body. Air direction (1830) to direct the direction of the received air through the air inlet (1832) through the first air outlet. And the second outlet (1834, 1835) of the air direction controller (1830), the first air outlet (1834) that directs the air to at least the lower surface (514) of the collector being The receiver (500), and the second air outlet (1835) that directs the air above at least the top surface (512) of the receiving storage device. 1. Method of claim 90, where the air direction controller (1830) determines the cavitation (1831) located in the air contact with the air inlet (1832) and the air outlet (1834). , 1835) of the air direction controller (1830), the air direction controller (1830) consisting of the air box (1836) arranged in the air cavity (1831), the air damper (1836) that controls at least part Of the intake air in the cavity (1831) to the first air outlet (1834) 8 2. The method of claim 76 that also includes an air damping weight (1836) to reduce the movement of the storage wand (1800) while being retained by the retention system. Data 8 3. The method of claim 76 that also includes directivity of air flow (1950) to the evacuation device (1930) in a pneumatic connection with the air inlet (1326) of the house. Test chamber cover (1340), air motive (1930) that directs air flow (1950) into the air inlet (1326) of the test socket housing (1340), the air flow at Move along a closed loop path 8. 4. Procedures of Clause 86 that include a glove. Receiving air flow (1950) into the air motive (1930) in the first direction (1934) and air flow delivery (1950) to the air inlet (1326) of the test compartment housing (1340). ) Follow the second direction (1938) in the position which is significantly perpendicular to the first direction (1934). 5. Method for Clause 83 also includes directing the air flow (1950) over the air cooler (1920), which is arranged in the path of the air flow. (1950) on the side Origin of air movers (1930) 8 6. The method of claim Article 76 also includes the delivery of air flow (1950) into the air inlet (1326) of the socket housing (1340) with the air flow rate up to approx. 0.122 m 3 / min (4.308 CFM) and air pressure up to approx 20.88 mm water (0.822 in water).