序号 专利名 申请号 申请日 公开(公告)号 公开(公告)日 发明人
81 Method of determining overspeed reliability US12485218 2009-06-16 US08042406B2 2011-10-25 Ron Harvey Rosenfield; Shiv C. Gupta
A method and system for determining the reliability of a rotating component compares a normalized stress curve with a normalized strength curve. The resulting overlap corresponds with the reliability of the rotating component.
82 Apparatus and methods for testing containers US11264569 2005-10-31 US20060090577A1 2006-05-04 Aaron Bates; Frank Middleton
An apparatus automatically tests the effect of pendular motion on the integrity of cartons or other containers having handles, by grasping the handles with a simulated hand connected to a simulated arm, which swings the carton along an arcuate path according to a predefined test protocol. A first test protocol simulates removal of the carton from an elevated shelf. A second test protocol simulates the oscillating motion of a human carrying a carton by its handle. A third test protocol simulates a human swinging the carton upward to an elevated shelf. The simulated hand may be connected to the simulated arm by a simulated wrist that allows articulation of the hand during the test, thereby more closely approximating handling of the carton by a human user. The simulated arm may be caused to pivot or oscillated by the force of gravity and alternatively, by a mechanical or electromechanical drive system.
83 Method and apparatus for recording changes associated with acceleration of a structure US10305171 2002-11-27 US06909985B2 2005-06-21 James M. Stana
The present invention is directed to recording changes associated with the acceleration of a structure. An exemplary embodiment includes an accelerometer array having at least one silicon beam type accelerometer, a nonvolatile memory, a clock timer, a programmable control unit operatively coupled to the accelerometer array, at least one non-volatile memory, and clock timer. The accelerometer array, the at least one non-volatile memory, the clock timer and the programmable control unit can be formed on a common semiconductor substrate (e.g., integrated), with the accelerometer array disposed in a central region.
84 High-speed rotation testing apparatus US10067396 2002-02-07 US06615670B2 2003-09-09 Koji Shibasaki; Takeshi Watabe; Shiro Shibasaki
A high-speed rotation testing apparatus includes a spindle 11 holding a test object S at its lower end, a driving motor 20 for applying torque to the spindle 11, and a frame 30 for supporting a rotor shaft 21 of the driving motor 20 so that the shaft is arranged toward the vertical direction of the apparatus, wherein the spindle 11 is driven directly by a driving motor 20 by inserting the spindle 11 into a through-hole 21a that penetrates the center of the rotor shaft 21 and coupling the upper ends of the rotor shaft 21 and the spindle 11 together, and the through-hole 21a has an inner diameter set so as to form a clearance in which the lower end of the spindle can swing, and further, a damping mechanism 40 that restrains swing is arranged in the vicinity of the lower end of the spindle 11, which projects from the lower end of the rotor shaft 21.
85 Centrifuge model test apparatus US794230 1997-01-30 US5767381A 1998-06-16 Takao Konno; Masaharu Sugano; Yuji Tadano
A centrifuge model test apparatus is accommodated in a pit, and comprises a vertical rotary shaft, a rotary arm horizontally secured to the rotary shaft, a swing bucket suspended from and supported at a pin on the rotary arm and located near the end thereof so as to be movable in the radial direction of the rotary arm or fixed, and a drive unit for rotating the rotary shaft. As the drive unit is driven and the rotational speed of the rotary shaft increases, the swing bucket is raised together with a sample contained therein due to the centrifugal force with the pin as a center and is placed at a nearly horizontal position when a predetermined rotational speed is reached. A partitioning plate provided under the swing bucket is moved upwards at the time when the swing bucket is raised, and the volume and surface area of the space defined by the partitioning plate and the pit reduce, and the frictional force due to the resistance of the air decreases. This makes it possible to increase the radius of the rotary arm or the load weight on the sample without increasing the driving force. As the rotary arm is made of high damping and easily welded material, vibration caused by resonance can be reduced when the testing apparatus of the centrifuge model is operated with a vibration generating device installed in the testing apparatus.
86 Test rig for rotors of gyrocraft US613998 1996-03-11 US5693896A 1997-12-02 Lucien Henri Baptiste Mistral; Gerard Donat Chabassieu
The rig comprises a vertical electric motor in a shell-type framework carrying a force balance itself supporting either a main rotor in dynamic tests or a complete propulsion assembly with main rotor in endurance tests, or a height extender supporting, on the one hand, an upper shaft line being coupled to a lower shaft line supported in the framework and driven by the motor and, on the other hand, an inverse-thrust rotor mast, driving a hub jig linked to blades mounted inverted so as to exercise a thrust downwards. The mast is linked to the shaft line by a torque meter and is mounted rotating in a bearing supported by a second balance fixed to the height extender. The mast and the upper shaft line are removable with the height extender in order to make the rig multi-purpose and useable for performance, endurance and dynamic tests of helicopter rotors.
87 Test device for equipment in motion US786839 1991-11-01 US5251497A 1993-10-12 Elie Bressan
A test apparatus for testing equipment in motion comprises a test device (1) for testing a piece of equipment (2) and a mobile enclosure (3) containing a gas lighter than air and surrounding the test equipment (2) located on the test device (1).
88 Tubular shaped sled test complex US718033 1985-03-29 US4599897A 1986-07-15 Joe S. Hunter
A sled test facility employing a tubular shaped track for testing missile d aircraft guidance and control systems. A blockhouse is at one end of the track and a recovery station at the other end. A compressor in the blockhouse and recovery station controls the g-profile of the sled as the sled moves in a cushion of air in the tubular track. Instrumentation and controls are provided in the blockhouse and recovering station.
89 Environmental rate of turntable US3487638D 1966-09-13 US3487638A 1970-01-06 ISLEY LOREN D; WIGGIN WILLIAM R; OSGOOD WINTHROP B JR
90 Acceleration control platform US3466932D 1967-09-15 US3466932A 1969-09-16 SCHULMAN MARVIN
91 Device for taking and recording the performance data of a running motor vehicle US19009762 1962-04-25 US3160463A 1964-12-08 FLAVIANO MOSCARINI
92 Motor operated latch mechanism US41733954 1954-03-19 US2949889A 1960-08-23 IVANKOVICS STEPHEN G; MIKEL GAROLD R
93 寿命判定装置及び寿命判定方法 JP2016017673 2016-02-02 JP2017138136A 2017-08-10 永島 拓也; 多木 良孝
【課題】演算負荷を抑制して寿命判定を行うことができる寿命判定装置を提供する。
【解決手段】寿命判定装置1は、所定時間毎に、ストレス因子についての計測値を取得する計測値取得部2と、第1の寿命に対する第2の寿命である第1の加速係数を、所定時間毎に取得する加速係数取得部3と、第1の加速係数の累積値及び所定時間の乗算値と、第2の寿命とを比較することにより寿命判定対象の装置の寿命の到来を判定する寿命判定部5とを有する。加速係数取得部3は、第1の加速係数の取得に際し、第2の加速係数を、所定値毎に格納したルックアップテーブル4を用いる。
【選択図】図1
94 Test board and method for determining latent failed state JP2012068888 2012-03-26 JP2012215573A 2012-11-08 MICHAEL GICKELEITER; THOMAS KRAMER; CHRISTIAN EIFRIG
PROBLEM TO BE SOLVED: To provide a test board and a method for determining latent failed states.SOLUTION: This invention is concerned with the test board and the method for determining latent failed states of a drive mechanism having an automatic operation unit (2). The automatic operation unit (2) is capable of moving a container (5) by previously defined operation sequence and extracting a liquid medium from the container (5) during a test process in accordance with a request, and extraction following the request is embodied by an adjustment device (6) for conveying the liquid medium in accordance with previously defined condition.
95 Inspection method of through-hole structure of the member JP2004552454 2003-09-12 JP2006518032A 2006-08-03 バイヤー、ロマーン
従来技術による部材の貫通孔の検査方法は一般にサーモグラフによる詰まり検出に高温ガスを使用する。 本発明による部材(10)の貫通孔構造の検査方法によれば、これは、カメラ(13)の波長範囲に少なくとも1つの吸収端を有する媒体が使用され、この媒体がカメラ画像(13)において不透明にて現われるようにすることによって簡単化される。
96 High-speed rotation testing apparatus JP2001041694 2001-02-19 JP3488696B2 2004-01-19 司郎 柴▲崎▼; 康司 柴▲崎▼; 岳史 渡部
97 Test equipment and improvements on the test method JP51678494 1994-01-19 JP3350788B2 2002-11-25 アンドリュー ノエル ショフィールド
98 Centrifugal force loading test equipment JP1499696 1996-01-31 JP3314603B2 2002-08-12 隆雄 今野; 正治 菅野
99 Centrifugal load tester JP1499696 1996-01-31 JPH09210871A 1997-08-15 KONNO TAKAO; SUGANO MASAHARU
PROBLEM TO BE SOLVED: To enlarge a rotary arm by making the space, defined by the rotary arm and a lower disc, narrower as an oscillatory frame ascends through increase of r.p.m. of the rotary arm until a predetermined r.p.m. is reached. SOLUTION: A driving force is transmitted from a driver 1 through a bevel shaft 3 and a transmission 2 to a rotary shaft 4 which then turns a rotary arm 6. When a centrifugal force is applied to an oscillatory frame 7 through rotation of the rotary arm 6, a sample case 9 ascends in proportion to increase in the r.p.m. of rotary arm 6 around a pin fulcrum 8 and a centrifugal acceleration is applied in the circumferential direction to the base of the case 9. Air in a pit 10 turns as the rotary arm 6 turns to produce windage loss resistance. A lower disc 10b is supported by a plurality of servo jacks 12 and lifted through the jack 12 such that the lower space of rotary arm 6 is made narrower as the r.p.m. of rotary arm 6 increases until a predetermined r.p.m. is reached. This structure reduces the frictional force of air on the side face of pit 10a and facilitates the lengthening of rotary arm 6. COPYRIGHT: (C)1997,JPO
100 JPH05508346A - JP50523692 1991-12-18 JPH05508346A 1993-11-25
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