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1. 发明申请

US20180343837A1 PLATFORM BIRD FEEDER WITH AN ADJUSTABLE WOBBLING BAFFLE 审中-公开
公开(公告)号：US20180343837A1
公开(公告)日：2018-12-06
申请号：US15827990
申请日：2017-11-30
申请人： WOODSTREAM CORPORATION
发明人： Judith Kim HOYSAK
IPC分类号： A01K39/01 , A01K39/014
CPC分类号： A01K39/0113 , A01K39/014 , Y10T29/49948
摘要： A platform bird feeder is provided including a base platform with a seed tray, a baffle and a center pole having a bottom end connected the tray, the baffle being tiltably and adjustably mounted to the pole above the base. Preferably, the seed tray has a seed protecting grate to hinder squirrels from accessing the seed in the tray. The height of the baffle above the seed tray may be adjusted up and down to allow the user to increase and decrease the seed access space, respectively, between the baffle and the tray. When the baffle is at a desired height, it is secured in place by an adjustable securing mechanism that, while holding the baffle at the desired height, allows the baffle to tilt or wobble when sufficient weight is placed on one side of the baffle.

2. 发明申请

US20180281132A1 Method for Tightening a Thread Joint 审中-公开
公开(公告)号：US20180281132A1
公开(公告)日：2018-10-04
申请号：US15606116
申请日：2017-05-26
申请人： Mikhail Borisovich MELNIKOV
发明人： Mikhail Borisovich MELNIKOV
IPC分类号： B23P19/06
CPC分类号： B23P19/061 , B23P2700/11 , E21B19/16 , F16B5/0275 , F16B25/0057 , F16B25/0073 , F16B31/04 , F16B33/02 , F16B2033/04 , F16D1/00 , F16D1/108 , Y10T29/49948 , Y10T29/49963
摘要： The invention relates to thread joints and can be used in mechanical engineering, equipment construction, the oil and gas industry and communal utility systems.A method for tightening a thread joint of a base part with a small thread pitch and a part to be attached with a large thread pitch by rotation in screw-in direction of a differential thread connector, comprising portions of a one-directional thread corresponding to the threads of the base part and the part to be attached. The differential thread connector is formed in such a way that it can be screwed on the small thread of the base part to a predetermined length, subsequently the part to be attached is screwed on the large thread of the differential thread connector until contact with the base part is reached, and the preliminary tightening is carried out in screw-in direction, and subsequently the differential thread connector is rotated in screw-out direction and the final tightening is carried out. For instance, the method is applicable for tightening two cylindrical parts, one part 1 with a threaded portion with a pitch S1 and a plane contact surface 4, to another part 2 with a threaded portion with a pitch S2 and a plane contact surface 5, the thread pitch S2 being larger than the pitch S1 by an amount of ΔS=S2−S1. A differential thread connector 3 is formed as a coupling with portions with an inner thread with pitches S1 and S2. The method for tightening a thread joint is carried out as follows. The part 1 with the thread pitch S1 is screwed into a threaded aperture of the differential thread joint 3 to a predetermined length A. Subsequently the part 2 with the thread pitch S2 is screwed into the differential thread connector 3 from the opposite end until coupling of the contact surface 5 of the part 2 with the contact surface 4 of the part 1 is reached. In this position the preliminary tightening of the joint with a torque M1 in the direction of the arrow 6 (screw-in) is carried out. Further, while the part 2 is kept immobile, the differential thread connector 3 is rotated around the arrow 7 (screw-out), and the final tightening of the joint is carried out with a torque M2>M1.

3. 发明授权

US10072729B2 Balancing device and method 有权
公开(公告)号：US10072729B2
公开(公告)日：2018-09-11
申请号：US14670227
申请日：2015-03-26
申请人： SAFRAN AIRCRAFT ENGINES
发明人： Olivier Belmonte , Lucie Galons
IPC分类号： F16F15/34 , F01D5/02 , F16F15/32 , G01M1/04 , G01M1/34
CPC分类号： F16F15/34 , F01D5/027 , F16F15/322 , G01M1/04 , G01M1/34 , Y10T29/49948
摘要： A balancing method for a rotating part device including a nut having an internal thread, and a countersunk collar is disclosed. The countersunk collar has a through-hole with a diameter greater than the diameter of the internal thread of the nut. The countersunk collar includes a balancing weight.

4. 发明授权

US10072464B2 Earth-boring tools including formation-engaging structures having retention features and related methods 有权
公开(公告)号：US10072464B2
公开(公告)日：2018-09-11
申请号：US15155470
申请日：2016-05-16
申请人： Baker Hughes Incorporated
发明人： Do Van Do , Juan Miguel Bilen , Steven C. Russell , Kenneth R. Evans , Jason E. Hoines , Oliver Matthews , R. Keith Glasgow , Chaitanya K. Vempati
IPC分类号： E21B10/00 , E21B10/633 , E21B10/43 , B23P15/28 , E21B10/42 , E21B10/54
CPC分类号： E21B10/633 , B23P15/28 , E21B10/42 , E21B10/43 , E21B10/54 , E21B2010/425 , Y10T29/49948 , Y10T29/49964
摘要： An earth-boring tool includes a formation-engaging structure with a formation-engaging surface at a distal end and a side surface between a proximal end and the distal end along a central axis of the formation-engaging structure. A generally linear recess may be formed in the side surface along an axis oriented at a non-parallel angle relative to the central axis of the formation-engaging structure. A generally helical recess may be formed in the side surface, and the generally helical recess may intersect the generally linear recess. Earth-boring tools may include such formation-engaging structures. Methods may be used to form such formation-engaging structures.

5. 发明申请

US20180231044A1 PUSH PIN WITH ANTIROTATIONAL STOPPER AND METHOD OF USE THEREOF 审中-公开
公开(公告)号：US20180231044A1
公开(公告)日：2018-08-16
申请号：US15891321
申请日：2018-02-07
申请人： William BEJIN , Thomas Dale OWEN
发明人： William BEJIN , Thomas Dale OWEN
IPC分类号： F16B21/16
CPC分类号： F16B21/16 , F16B33/002 , F16B35/048 , F16L3/137 , F16L3/233 , H01R4/48 , H01R13/73 , Y10T29/49948
摘要： A push pin with rotational stopper and method of use thereof includes a push pin configured with a plurality of retention barbs extending outward from a surface of the insertion member, the insertion member configured with an anti-rotation section to friction fit therewith a sidewall of an aperture in the panel, an disc spring positioned proximate said anti-rotation section and configured to provide an opposing force to said retention barbs to limit insertion and removal therein the aperture in the panel.

6. 发明申请

US20180172055A1 Method for the connection of sheet metal parts and component assembly as well as setting head and die button 审中-公开
公开(公告)号：US20180172055A1
公开(公告)日：2018-06-21
申请号：US15895560
申请日：2018-02-13
申请人： PROFIL Verbindungstechnik GmbH & Co. KG
发明人： Oliver Diehl , Andreas Lembach
IPC分类号： F16B37/06 , B29C65/00 , F16B5/04 , B21J15/02 , B29C65/56
CPC分类号： F16B37/062 , B21J15/025 , B21J15/147 , B29C65/562 , B29C65/602 , B29C66/1122 , B29C66/21 , B29C66/41 , B29C66/721 , B29C66/7212 , B29C66/7392 , B29C66/7394 , B29C66/8161 , B29C66/8167 , B29C66/8242 , B29C66/8322 , F16B5/04 , F16B19/05 , F16B19/06 , Y10T29/49948 , Y10T403/4949 , B29K2307/04 , B29K2309/08 , B29K2277/10
摘要： A component assembly having a stacked arrangement comprising an upper and lower sheet part, of which at least one is formed as an organic sheet composite part, with an auxiliary joining part and with at least one apertured metal washer, wherein the auxiliary joining part has a functional section having an undercut at one end and also has a piercing section at the other end having a lateral shaft surface and a shaft recess formed therein, wherein the metal washer contacts a surface of the organic sheet composite part, with the functional section or the piercing section extending through an aperture of the metal washer and wherein washer material has been driven into the undercut or into the at least one shaft recess.

7. 发明授权

US09976584B2 Multi-piece panel fastener 有权
公开(公告)号：US09976584B2
公开(公告)日：2018-05-22
申请号：US14524154
申请日：2014-10-27
申请人： Eaton Corporation
发明人： David Charles Nelson
IPC分类号： F16B5/06 , F16B21/07
CPC分类号： F16B5/065 , F16B21/075 , Y10T24/44026 , Y10T29/49948
摘要： A fastener includes a clip including a flexible head having an outer surface configured to engage and edge of a first slot in a first panel when the flexible head is inserted therein and a retainer configured to be inserted into a channel within the flexible head to impede flexing of the flexible head thereby retain the flexible head in the first slot. The clip may further include at least one member extending from the head and configured to engage a second slot in a second panel to hold the first and second panels together when the first and second slots are positioned in an opposing relationship. In some embodiments, the at least one member may include first and second spring arm members extending from the head and having outer surfaces configured to engage edges of the second slot when inserted therein. Methods using such fasteners are also discussed.

8. 发明申请

US20180104775A1 ASSEMBLY OF AN AIRCRAFT STRUCTURE ASSEMBLY WITHOUT SHIMMING, LOCATING FIXTURES OR FINAL-HOLE-SIZE DRILL JIGS 审中-公开
公开(公告)号：US20180104775A1
公开(公告)日：2018-04-19
申请号：US15846508
申请日：2017-12-19
申请人： THE BOEING COMPANY
发明人： David Ray Turner , Donald L. Erion , Teresa M. Finchamp , Gregory Jon Goodman
IPC分类号： B23P15/00 , B64F5/10 , G05B19/418 , G05B19/4097
CPC分类号： B23P15/00 , B23P2700/01 , B64F5/10 , G05B19/4097 , G05B19/41805 , Y02P90/04 , Y10T29/49947 , Y10T29/49948 , Y10T29/49956 , Y10T29/49963
摘要： A method is provided for assembling an aircraft structure assembly composed of a plurality of sections, and doing so without use of any shimming, locating fixtures or final-hole-size drill jigs. The method includes supporting the first and second frame sections on respective adjustable supports, and positioning the interconnecting frame section therebetween. The method includes aligning first pre-drilled mating holes in the interconnecting frame section with first pre-drilled mating holes in the first and second frame sections, and installing fasteners through the aligned, first pre-drilled mating holes. The method includes positioning a structural mating section relative to the first and second frame sections and interconnecting frame section. And aligning second pre-drilled mating holes in the structural mating section with second pre-drilled mating holes in at least one of the frame sections, and installing fasteners through the aligned, second pre-drilled mating holes to secure the structural mating section.

9. 发明授权

US09939090B2 Extraction device for removing an adapter secured in a port 有权
公开(公告)号：US09939090B2
公开(公告)日：2018-04-10
申请号：US13929593
申请日：2013-06-27
申请人： The Gates Corporation
发明人： Donald R. Gilbreath
IPC分类号： F16L23/00 , F16B39/02 , F16B39/04 , F16B39/10 , F16L19/00 , F16L19/02 , F16L21/08
CPC分类号： F16L21/08 , F16B39/00 , F16B39/02 , F16B39/101 , F16L19/005 , F16L19/02 , F16L23/00 , F16L2201/10 , Y10T29/49815 , Y10T29/49948 , Y10T29/5367
摘要： This disclosure relates generally to couplings used in mining and other applications. An extraction device for removing an adapter from a port formed in a structure is provided. The extraction device may include an end wall and a side wall. The end wall may define an external face of the extraction device. The side wall may extend axially away from a periphery of the end wall. The side wall may terminate at an end face of the extraction device. The end face may have a larger dimension than the port so as to abut the structure adjacent to a periphery of the port. The side wall may include an inner surface and an outer surface. The inner surface may have a threaded portion.

10. 发明授权

US09927592B2 Cable enclosure systems, plugs and methods for using the same 有权
公开(公告)号：US09927592B2
公开(公告)日：2018-03-27
申请号：US15269596
申请日：2016-09-19
申请人： CommScope Technologies LLC
发明人： Roy Keller Thompson , Thomas Ross Marmon , Julian S. Mullaney , William Alan Carrico , Barry Wayne Allen
IPC分类号： G02B6/44 , H02G15/007 , G02B6/38
CPC分类号： G02B6/4471 , G02B6/3887 , G02B6/4444 , G02B6/4446 , G02B6/4477 , G02B6/4478 , H02G15/007 , Y10T29/49948
摘要： An enclosure system for receiving a cable includes an enclosure having an inner chamber and an open position exposing the inner chamber and a closed position covering the inner chamber. A cable receiving port in a wall of the enclosure extends along a longitudinal axis from outside of the enclosure into the inner chamber. The cable receiving port is configured to receive a cable therein when the cable is advanced axially into the port without rotation of the cable when the enclosure is in the closed position. A mating member is associated with the cable receiving port that limits rotation of the cable when the cable is advanced axially into the port. An axial retention member is associated with the cable receiving port that limits axial movement of the cable out of the port when the cable is advanced axially into the port to a lock position.

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