US3387606A - Inductive signal transfer device, useful for aviators' helmets - Google Patents
Inductive signal transfer device, useful for aviators' helmets Download PDFInfo
- Publication number
- US3387606A US3387606A US178980A US17898062A US3387606A US 3387606 A US3387606 A US 3387606A US 178980 A US178980 A US 178980A US 17898062 A US17898062 A US 17898062A US 3387606 A US3387606 A US 3387606A
- Authority
- US
- United States
- Prior art keywords
- core
- plug
- receptacle
- signal transfer
- winding
- 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
- 230000001939 inductive effect Effects 0.000 title description 9
- 230000035699 permeability Effects 0.000 claims description 2
- 230000009467 reduction Effects 0.000 claims description 2
- 238000004804 winding Methods 0.000 description 26
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 20
- 229910052760 oxygen Inorganic materials 0.000 description 20
- 239000001301 oxygen Substances 0.000 description 20
- 238000004891 communication Methods 0.000 description 10
- 239000002184 metal Substances 0.000 description 10
- 230000004907 flux Effects 0.000 description 9
- 230000006698 induction Effects 0.000 description 4
- 230000000295 complement effect Effects 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000008878 coupling Effects 0.000 description 2
- 238000010168 coupling process Methods 0.000 description 2
- 238000005859 coupling reaction Methods 0.000 description 2
- IWEDIXLBFLAXBO-UHFFFAOYSA-N dicamba Chemical compound COC1=C(Cl)C=CC(Cl)=C1C(O)=O IWEDIXLBFLAXBO-UHFFFAOYSA-N 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 238000007654 immersion Methods 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 235000013405 beer Nutrition 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- ZPUCINDJVBIVPJ-LJISPDSOSA-N cocaine Chemical compound O([C@H]1C[C@@H]2CC[C@@H](N2C)[C@H]1C(=O)OC)C(=O)C1=CC=CC=C1 ZPUCINDJVBIVPJ-LJISPDSOSA-N 0.000 description 1
- 230000005494 condensation Effects 0.000 description 1
- 238000009833 condensation Methods 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000004132 cross linking Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005284 excitation Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 210000002445 nipple Anatomy 0.000 description 1
- 238000006213 oxygenation reaction Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F38/00—Adaptations of transformers or inductances for specific applications or functions
- H01F38/14—Inductive couplings
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62B—DEVICES, APPARATUS OR METHODS FOR LIFE-SAVING
- A62B9/00—Component parts for respiratory or breathing apparatus
- A62B9/04—Couplings; Supporting frames
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D10/00—Flight suits
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S336/00—Inductor devices
- Y10S336/02—Separable
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S439/00—Electrical connectors
- Y10S439/95—Electrical connector adapted to transmit electricity to mating connector without physical contact, e.g. by induction, magnetism, or electrostatic field
Definitions
- This invention relates to inductive signal transfer devices and more particularly to their use in combination with an oxygen supply connection to a mask or helmet in a unitary quick disconnect arrangement which avoids the use of metal to metal contacts.
- Astronauts and pilots of military aircraft in the upper atmosphere require a helmet or mask for the control of the oxygen or air supply to the pilot and, at the same time, require connections which can be quickly made or broken in the event it becomes necessary for the pilot to be quickly separated from the craft.
- a diver may require a helmet with an oxygen supply and a communication system associated therewith which may be broken away from the helmet by a single unitary quick disconnect device capable of instantaneous action. It has previously been known to combine with a quick disconnect arrangement for an air supply, a plurality of electrical plugs and sockets each making connection with one circuit in a helmet and with an external circuit.
- a further object of the invention is to provide a combined quick disconnect electrical connection for a plu- 3,387,606 Patented June 11, 1968 rality of circuits and an oxygen supply quick disconnect connection in one unitary assembly.
- a further object is to provide an induction signal transfer device for a plurality of circuits assembled in a single plug-in unit having no exposed electrical contacts subject to corrosion or shorting by atmospheric moisture.
- a still further object of the invention is to provide an inductive signal transfer device for a plurality of circuits where cross talk between the circuits is eliminated.
- this invention utilizes paired transformer core elements in plug and receiver portions, one for each circuit to be established. Adjacent pairs of flux controlling cores are closely spaced but disposed to avoid cross linking flux. Each core and winding is embedded in plastic or the like to present a fully insulated exterior.
- FIG. 1 is a schematic view of a quick disconnect oxygen supply hose connection combined with inductively coupled electrical connections for the pilots communication system.
- FIG. 2 is a schematic diagram of a portion of a plug and receptacle of FIG. 1, illustrating in detail the circuit connection between ear phones, microphones and external circuits, and
- FIG. 3 illustrates an alternative form of a signal transfer device for a plurality of circuits, employing a plug and receptacle suitable for headwear use in which cross talk between circuits is avoided by a further arrangement of the respective cores of the signal transfer devices.
- FIG. 1 there is illustrated at 10 an oxygen supply hose connected to a supply (not shown) such as might be contained in the aircraft in which the pilot is operating.
- An oxygen outlet to the mask or helmet of the pilot is indicated at 11 as a tubular portion of the receiver portion of the quick disconnect fixture.
- the hose member 10 preferably terminates in a plug member 12 which may be of rectangular form having plane surfaces at the upper and lower sides thereof as viewed in FIG. 1, suitable for close fitting insertion in a receiver 13 to which the hose member 10 is to be connected by way of the plug member 12, thereby to provide a continuous oxygen supply from 10 to 11. Details of such a quick disconnect feature in the oxygen supply for a helmet are disclosed in patent application Ser. No. 166,565 filed Jan.
- the copending application employs metal to metal contacts in the faces of the plug member 12 and the receiver member 13 adjacent thereto.
- an arrangement is provided for replacing the metal to metal contacts with inductive signal transfer arrangements employing transformer core halves 14 and 15, disposed one in the plug member and the other in the reltssv sos DCver member immediately adjacent thereto when the plug member is seated within the receiver member.
- transformer core halves 14 and 15 At the opposite face of the plug member 12 is disposed a transformer core half 16 and immediately adjacent thereto is the complementary member 17 in the receiver member, each such core member being wholly within the member and so positioned that when the quick disconnect device is assembled the magnetic circuit between core members 14 and 15 and between members 16 and 17 is substantially closed.
- Leads l818 and 1919 correspond each to a circuit extending into the plug member and connecting with opposite terminals of windings 21 and 22 on the corresponding primary core members 14 or 16.
- the assembled core and winding shall be embedded or potted in a plastic block as at 23 and 24, preferably formed by casting.
- One core and winding may be placed in the plug pocket 25 and another in receptacle pocked 26 in a position to leave each of the core end 27 lying immediately beneath the surface as the block is cast thereover.
- the plug member is engaged Within the receiver member and firmly held in that position by means of a retaining hook on the receiver member as at 28 and a retaining bail 29 attached to the plug member.
- a retaining hook on the receiver member as at 28
- a retaining bail 29 attached to the plug member.
- the bail When the bail is passed over the hook and the plug 12 is pressed into the receiver member 13 it may be locked into position by a lever 30 to establish the airtight connection desired and, at the same time, hold corresponding core ends 27 in position adjacent each other, separated only by a thin section of the plastic block respectively surrounding each such core member.
- FIG. 2 there are shown portions of members 12 and 13 in section, respectively, with core members 14, 16. 15 and 17 in position to substantially complete magnetic circuits therebetween to permit signal transfer by induction.
- Winding 21 is connected to ear phones 31 by way of the leads 32 and winding 21' is connected to an external circuit by way of the leads 18.
- the winding 22 is connected to a microphone 33 by Way of leads 34 and winding 22' is connected to the external circuitry by way of leads 19.
- second microphone may be connected to a further receiver core 35 and thence to a corresponding core 36 on the plug.
- Winding 37 on the core 35 extends to microphone 38 and corresponding leads and winding on the core 36 extends to circuitry within the airplane.
- Such a third signal transfer device might be used, for example, with a second microphone or other device as at 38, which might connect to a second signal output from the pilot, going by internal craft connections to a copilot.
- the microphone 33 might be of the dynamic type in which a sound powered diaphragm and signal generator furnishes current inductively coupling windings 22 and 22' thence extending to the aircraft communication system by means of leads 19.
- Either microphone 38 or 33 might be of the carbon button type or of any other construction employing a small battery to provide a current which is modulated by the action of the microphone in order to provide a more adequate signal to be coupled to the external communication system.
- the contained cores 14 and 16 are oppositely disposed to minimize flux thcrebetween both by separation of pole pieces 27 and by orientation.
- the cores 35 and 36 may be disposed at right angles to the cores 14 and 15, or to 16 and 17 such that any leakage flux is at right angles rather than parallel to the core structure which might otherwise gather a portion thereof to induce cross coupled signals.
- Such an embodiment of the invention as has previously been described is particularly adapted for use with a helmet-mounted oxygen supply connection of the quick disconnect type. but is not so limited in its application.
- This arrangement may be employed in a divers helmet, a bathysphere, or in any other similar arrangement in which it is necessary to pass signals through an outer wall into an inner container without the use of metal to metal contacts such as could be shorted by immersion in water or by atmospheric moisture conditions.
- a cable 41 for this purpose might include a number of signal leads all enclosed within a waterproof rubber or plastic covering which connects to a plug member 42 by means of a fairlead arrangement 43 protecting the cable against chafing or breaking at the connection point.
- Plug member 42 in this version may be of cylindrical form in which corresponding core halves as at 14 and 16 of FIG. 2 are employed each with its winding thereon connecting to the leads within the cable 41.
- Such core members are disposed within the plug member in a position to exactly match the position of the corresponding core halves 15 and 17 disposed within the outer Walls or lateral projections of the receiver and socket member 48, generally in the manner illustrated in FIG. 2, except that orientation is now required between the cylindrical plug and receptacle members so that the corresponding core halves will be oppositely disposed for maximum transfer of signal.
- Such a connector may also conveniently employ a third core 44 like core 35 but disposed in the end of the plug member to cooperate with a similar core 44 in the end of the socket member for the transfer of a third set of signals.
- the plug member 42 is preferably supplied with a key portion 46 along one face thereof which fits within a slot 47 in the corresponding face of the receptable member 48 such that when the two are placed in key-oriented operative position this position is maintained with certarnty and exactitude.
- the socket member is preferably attached to a helmet or enclosure wall at 49 by means of attached nipple 51, collar 52 and nut 53. Internal connections pass from the socket member through a hole 54 in wall 49 to leave an airtight enclosure through which signals pass without use of exposed metal electrical inserts or contacts.
- Spring clips 55 and 56 are appropriately secured to the socket member along two or more opposed sides thereof by means of retaining ring 57 and/or slots according to the method of manufacture most convenient. Clips 55 and 56 have turned in portions 53 arranged to overlie the outer end of the plug member when in place and retain it in that position, and have sloped portions 59 adapted to ride over the plug as it is inserted.
- a first transformer having a secondary core member and winding entirely imbedded within a plastic receptacle wall
- plug and receptacle units being keyed for engagement in predetermined alignment
- said core members being substantially of C-form and of size and disposition within said plug and receptacle units, when aligned, to substantially complete a high permeability magnetic path through said primary and secondary core members,
- a second transformer having primary and secondary core members each with a winding thereon entirely imbedded within receptacle and plug units, respectively, said core members being oriented at least 90 from the core members of the first transformers for reduction of magnetic intercoupling therebetween, and
- a first signal transfer means including matched transformer core portions in juxtaposition one in said plug member and one in said receiver member,
- sadi core portions being substantially of semicircular shape, each having thereon an energizing winding, one to generate when electrically energized flux variations through both said portions and the other to generate voltage signals by induction in response to said fiux variations,
- a second signal transfer means generally like the first and including transformer core portions and windings being disposed with ends of said core portions of said plug member terminating in directions separated substantially at least 90,
- impregnating means covering said core and windings of each signal transfer means and extending to form predetermined spacing between said core portions of each said transfer means
- oxygen hose supply means including a termination for connection to said helmet
- receiver means detachably holding said termination in fluid tight relation to said helmet
- a signal transfer device for quick disconnect service comprising,
- a second split core disposed as the first to complete a similar magnetic pat-h and being :at opposite sides of said plug and receptacle members from first said core for minimizing flux linkage therebetween,
- a third split core dispose-d half within said plug at an inner end thereof and half within said receptacle member with the split core ends in respective juxtaposition when in said orientation
- each core half for transferring signals to and from said plug member and said receptacle member in three magnetically and electrically separate circuits.
- a signal transfer assembly for quick disconnect service for a plurality of simultaneous signals without exposed intervening contacts comprising,
- a cylindrical plastic plug member including therein a plurality of split magnetic core members of C shape each having a pair of ends terminating immediately beneath one surface of said plug member, the respective members being disposed in opposed relation for minimizing magnetic linkage therebetween,
- a cylindrical plastic receptacle member having a similar plurality of split core members complementary to first said members and arranged with corresponding core ends in juxtaposition to said ends, respectively, in said plug member, when the plug member is seated in fixed orientation therein,
- one said core member terminates within an inner end of said plug member and at least one said core member terminates within and at a lateral side of said plug member.
Landscapes
- Health & Medical Sciences (AREA)
- Engineering & Computer Science (AREA)
- Pulmonology (AREA)
- General Health & Medical Sciences (AREA)
- Power Engineering (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connector Housings Or Holding Contact Members (AREA)
- Details Of Connecting Devices For Male And Female Coupling (AREA)
Description
Claims (1)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US178980A US3387606A (en) | 1962-03-12 | 1962-03-12 | Inductive signal transfer device, useful for aviators' helmets |
GB9780/63A GB1025448A (en) | 1962-03-12 | 1963-03-12 | Inductive signal transfer device |
JP1296563A JPS402940B1 (en) | 1962-03-12 | 1963-03-12 | Inductive signal transfer device, useful for aviators' helmets |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US178980A US3387606A (en) | 1962-03-12 | 1962-03-12 | Inductive signal transfer device, useful for aviators' helmets |
Publications (1)
Publication Number | Publication Date |
---|---|
US3387606A true US3387606A (en) | 1968-06-11 |
Family
ID=22654715
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US178980A Expired - Lifetime US3387606A (en) | 1962-03-12 | 1962-03-12 | Inductive signal transfer device, useful for aviators' helmets |
Country Status (3)
Country | Link |
---|---|
US (1) | US3387606A (en) |
JP (1) | JPS402940B1 (en) |
GB (1) | GB1025448A (en) |
Cited By (44)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3667392A (en) * | 1970-04-06 | 1972-06-06 | Us Navy | Ordnance fuze encoding and decoding system |
US3667342A (en) * | 1970-04-08 | 1972-06-06 | Us Navy | Magnetic weapon link transducer |
US3682098A (en) * | 1969-01-11 | 1972-08-08 | Messerschmitt Boelkow Blohm | Explosive charge ignition system |
US3703891A (en) * | 1970-08-28 | 1972-11-28 | Us Air Force | Multi-purpose helmet assembly especially for use with a catheter |
US3728935A (en) * | 1972-01-05 | 1973-04-24 | Us Navy | Coded induction rocket motor ignition system |
US3743989A (en) * | 1971-10-01 | 1973-07-03 | Thomson Csf | Electrical connecting device |
US3772625A (en) * | 1971-05-17 | 1973-11-13 | E Raupach | Transformer for producing or measuring high and very high potentials or for measuring currents at high potentials in cascade connection |
US3892234A (en) * | 1973-06-06 | 1975-07-01 | Gen Aquadyne Inc | Diver{3 s pressurized equipment housings |
US4030058A (en) * | 1976-03-30 | 1977-06-14 | Westinghouse Electric Corporation | Inductive coupler |
US4038625A (en) * | 1976-06-07 | 1977-07-26 | General Electric Company | Magnetic inductively-coupled connector |
US4236086A (en) * | 1977-11-25 | 1980-11-25 | Siemens Aktiengesellschaft | Apparatus for the detection and processing of electric signals |
US4609239A (en) * | 1984-03-06 | 1986-09-02 | Wabco Westinghouse Fahrzeugbremsen Gmbh | Electropneumatic coupling element for providing a pressure-tight connection between a pressure supply line and a pressure supply connection |
US4788544A (en) * | 1987-01-08 | 1988-11-29 | Hughes Tool Company - Usa | Well bore data transmission system |
US4845493A (en) * | 1987-01-08 | 1989-07-04 | Hughes Tool Company | Well bore data transmission system with battery preserving switch |
US4884071A (en) * | 1987-01-08 | 1989-11-28 | Hughes Tool Company | Wellbore tool with hall effect coupling |
US5236048A (en) * | 1991-12-10 | 1993-08-17 | Halliburton Company | Apparatus and method for communicating electrical signals in a well, including electrical coupling for electric circuits therein |
WO1993026062A1 (en) * | 1992-06-16 | 1993-12-23 | Dill Systems Corp. | Magnetic circuits for communicating data |
US5677667A (en) * | 1995-02-23 | 1997-10-14 | Vehicle Enhancement Systems, Inc. | Data communications apparatus for tractor/trailer using pneumatic coupler |
US5814900A (en) * | 1991-07-30 | 1998-09-29 | Ulrich Schwan | Device for combined transmission of energy and electric signals |
US5890929A (en) * | 1996-06-19 | 1999-04-06 | Masimo Corporation | Shielded medical connector |
US6032546A (en) * | 1997-07-21 | 2000-03-07 | Stone; Neil | System for transferring electrical power between non-contacting elements in relative motion |
US6111524A (en) * | 1995-11-09 | 2000-08-29 | Vehicle Enhancement Systems, Inc. | Systems and methods for identifying tractor/trailers and components thereof |
US6127939A (en) * | 1996-10-14 | 2000-10-03 | Vehicle Enhancement Systems, Inc. | Systems and methods for monitoring and controlling tractor/trailer vehicle systems |
US20020193004A1 (en) * | 2001-06-14 | 2002-12-19 | Boyle Bruce W. | Wired pipe joint with current-loop inductive couplers |
US6604038B1 (en) | 1999-11-09 | 2003-08-05 | Power Talk, Inc. | Apparatus, method, and computer program product for establishing a remote data link with a vehicle with minimal data transmission delay |
US6705898B2 (en) * | 2000-11-07 | 2004-03-16 | Endress + Hauser Conducta Gesellschaft Fur Mess-Und Regeltechnik Mbh +Co. | Connector for connecting a transmission line to at least one sensor |
US20040217880A1 (en) * | 2003-04-29 | 2004-11-04 | Brian Clark | Method and apparatus for performing diagnostics in a wellbore operation |
US20050016787A1 (en) * | 1999-11-17 | 2005-01-27 | Lesesky Alan C. | Method for data communication between a vehicle and a remote terminal |
US20050016540A1 (en) * | 2003-07-24 | 2005-01-27 | Werner Jumpertz | Respirator product with an electric component |
US20050046591A1 (en) * | 2003-08-29 | 2005-03-03 | Nicolas Pacault | Method and apparatus for performing diagnostics on a downhole communication system |
US20060208873A1 (en) * | 1995-11-09 | 2006-09-21 | Alan Lesesky | System, apparatus and methods for data communication between vehicle and remote data communication terminal, between portions of vehicle and other portions of vehicle, between two or more vehicles, and between vehicle and communications network |
US20070173099A1 (en) * | 2002-06-25 | 2007-07-26 | Resmed Limited | Method and apparatus for control of appliance coupler retention and withdrawal forces |
US20090191246A1 (en) * | 2004-08-11 | 2009-07-30 | Catalysts& Chemicals Industries Co., Ltd. | Method of producing scale-like composite particles |
WO2010027282A2 (en) * | 2008-09-05 | 2010-03-11 | Fisher & Paykel Healthcare Limited | Contactless power transfer in a system for providing respiratory gases to a user for therapeutic purposes |
US20120045907A1 (en) * | 2009-06-30 | 2012-02-23 | Nissan Motor Co., Ltd. | Electrical component structure |
US8997652B2 (en) | 2003-05-08 | 2015-04-07 | Lone Star Ip Holdings, Lp | Weapon and weapon system employing the same |
US9006628B2 (en) | 2005-09-30 | 2015-04-14 | Lone Star Ip Holdings, Lp | Small smart weapon and weapon system employing the same |
US9068803B2 (en) | 2011-04-19 | 2015-06-30 | Lone Star Ip Holdings, Lp | Weapon and weapon system employing the same |
US9068796B2 (en) | 2006-09-29 | 2015-06-30 | Lone Star Ip Holdings, Lp | Small smart weapon and weapon system employing the same |
US9467207B2 (en) | 2013-09-12 | 2016-10-11 | The United States Of America As Represented By The Secretary Of The Army | System for transferring electrical energy |
US9550568B2 (en) * | 2006-10-26 | 2017-01-24 | Lone Star Ip Holdings, Lp | Weapon interface system and delivery platform employing the same |
EP3457524A1 (en) * | 2014-06-06 | 2019-03-20 | IHI Corporation | Power-transmitting device, power-receiving device, and wireless power supply system |
CN112216092A (en) * | 2019-07-10 | 2021-01-12 | 恩德莱斯和豪瑟尔分析仪表两合公司 | Field device and remote station |
US20210111513A1 (en) * | 2009-03-11 | 2021-04-15 | Masimo Corporation | Magnetic connector |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3711691A1 (en) * | 1987-04-07 | 1988-10-27 | Bayerische Motoren Werke Ag | DEVICE FOR INDUCTIVE POWER SUPPLY OF AN ELECTRICAL CIRCUIT ARRANGED ON A ROTATING SHAFT |
NO944266L (en) * | 1993-11-15 | 1995-05-16 | Hughes Aircraft Co | Inductive charging system |
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US2745074A (en) * | 1951-01-11 | 1956-05-08 | Ralph E Darling | Electrically equipped oxygen hose |
US2854642A (en) * | 1955-10-25 | 1958-09-30 | Anco Mfg Corp | Intermediate frequency transformer with toroidal coils |
US2857576A (en) * | 1956-06-02 | 1958-10-21 | Knorr Bremse Gmbh | Coupling devices |
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-
1962
- 1962-03-12 US US178980A patent/US3387606A/en not_active Expired - Lifetime
-
1963
- 1963-03-12 JP JP1296563A patent/JPS402940B1/en active Pending
- 1963-03-12 GB GB9780/63A patent/GB1025448A/en not_active Expired
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US2889522A (en) * | 1953-08-05 | 1959-06-02 | Gen Instrument Corp | Tuned transformer assembly |
US2886788A (en) * | 1954-05-04 | 1959-05-12 | Sprague Electric Co | Variable inductor |
US2854642A (en) * | 1955-10-25 | 1958-09-30 | Anco Mfg Corp | Intermediate frequency transformer with toroidal coils |
US2857576A (en) * | 1956-06-02 | 1958-10-21 | Knorr Bremse Gmbh | Coupling devices |
US3210715A (en) * | 1962-01-16 | 1965-10-05 | Robertshaw Controls Co | Quick disconnect coupling |
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JPS402940B1 (en) | 1965-02-16 |
GB1025448A (en) | 1966-04-06 |
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Legal Events
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Owner name: LIFE SUPPORT PRODUCTS, INC., Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:ROBERTSHAW CONTROLS COMPANY, 1701 BYRD AVE., RICHMOND, VA. A CORP. OF DEL.;REEL/FRAME:004086/0511 Effective date: 19820930 Owner name: LIFE SUPPORT PRODUCTS, INC.,, CALIFORNIA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:ROBERTSHAW CONTROLS COMPANY, 1701 BYRD AVE., RICHMOND, VA. A CORP. OF DEL.;REEL/FRAME:004086/0511 Effective date: 19820930 |
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Owner name: SABRE INDUSTRIES, INC., A CORP OF CA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:LIFE SUPPORT PRODUCTS, INC.;REEL/FRAME:004296/0493 Effective date: 19840806 |