Dodging lens device of airplane hose passage lamp and airplane hose passage lamp
The invention discloses a dodging lens device of an airplane hose passage lamp and the airplane hose passage lamp. The dodging lens device of the airplane hose passage lamp comprises a three-in-one TIR lens group, a light-emitting disc positioning column and a circular light-emitting disc. And the t...
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| creator | ZHANG TAO WANG TINGTING HU KANGHUI |
| description | The invention discloses a dodging lens device of an airplane hose passage lamp and the airplane hose passage lamp. The dodging lens device of the airplane hose passage lamp comprises a three-in-one TIR lens group, a light-emitting disc positioning column and a circular light-emitting disc. And the three-in-one TIR lens group is positioned on the light incident surface side of the circular light emitting disc. The three-in-one TIR lens group is provided with three single TIR lenses which are connected to form a three-petal-shaped structure. The monomeric TIR lens is configured to convert an LED Lambert light source to a collimated light source. And the light-emitting disc positioning column is positioned on the light-in surface side of the circular light-emitting disc. And the light-emitting surface of the circular light-emitting disc is configured to convert a collimated light source into a uniform light source with a specific beam angle. The three-in-one TIR lens group converts an LED Lambert light source in |
| format | Patent |
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The dodging lens device of the airplane hose passage lamp comprises a three-in-one TIR lens group, a light-emitting disc positioning column and a circular light-emitting disc. And the three-in-one TIR lens group is positioned on the light incident surface side of the circular light emitting disc. The three-in-one TIR lens group is provided with three single TIR lenses which are connected to form a three-petal-shaped structure. The monomeric TIR lens is configured to convert an LED Lambert light source to a collimated light source. And the light-emitting disc positioning column is positioned on the light-in surface side of the circular light-emitting disc. And the light-emitting surface of the circular light-emitting disc is configured to convert a collimated light source into a uniform light source with a specific beam angle. 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The dodging lens device of the airplane hose passage lamp comprises a three-in-one TIR lens group, a light-emitting disc positioning column and a circular light-emitting disc. And the three-in-one TIR lens group is positioned on the light incident surface side of the circular light emitting disc. The three-in-one TIR lens group is provided with three single TIR lenses which are connected to form a three-petal-shaped structure. The monomeric TIR lens is configured to convert an LED Lambert light source to a collimated light source. And the light-emitting disc positioning column is positioned on the light-in surface side of the circular light-emitting disc. And the light-emitting surface of the circular light-emitting disc is configured to convert a collimated light source into a uniform light source with a specific beam angle. The three-in-one TIR lens group converts an LED Lambert light source in</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMSTHEREOF</subject><subject>HEATING</subject><subject>INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21Sand F21V, RELATING TO USESOR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-PORTABLE LIGHTING DEVICES</subject><subject>OPTICAL ELEMENTS, SYSTEMS, OR APPARATUS</subject><subject>OPTICS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHERARTICLES, NOT OTHERWISE PROVIDED FOR</subject><subject>SYSTEMS THEREOF</subject><subject>TRANSPORTING</subject><subject>VEHICLE LIGHTING DEVICES SPECIALLY ADAPTED FOR VEHICLEEXTERIORS</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZAhwyU9Jz8xLV8hJzStWSEkty0xOVchPU0jMLCrIScxLVcjIL05VKEgsLk5MT1XIScwtUEjMS8EjzcPAmpaYU5zKC6W5GRTdXEOcPXRTC_LjU4sLEpNT81JL4p39DA0tDIwNDU0tHI2JUQMARA02pw</recordid><startdate>20240514</startdate><enddate>20240514</enddate><creator>ZHANG TAO</creator><creator>WANG TINGTING</creator><creator>HU KANGHUI</creator><scope>EVB</scope></search><sort><creationdate>20240514</creationdate><title>Dodging lens device of airplane hose passage lamp and airplane hose passage lamp</title><author>ZHANG TAO ; WANG TINGTING ; HU KANGHUI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN118031158A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2024</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMSTHEREOF</topic><topic>HEATING</topic><topic>INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21Sand F21V, RELATING TO USESOR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-PORTABLE LIGHTING DEVICES</topic><topic>OPTICAL ELEMENTS, SYSTEMS, OR APPARATUS</topic><topic>OPTICS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHERARTICLES, NOT OTHERWISE PROVIDED FOR</topic><topic>SYSTEMS THEREOF</topic><topic>TRANSPORTING</topic><topic>VEHICLE LIGHTING DEVICES SPECIALLY ADAPTED FOR VEHICLEEXTERIORS</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>ZHANG TAO</creatorcontrib><creatorcontrib>WANG TINGTING</creatorcontrib><creatorcontrib>HU KANGHUI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ZHANG TAO</au><au>WANG TINGTING</au><au>HU KANGHUI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Dodging lens device of airplane hose passage lamp and airplane hose passage lamp</title><date>2024-05-14</date><risdate>2024</risdate><abstract>The invention discloses a dodging lens device of an airplane hose passage lamp and the airplane hose passage lamp. 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| language | chi ; eng |
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| subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMSTHEREOF HEATING INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21Sand F21V, RELATING TO USESOR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS LIGHTING MECHANICAL ENGINEERING NON-PORTABLE LIGHTING DEVICES OPTICAL ELEMENTS, SYSTEMS, OR APPARATUS OPTICS PARACHUTES PERFORMING OPERATIONS PHYSICS STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHERARTICLES, NOT OTHERWISE PROVIDED FOR SYSTEMS THEREOF TRANSPORTING VEHICLE LIGHTING DEVICES SPECIALLY ADAPTED FOR VEHICLEEXTERIORS WEAPONS |
| title | Dodging lens device of airplane hose passage lamp and airplane hose passage lamp |
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