RADOME RING FOR FLYING BODY
PROBLEM TO BE SOLVED: To prevent increase of flight times of flying bodies in these days, and damage of a radome resulting from increasing flight speed.SOLUTION: A slit is provided in a radome ring for a flying body connecting a radome provided at the tip part of the flying body and a shell to be a...
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| Main Author | |
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| Format | Patent |
| Language | English Japanese |
| Published |
05.09.2016
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| Subjects | |
| Online Access | Get full text |
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| Abstract | PROBLEM TO BE SOLVED: To prevent increase of flight times of flying bodies in these days, and damage of a radome resulting from increasing flight speed.SOLUTION: A slit is provided in a radome ring for a flying body connecting a radome provided at the tip part of the flying body and a shell to be a body portion of the flying body. Consequently, deformation of expanding to radial outside of the radome ring can be absorbed in an in-plane direction of the radome ring, and then heat stress occurring at a portion connecting the radome and the radome ring can be reduced.SELECTED DRAWING: Figure 2
【課題】近年の飛しょう体の飛しょう時間の増加や、飛しょう速度の高速化により生じるレドームの破損を防止する。【解決手段】飛しょう体の先端部に設けられるレドームと、飛しょう体の本体部分であるシェルとを接合する飛しょう体用レドームリングにスリットを設ける。これにより、レドームリングの径方向外側に膨張する変形をレドームリングの面内方向で吸収でき、レドームとレドームリングを接合する部位に生じる熱応力を緩和することができる。【選択図】図２ |
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| AbstractList | PROBLEM TO BE SOLVED: To prevent increase of flight times of flying bodies in these days, and damage of a radome resulting from increasing flight speed.SOLUTION: A slit is provided in a radome ring for a flying body connecting a radome provided at the tip part of the flying body and a shell to be a body portion of the flying body. Consequently, deformation of expanding to radial outside of the radome ring can be absorbed in an in-plane direction of the radome ring, and then heat stress occurring at a portion connecting the radome and the radome ring can be reduced.SELECTED DRAWING: Figure 2
【課題】近年の飛しょう体の飛しょう時間の増加や、飛しょう速度の高速化により生じるレドームの破損を防止する。【解決手段】飛しょう体の先端部に設けられるレドームと、飛しょう体の本体部分であるシェルとを接合する飛しょう体用レドームリングにスリットを設ける。これにより、レドームリングの径方向外側に膨張する変形をレドームリングの面内方向で吸収でき、レドームとレドームリングを接合する部位に生じる熱応力を緩和することができる。【選択図】図２ |
| Author | YANO KENICHIRO |
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| Discipline | Medicine Chemistry Sciences |
| DocumentTitleAlternate | 飛しょう体用レドームリング |
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| Notes | Application Number: JP20150043109 |
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| RelatedCompanies | MITSUBISHI ELECTRIC CORP |
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| Snippet | PROBLEM TO BE SOLVED: To prevent increase of flight times of flying bodies in these days, and damage of a radome resulting from increasing flight... |
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| SubjectTerms | AMMUNITION ANTENNAS, i.e. RADIO AERIALS BASIC ELECTRIC ELEMENTS BLASTING ELECTRICITY EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS |
| Title | RADOME RING FOR FLYING BODY |
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