http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2019196142-A

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assignee http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_8e43b4ca6b41ce9f54c9a895d474c81a
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C31-036
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filingDate 2018-05-11-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_cb0a364d6391732c8ebe3d011ee6c1ce
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publicationDate 2019-11-14-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber JP-2019196142-A
titleOfInvention Impact shock absorber and flying vehicle equipped with shock shock absorber
abstract The present invention provides a deployment device such as a parachute and a flying body including the deployment device, which can easily and accurately inject and deploy a parachute and the like. A deployment device 90 includes an actuator 88 and a parachute or paraglider 86. The actuator 88 includes a gas generator 84 having a cup-shaped case 85 for containing an igniting agent, a piston 81 having a concave portion 82 and a piston head 83 formed integrally with the concave portion 82, and a piston 81 for containing the piston 81. And a bottomed cylindrical housing 80 that regulates the propulsion direction of the piston 81. The parachute or paraglider 86 is connected and accommodated by a string-like member to the flying object 100 or a device attached to the flying object 100 in a state of being arranged on the piston head 83. A communication portion 51 is formed between the inner wall of the housing 80 and the outer peripheral portion of the piston head 83. [Selection] Figure 2
isCitedBy http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-7276197-B2
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priorityDate 2018-05-11-04:00^^<http://www.w3.org/2001/XMLSchema#date>
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Total number of triples: 32.