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公开(公告)号:SI3218263T1
公开(公告)日:2022-08-31
申请号:SI201531839
申请日:2015-11-10
Applicant: ASCENT AEROSYSTEMS INC
Inventor: MERINGER JONATHAN R , MERINGER NATHANIEL R
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公开(公告)号:PL3218263T3
公开(公告)日:2022-07-11
申请号:PL15859431
申请日:2015-11-10
Applicant: ASCENT AEROSYSTEMS INC
Inventor: MERINGER JONATHAN R , MERINGER NATHANIEL R
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公开(公告)号:ES2915064T3
公开(公告)日:2022-06-20
申请号:ES15859431
申请日:2015-11-10
Applicant: ASCENT AEROSYSTEMS INC
Inventor: MERINGER JONATHAN , MERINGER NATHANIEL
Abstract: Un dispositivo volador no tripulado, que comprende: un cuerpo; un cubo (40) de rotor acoplado giratoriamente al cuerpo; una primera aspa (60A) y al menos una segunda aspa (60B), aspas (60A, 60B) que están configuradas para proporcionar sustentación vertical; un conjunto de acoplamiento para acoplar cada una de la primera aspa (60A) y la al menos una segunda aspa (60B) al cubo (40) de rotor, en donde cada conjunto de acoplamiento comprende un brazo (65) de rotor que tiene una primera sección (65B) de brazo de rotor a la que están acopladas las aspas (60A, 60B), estando cada primera sección (65B) de brazo de rotor acoplada de manera articulada con respecto al cubo (40) de rotor en una bisagra (70); en donde tanto la primera aspa (60A) como la al menos una segunda aspa (60B) pueden girar en torno al cuerpo, y en donde la primera aspa (60A) y la al menos una segunda aspa (60B) pueden desplegarse lejos del cuerpo mediante la rotación de la primera y la al menos una segunda aspa en torno al cuerpo, caracterizado por medios para forzar la primera aspa (60A) y la al menos una segunda aspa (60B) a pivotar en torno a dichas bisagras (70) para hacer caer las aspas (60A, 60B) hacia el cuerpo.
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公开(公告)号:PT3218263T
公开(公告)日:2022-05-16
申请号:PT15859431
申请日:2015-11-10
Applicant: ASCENT AEROSYSTEMS INC
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公开(公告)号:US20220219820A1
公开(公告)日:2022-07-14
申请号:US17709883
申请日:2022-03-31
Applicant: Ascent AeroSystems Inc.
Inventor: Jonathan R. Meringer , Nathaniel R. Meringer
Abstract: An unmanned flying device including a body; a first blade and at least a second blade; a coupling assembly for coupling the first blade and the at least second blade to the body, wherein the coupling assembly urges the collapsing of the first blade and the at least second blade towards the body; and wherein both the first blade and the at least second blade are rotateable about the body, and wherein the first blade and the at least second blade are deployable away from the body via rotation of the first and the at least second blades about the body.
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公开(公告)号:US11292595B2
公开(公告)日:2022-04-05
申请号:US16151637
申请日:2018-10-04
Applicant: Ascent AeroSystems Inc.
Inventor: Jonathan R. Meringer , Nathaniel R. Meringer
Abstract: An unmanned flying device including a body; a first blade and at least a second blade; a coupling assembly for coupling the first blade and the at least second blade to the body, wherein the coupling assembly urges the collapsing of the first blade and the at least second blade towards the body; and wherein both the first blade and the at least second blade are rotatable about the body, and wherein the first blade and the at least second blade are deployable away from the body via rotation of the first and the at least second blades about the body.
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公开(公告)号:US20190092466A1
公开(公告)日:2019-03-28
申请号:US16151637
申请日:2018-10-04
Applicant: Ascent AeroSystems Inc.
Inventor: Jonathan R. Meringer , Nathaniel R. Meringer
Abstract: An unmanned flying device including a body; a first blade and at least a second blade; a coupling assembly for coupling the first blade and the at least second blade to the body, wherein the coupling assembly urges the collapsing of the first blade and the at least second blade towards the body; and wherein both the first blade and the at least second blade are rotateable about the body, and wherein the first blade and the at least second blade are deployable away from the body via rotation of the first and the at least second blades about the body.
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公开(公告)号:US12122541B2
公开(公告)日:2024-10-22
申请号:US17709883
申请日:2022-03-31
Applicant: Ascent AeroSystems Inc.
Inventor: Jonathan R. Meringer , Nathaniel R. Meringer
IPC: B64C27/50 , B64C27/00 , B64U10/13 , B64U30/24 , B64U30/293 , B64U70/10 , B64U101/31
CPC classification number: B64U30/293 , B64C27/006 , B64C27/50 , B64U10/13 , B64U30/24 , B64U70/10 , B64U2101/31 , B64U2201/10 , B64U2201/20
Abstract: An unmanned flying device including a body; a first blade and at least a second blade; a coupling assembly for coupling the first blade and the at least second blade to the body, wherein the coupling assembly urges the collapsing of the first blade and the at least second blade towards the body; and wherein both the first blade and the at least second blade are rotatable about the body, and wherein the first blade and the at least second blade are deployable away from the body via rotation of the first and the at least second blades about the body.
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公开(公告)号:EP4053016A1
公开(公告)日:2022-09-07
申请号:EP22160618.9
申请日:2015-11-10
Applicant: Ascent Aerosystems Inc.
Inventor: MERINGER, Jonathan R , MERINGER, Nathaniel R
Abstract: An unmanned flying device including a body; a first blade and at least a second blade; a coupling assembly for coupling the first blade and the at least second blade to the body, wherein the coupling assembly urges the collapsing of the first blade and the at least second blade towards the body; and wherein both the first blade and the at least second blade are rotateable about the body, and wherein the first blade and the at least second blade are deployable away from the body via rotation of the first and the at least second blades about the body.
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公开(公告)号:EP3218263A4
公开(公告)日:2018-07-04
申请号:EP15859431
申请日:2015-11-10
Applicant: ASCENT AEROSYSTEMS INC
Inventor: MERINGER JONATHAN R , MERINGER NATHANIEL R
CPC classification number: B64C39/024 , B64C27/10 , B64C27/50 , B64C2201/102 , B64C2201/108 , B64C2201/18
Abstract: An unmanned flying device including a body; a first blade and at least a second blade; a coupling assembly for coupling the first blade and the at least second blade to the body, wherein the coupling assembly urges the collapsing of the first blade and the at least second blade towards the body; and wherein both the first blade and the at least second blade are rotatable about the body, and wherein the first blade and the at least second blade are deployable away from the body via rotation of the first and the at least second blades about the body.
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