公开(公告)号：US20130026289A1

公开(公告)日：2013-01-31

申请号：US13634756

申请日：2010-04-22

Applicant: Kenji Uegaki

Inventor： Kenji Uegaki

IPC: B64C25/58 ,  F16F7/12

CPC classification number: F16F7/121 ,  F16F2224/0225

Abstract: An object of the invention is to provide an energy absorption structure that can suppress the fall of an energy absorption member when a load is applied to the energy absorption structure. According to the energy absorption structure of the invention, when a load is applied to the energy absorption structure, the relative displacement between a first member and an energy absorption member is suppressed by a displacement suppressing member that connect the first member with the energy absorption member. Accordingly, the fall of the energy absorption member can be suppressed.

Abstract translation: 本发明的目的是提供一种能量吸收结构，其能够在负载施加到能量吸收结构时抑制能量吸收构件的下降。 根据本发明的能量吸收结构，当向能量吸收结构施加负载时，通过将第一构件与能量吸收构件连接的位移抑制构件抑制第一构件与能量吸收构件之间的相对位移， 。 因此，能够抑制能量吸收部件的下降。

公开(公告)号：US20110272523A1

公开(公告)日：2011-11-10

申请号：US13144313

申请日：2009-01-18

Applicant: Kenji Uegaki

Inventor： Kenji Uegaki

IPC: B64C25/56

CPC classification number: B64C1/062 ,  B64D17/80 ,  B64D2201/00

Abstract: An air bag 4 is inflated in a shock absorption system 1 by a high pressure air cylinder 5 at the time of a collision between an aircraft and the ground that is caused by inability to fly or the like, so that a cover body 2 is unfolded to the outside from a bottom portion 11a of a fuselage 11 of the aircraft 10 and the air bag 4 is disposed inside the cover body 2. Accordingly, a sufficient shock absorption stroke is obtained, so that it may be possible to reliably absorb shock that is generated at the fuselage 11 during the collision between the aircraft and the ground caused by an inability to fly or the like. Further, the cover body 2 is unfolded from the bottom portion 11a of the fuselage 11 so as to spread out toward the rear side of the aircraft 10. Accordingly, it may be possible to make the fuselage 11 smoothly slide on the ground during the collision between the aircraft and the ground that is caused by an inability to fly or the like. Therefore, according to the shock absorption system 1, it may be possible to prevent the fuselage 11 of the aircraft 10 from being damaged during the collision between the aircraft and the ground that is caused by an inability to fly or the like.

Abstract translation: 空气囊4在飞行器与地面之间由于不能飞行等引起的碰撞时由高压气缸5在减震系统1中膨胀，使得盖体2展开 从飞机10的机身11的底部11a到外面，并且气囊4设置在盖体2的内侧。因此，获得足够的冲击吸收冲程，使得可以可靠地吸收冲击， 在飞机和地面之间的碰撞期间由于不能飞行等而导致在机身11处产生。 此外，盖体2从机身11的底部11a展开，以便朝向飞机10的后侧展开。因此，可能使机身11在碰撞期间在地面上平滑地滑动 在由于无法飞行等而引起的飞机和地面之间。 因此，根据减震系统1，可以防止飞机10的机身11在由于不能飞行等引起的飞机和地面之间的碰撞期间被损坏。

公开(公告)号：US20120319441A1

公开(公告)日：2012-12-20

申请号：US13578507

申请日：2010-03-12

Applicant: Kenji Uegaki

Inventor： Kenji Uegaki

IPC: B64D11/06 ,  B60N2/42

CPC classification number: B64D11/0689 ,  B60N2/24 ,  B60N2/4242 ,  B60N2/42709 ,  B60N2/42736 ,  B64D11/0619 ,  Y02T50/46

Abstract: An object of the invention is to provide a structure for an aircraft seat section is configured to be able to have an appropriate impact absorbing stroke in an aircraft having a small interior space. The structure is provided with a survival tub (1) which is an occupant protection member for surrounding from the lower side of the aircraft body, the space for an occupant (51) which includes a seat (50) on which the occupant sits. Preferably, the survival tub (1) is held by link mechanisms (4, 5) and an impact absorption operation section (9) so that during impact, the survival tub (1) can move to the upper side of the aircraft body.

Abstract translation: 本发明的目的是提供一种用于飞行器座椅部分的结构，其能够在具有小的内部空间的飞行器中具有适当的冲击吸收行程。 该结构设置有作为乘员保护构件的救生桶（1），该乘员保护构件用于围绕飞行器主体的下侧，乘员空间（51），其包括座椅（50），乘员坐在座椅上。 优选地，存活桶（1）由连杆机构（4,5）和冲击吸收操作部（9）保持，使得在冲击期间，救生桶（1）能够移动到飞行器主体的上侧。