IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0874385
(2001-06-06)
|
우선권정보 |
JP-0172516 (2000-06-08) |
발명자
/ 주소 |
|
출원인 / 주소 |
|
대리인 / 주소 |
|
인용정보 |
피인용 횟수 :
12 인용 특허 :
7 |
초록
▼
A front seat 2 is divided into a driver seat 2a and a front passenger seat 2b, a second-row seat 3 and a rearmost seat 4 are divided into a first seat 3a, 4a and a second seat 3b, 4b, the front passenger seat 2b and the second seat 4b of the rearmost seat 4 are configured so as to be foldable, and t
A front seat 2 is divided into a driver seat 2a and a front passenger seat 2b, a second-row seat 3 and a rearmost seat 4 are divided into a first seat 3a, 4a and a second seat 3b, 4b, the front passenger seat 2b and the second seat 4b of the rearmost seat 4 are configured so as to be foldable, and the second seat 3b of the second-row seat 3 is configured so as to be movable to the vicinity of the driver seat 2a and to the vicinity of the first seat 4a of the rearmost seat 4. Therefore, infants seated on the first seats 3a and 4a of the second-row seat 3 and the rearmost seat 4 can easily be taken care of and communicated with. Also, by moving the second seat 3b of the second-row seat to the vicinity of the driver seat 2a, communication with a driver can be provided easily.
대표청구항
▼
A front seat 2 is divided into a driver seat 2a and a front passenger seat 2b, a second-row seat 3 and a rearmost seat 4 are divided into a first seat 3a, 4a and a second seat 3b, 4b, the front passenger seat 2b and the second seat 4b of the rearmost seat 4 are configured so as to be foldable, and t
A front seat 2 is divided into a driver seat 2a and a front passenger seat 2b, a second-row seat 3 and a rearmost seat 4 are divided into a first seat 3a, 4a and a second seat 3b, 4b, the front passenger seat 2b and the second seat 4b of the rearmost seat 4 are configured so as to be foldable, and the second seat 3b of the second-row seat 3 is configured so as to be movable to the vicinity of the driver seat 2a and to the vicinity of the first seat 4a of the rearmost seat 4. Therefore, infants seated on the first seats 3a and 4a of the second-row seat 3 and the rearmost seat 4 can easily be taken care of and communicated with. Also, by moving the second seat 3b of the second-row seat to the vicinity of the driver seat 2a, communication with a driver can be provided easily. ttachment, (1.4.3.2.) said actuator reactor attached to said outer guide element attachment of said outer guide element, (1.4.3.3.) said actuator reactor positioned proximal to said actuator initiator when said energy absorbing structure is in said stowed position, (1.4.3.4.) said actuator reactor comprising means responsive to said repulsive force of said actuator force generation means; (1.5.) a plurality of compressible beams (6), said compressible beams comprising, (1.5.1.) a base beam portion comprising (1.5.1.1.) a rotational attachment end, (1.5.1.2.) a translational end, and (1.5.1.3.) a rotational joint (9), said rotational joint connected to said rotational attachment end of said base beam portion; (1.5.2.) an outer beam portion comprising (1.5.2.1.) a rotational attachment end, (1.5.2.2.) a translational end, and (1.5.2.3.) a rotational joint (9), said rotational joint connected to said rotational attachment end of said outer beam portion; (1.5.3.) a translational joint (8), (1.5.3.1.) said translation joint translationally coupled to said translational end of said outer beam portion and said translation end of said inner beam portion; (1.6.) said rotational joint of said base beam portion rotateably attached to one of said plurality of rotational beam attachments of said base rigid guide element; (1.7.) said rotational joint of said outer beam portion rotateably attached to one of said plurality of rotational beam attachments of said outer rigid guide element; (1.8.) at least one of said compressible beams further comprises locking means for locking at least one of said joints of said compressible beam; (2.) said energy absorbing structure further comprises a principal axis of deployment, said principal axis of deployment being generally aligned to a principal axis of movement between said bodies moving with said relative motion. 2. The device for absorbing impact, according to claim 1, wherein: said rigid guide elements (7) take the form of elongated bodies which extend in a plane substantially perpendicular to said principal axis of movement between said bodies moving with said, relative motion. 3. The device for absorbing impact according to claim 1, wherein: said translation joints (8) further comprise means of translation of said compressible beam parallel to a longitudinal axis of said compressible beams. 4. The device for absorbing impact, according to claim 1, wherein: said rotational joints (9) of said compressible beams (6) comprise means of rotation of said compressible beams around an axis which is fixed, or mobile in the perpendicular to a longitudinal axis of the compressible beams, respectively. 5. The device for absorbing impact, according to claim 1, wherein: at least some of said compressible beams (6) further comprise (1.) means of telescopically mating said outer beam portion into said base beam portion, (2.) means of collapsing said outer beam portion into said base beam portion. 6. The device for absorbing impact, according to claim 1, wherein: said energy absorbing structure (3) further comprises (1.) a three-dimensional shape, (2.) means to resist mechanical forces, said mechanical forces selected from the group consisting of lateral forces, transversal forces and axial forces. 7. The device for absorbing impact, according to claim 1, wherein: said actuators (4) are explosive thrusters, (1.) said explosive thrusters comprise a piston portion and a body portion, (1.1.) said piston portion being preferably separable from said body portion of said thruster when said piston portion is extended. 8. The device for absorbing impact, according to claim 1, wherein: (1.) said actuator (4) is a thruster, (2.) said thruster comprising a body and a shaft, (2.1.) said body of said thruster attached to a thruster body attachment of said device for absorbing impact, (2.1.1.) said thruster body attachment chosen from the group
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