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1. 发明申请

WO1982001854A1 VEHICLE CRASHWORTHY SEAT 审中-公开
标题翻译：车辆CRASHWORTHY座椅
公开(公告)号：WO1982001854A1
公开(公告)日：1982-06-10
申请号：PCT/US1981001625
申请日：1981-12-07
申请人： BOEING CO
发明人： BOEING CO , CAMPBELL RICHARD F
IPC分类号： B60R21/10
CPC分类号： B60N2/42736 , B60N2/4242 , B64D11/0689 , B64D25/04
摘要： Un siege d'anti-ecrasement pour un membre d'equipage d'un helicoptere comprend un baquet (12) relie a une structure de support (18) par un attenuateur d'energie reglable (44) du type a flexion de cable. L'attenuateur comprend un cadre (46) porte par le baquet, trois cables metalliques paralleles verticaux (68, 70, 72) relies aux extremites opposees au cadre de l'attenuateur, et un assemblage a chariot (74) fixe sur la structure de support contenant trois jeux de trois rouleaux (86, 88, 90), tournant autour de trois axes horizontaux espaces verticalement, autour desquels les trois cables sont plies et deplies lorsque le baquet subit une collision vers le bas lors d'un ecrasement de l'helicoptere. Les deux rouleaux inferieurs de deux de ces ensembles de trois rouleaux sont deplacables le long de leurs axes entre une position engagee et une position degagee par rapport a un cable associe a ces rouleaux. Ces rouleaux deplacables sont connectes a un mecanisme d'ajustement de l'attenuateur a fonctionnement manuel (126) ayant un reglage maximum sur lequel tous les rouleaux sont engages avec leurs cables associes, un reglage intermediaire sur lequel seulement deux des trois ensembles de trois rouleaux sont engages avec leurs cables associes, et un reglage minimum sur lequel seulement un cable est engage avec l'ensemble de trois rouleaux qui n'est pas connecte au mecanisme d'ajustement. En selectionnant un reglage maximum, un reglage intermediaire et un reglage minimum du mecanisme d'ajustement en fonction du poids de l'occupant du siege, la distance de collision maximum du siege est reduite sans nuire a la protection assuree a l'occupant du siege contre les forces dangereuses d'acceleration.

2. 发明专利

DE3152570A1 未知
公开(公告)号：DE3152570A1
公开(公告)日：1983-01-13
申请号：DE3152570
申请日：1981-12-07
申请人： BOEING CO
发明人： CAMPBELL RICHARD F
IPC分类号： B60R21/10

3. 发明专利

IT8112697D0 未知
公开(公告)号：IT8112697D0
公开(公告)日：1981-12-04
申请号：IT1269781
申请日：1981-12-04
申请人： BOEING CO
发明人： CAMPBELL RICHARD F
IPC分类号： B60N2/42 , B60N2/427 , B64D11/06 , B64D25/04 , B64D
摘要： A crashworthy helicopter crew seat, which includes a seat bucket connected to a support structure by an adjustable energy attenuator of the wire bending type. The attenuator includes a frame carried by the seat bucket, three parallel, vertically disposed wires connected at opposite ends to the attenuator frame, and a trolley assembly affixed to the support structure containing three sets of three rollers, rotatable about three vertically spaced horizontal axes, about which the three wires are respectfully bent and unbent as the seat bucket strokes downward during a crash of the helicopter. The lower two rollers of two of these sets of three rollers are displaceable along their axes between an engaged position and a disengaged position relative to a wire associated with these rollers. These displaceable rollers are connected to a manually operated attenuator adjustment mechanism having a maximum setting at which all rollers are engaged with their associated wires, an intermediate setting at which only two of the three sets of three rollers are engaged with their associated wires, and a minimum setting at which only one wire is engaged with the set of three rollers which is not connected to the adjustment mechanism. By selecting a maximum, intermediate, and minimum settings of the adjustment mechanism in accordance with the weight of the seat occupant, the maximum stroke distance of the seat is reduced without detrimentally affecting the protection afforded the occupant of the seat against dangerous acceleration forces.

4. 发明专利

DE3152570C2 未知
公开(公告)号：DE3152570C2
公开(公告)日：1992-07-30
申请号：DE3152570
申请日：1981-12-07
申请人： BOEING CO
发明人： CAMPBELL RICHARD F
IPC分类号： B60N2/42 , B60N2/427 , B64D11/06 , B64D25/04
摘要： A crashworthy helicopter crew seat, which includes a seat bucket connected to a support structure by an adjustable energy attenuator of the wire bending type. The attenuator includes a frame carried by the seat bucket, three parallel, vertically disposed wires connected at opposite ends to the attenuator frame, and a trolley assembly affixed to the support structure containing three sets of three rollers, rotatable about three vertically spaced horizontal axes, about which the three wires are respectfully bent and unbent as the seat bucket strokes downward during a crash of the helicopter. The lower two rollers of two of these sets of three rollers are displaceable along their axes between an engaged position and a disengaged position relative to a wire associated with these rollers. These displaceable rollers are connected to a manually operated attenuator adjustment mechanism having a maximum setting at which all rollers are engaged with their associated wires, an intermediate setting at which only two of the three sets of three rollers are engaged with their associated wires, and a minimum setting at which only one wire is engaged with the set of three rollers which is not connected to the adjustment mechanism. By selecting a maximum, intermediate, and minimum settings of the adjustment mechanism in accordance with the weight of the seat occupant, the maximum stroke distance of the seat is reduced without detrimentally affecting the protection afforded the occupant of the seat against dangerous acceleration forces.

5. 发明专利

IT1205451B 未知
公开(公告)号：IT1205451B
公开(公告)日：1989-03-23
申请号：IT1269781
申请日：1981-12-04
申请人： BOEING CO
发明人： CAMPBELL RICHARD F
IPC分类号： B60N2/42 , B60N2/427 , B64D11/06 , B64D25/04 , B64D
摘要： A crashworthy helicopter crew seat, which includes a seat bucket connected to a support structure by an adjustable energy attenuator of the wire bending type. The attenuator includes a frame carried by the seat bucket, three parallel, vertically disposed wires connected at opposite ends to the attenuator frame, and a trolley assembly affixed to the support structure containing three sets of three rollers, rotatable about three vertically spaced horizontal axes, about which the three wires are respectfully bent and unbent as the seat bucket strokes downward during a crash of the helicopter. The lower two rollers of two of these sets of three rollers are displaceable along their axes between an engaged position and a disengaged position relative to a wire associated with these rollers. These displaceable rollers are connected to a manually operated attenuator adjustment mechanism having a maximum setting at which all rollers are engaged with their associated wires, an intermediate setting at which only two of the three sets of three rollers are engaged with their associated wires, and a minimum setting at which only one wire is engaged with the set of three rollers which is not connected to the adjustment mechanism. By selecting a maximum, intermediate, and minimum settings of the adjustment mechanism in accordance with the weight of the seat occupant, the maximum stroke distance of the seat is reduced without detrimentally affecting the protection afforded the occupant of the seat against dangerous acceleration forces.

6. 发明专利

DE3152570T1 未知
公开(公告)号：DE3152570T1
公开(公告)日：1983-01-13
申请号：DE3152570
申请日：1981-12-07
申请人： BOEING CO
发明人： CAMPBELL RICHARD F
IPC分类号： B60N2/42 , B60N2/427 , B64D11/06 , B64D25/04 , B60R21/10
摘要： A crashworthy helicopter crew seat, which includes a seat bucket connected to a support structure by an adjustable energy attenuator of the wire bending type. The attenuator includes a frame carried by the seat bucket, three parallel, vertically disposed wires connected at opposite ends to the attenuator frame, and a trolley assembly affixed to the support structure containing three sets of three rollers, rotatable about three vertically spaced horizontal axes, about which the three wires are respectfully bent and unbent as the seat bucket strokes downward during a crash of the helicopter. The lower two rollers of two of these sets of three rollers are displaceable along their axes between an engaged position and a disengaged position relative to a wire associated with these rollers. These displaceable rollers are connected to a manually operated attenuator adjustment mechanism having a maximum setting at which all rollers are engaged with their associated wires, an intermediate setting at which only two of the three sets of three rollers are engaged with their associated wires, and a minimum setting at which only one wire is engaged with the set of three rollers which is not connected to the adjustment mechanism. By selecting a maximum, intermediate, and minimum settings of the adjustment mechanism in accordance with the weight of the seat occupant, the maximum stroke distance of the seat is reduced without detrimentally affecting the protection afforded the occupant of the seat against dangerous acceleration forces.

7. 发明公开

EP0065982A4 VEHICLE CRASHWORTHY SEAT. 失效
标题翻译：事故车辆座椅。
公开(公告)号：EP0065982A4
公开(公告)日：1984-04-17
申请号：EP82900240
申请日：1981-12-07
申请人： BOEING CO
发明人： CAMPBELL RICHARD F
IPC分类号： B60N2/42 , B60N2/427 , B64D11/06 , B64D25/04 , B60R21/10
CPC分类号： B60N2/42736 , B60N2/4242 , B64D11/0689 , B64D25/04

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