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Inward opening type opening mechanism of airplane cabin door
The invention discloses an aircraft cabin door inward opening type opening mechanism which comprises a cabin door, a connecting support, an adjusting connecting rod, an actuator cylinder and a connecting body, the cabin door comprises a first cabin door body and a second cabin door body, and the connecting support comprises a connecting rod fixing support, a fuselage support, a first cabin door support, a second cabin door support, an actuator cylinder support and a door frame support. The second cabin door support is arranged on one side of the second cabin door, one end of the adjusting connecting rod is arranged on the second cabin door support, and the connecting rod fixing support is arranged at the other end of the adjusting connecting rod; one end of the actuating cylinder is arranged on the second cabin door; according to the technical scheme, the second cabin door support is arranged on one side of the second cabin door, one end of the adjusting connecting rod is arranged on the second cabin door support, and the connecting rod fixing support is arranged at the other end of the adjusting connecting rod; and one end of the actuating cylinder is arranged on the second cabin door, so that the influence of opening the cabin door in the aircraft flight process on aircraft driving is reduced, and the internal space of the cabin is fully utilized.
本发明公开了一种飞机舱门内开式开启机构,包括舱门、连接支座、调节连杆、作动筒和连接体,所述舱门包括第一舱门和第二舱门,所述连接支座包括连杆固定支座、机身支座、第一舱门支座、第二舱门支座、作动筒支座和门框支座,第二舱门支座设置于第二舱门的一侧,调节连杆的一端设置于第二舱门支座上,所述连杆固定支座设置于调节连杆的另一端;所述作动筒的一端设置于第二舱门上;采用上述技术方案,由于第二舱门支座设置于第二舱门的一侧,调节连杆的一端设置于第二舱门支座上,所述连杆固定支座设置于调节连杆的另一端;所述作动筒的一端设置于第二舱门上,使得减少飞机飞行过程中打开舱门影响飞机驾驶且充分利用机舱内部空间。
Inward opening type opening mechanism of airplane cabin door
The invention discloses an aircraft cabin door inward opening type opening mechanism which comprises a cabin door, a connecting support, an adjusting connecting rod, an actuator cylinder and a connecting body, the cabin door comprises a first cabin door body and a second cabin door body, and the connecting support comprises a connecting rod fixing support, a fuselage support, a first cabin door support, a second cabin door support, an actuator cylinder support and a door frame support. The second cabin door support is arranged on one side of the second cabin door, one end of the adjusting connecting rod is arranged on the second cabin door support, and the connecting rod fixing support is arranged at the other end of the adjusting connecting rod; one end of the actuating cylinder is arranged on the second cabin door; according to the technical scheme, the second cabin door support is arranged on one side of the second cabin door, one end of the adjusting connecting rod is arranged on the second cabin door support, and the connecting rod fixing support is arranged at the other end of the adjusting connecting rod; and one end of the actuating cylinder is arranged on the second cabin door, so that the influence of opening the cabin door in the aircraft flight process on aircraft driving is reduced, and the internal space of the cabin is fully utilized.
本发明公开了一种飞机舱门内开式开启机构,包括舱门、连接支座、调节连杆、作动筒和连接体,所述舱门包括第一舱门和第二舱门,所述连接支座包括连杆固定支座、机身支座、第一舱门支座、第二舱门支座、作动筒支座和门框支座,第二舱门支座设置于第二舱门的一侧,调节连杆的一端设置于第二舱门支座上,所述连杆固定支座设置于调节连杆的另一端;所述作动筒的一端设置于第二舱门上;采用上述技术方案,由于第二舱门支座设置于第二舱门的一侧,调节连杆的一端设置于第二舱门支座上,所述连杆固定支座设置于调节连杆的另一端;所述作动筒的一端设置于第二舱门上,使得减少飞机飞行过程中打开舱门影响飞机驾驶且充分利用机舱内部空间。
Inward opening type opening mechanism of airplane cabin door
一种飞机舱门内开式开启机构
LAO SHANLIN (Autor:in) / CHEN DONG (Autor:in) / CHEN LIN (Autor:in) / CUI RUIQIN (Autor:in) / ZHONG WENXIN (Autor:in) / WANG GANG (Autor:in) / WANG HONGMEI (Autor:in)
16.08.2024
Patent
Elektronische Ressource
Chinesisch
IPC:
E05F
DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION
,
Vorrichtungen zum Bewegen der Flügel in die Offen- oder Schließstellung
/
B64C
AEROPLANES
,
Flugzeuge
/
E05D
Scharniere oder andere Aufhängevorrichtungen für Türen, Fenster oder Flügel
,
HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS, OR WINGS
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