CN113685101B - A outer handle mechanism, emergent hatch door and aircraft for out-turning formula emergent hatch door - Google Patents
A outer handle mechanism, emergent hatch door and aircraft for out-turning formula emergent hatch door Download PDFInfo
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- CN113685101B CN113685101B CN202111025737.5A CN202111025737A CN113685101B CN 113685101 B CN113685101 B CN 113685101B CN 202111025737 A CN202111025737 A CN 202111025737A CN 113685101 B CN113685101 B CN 113685101B
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- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05C—BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
- E05C19/00—Other devices specially designed for securing wings, e.g. with suction cups
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
- B64C1/1407—Doors; surrounding frames
- B64C1/1423—Passenger doors
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- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05C—BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
- E05C19/00—Other devices specially designed for securing wings, e.g. with suction cups
- E05C19/10—Hook fastenings; Fastenings in which a link engages a fixed hook-like member
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Abstract
Description
技术领域technical field
本发明涉及用于外翻式应急舱门的外手柄机构、应急舱门及飞行器,属于飞行器机构设计领域。The invention relates to an outer handle mechanism for an eversion-type emergency cabin door, an emergency cabin door and an aircraft, and belongs to the field of aircraft mechanism design.
背景技术Background technique
民用飞机外翻式应急舱门作为飞机应急情况下客舱内乘客逃生的重要出口,在满足CCAR-25-R4中相关条款要求的前提下,为保证外翻式应急舱门能够正常的打开和关闭,最大限度地减低乘客的伤害程度,提高人员的生还率,设计一种可与内手柄无联动关系且安全可靠的外手柄机构显得十分必要。As an important exit for passengers in the passenger cabin to escape in the event of an aircraft emergency, the everted emergency hatch of civil aircraft, on the premise of meeting the requirements of the relevant clauses in CCAR-25-R4, in order to ensure that the everted emergency hatch can be opened and closed normally. It is necessary to design a safe and reliable outer handle mechanism that can be unlinked with the inner handle to minimize the injury degree of passengers and improve the survival rate of personnel.
目前,作为上述外手柄机构,例如有专利文献CN106741833B(以下称“专利文献1”)公开的外手柄机构,其具有:包括驱动曲柄和曲柄锁钩的曲柄锁钩机构;经由连杆、曲柄、插耳连杆改变曲柄锁钩与驱动曲柄的离合状态(外手柄与内手柄的离合状态)的次级翻板;以及用于使次级翻板成为能操作上述离与合的翻板整体打开状态的初级翻板。At present, as the above-mentioned outer handle mechanism, for example, there is an outer handle mechanism disclosed in Patent Document CN106741833B (hereinafter referred to as "
并且,在专利文献1的外手柄机构中,次级翻板与初级翻板铰接,在铰接位置处通过扭簧使初级翻板和次级翻板保持相对固定的位置;次级翻板与外手柄主结构件之间用两根拉伸弹簧相连;初级翻板铰接在外手柄主结构件上,并在铰接位置处通过两个扭簧与外手柄主结构件保持相对固定的位置关系。In addition, in the outer handle mechanism of
发明内容SUMMARY OF THE INVENTION
发明所要解决的技术问题The technical problem to be solved by the invention
然而,尤其考虑到实际中可能存在的加工误差及飞机部件要求的装配精度,专利文献1的外手柄机构结构复杂,部件数量多,加工和维修难度大。而且,专利文献1的离合机构驱动零件与手柄锁定机构驱动零件通过弹簧铰接于一起,使加工和维修难度进一步增加。However, especially considering the possible machining errors in practice and the assembly accuracy required for aircraft components, the outer handle mechanism of
鉴于上述问题,本发明提供一种用于外翻式应急舱门的外手柄机构,其能够实现舱门的打开和关闭,能够实现内外手柄的离合功能,具有手柄锁定功能,安全可靠并能降低设计和加工难度。并且,本发明还提供一种具有上述外手柄机构的应急舱门以及具有该应急舱门的飞行器。In view of the above problems, the present invention provides an outer handle mechanism for an eversion-type emergency cabin door, which can realize the opening and closing of the cabin door, realize the clutch function of the inner and outer handles, has the handle locking function, is safe and reliable, and can reduce the Design and processing difficulty. In addition, the present invention also provides an emergency hatch having the above-mentioned outer handle mechanism and an aircraft having the emergency hatch.
解决技术问题所采用的技术方案Technical solutions adopted to solve technical problems
本发明的一形态的用于外翻式应急舱门的外手柄机构,包括:手柄主体,该手柄主体与固定于舱门主体的锁轴铰接;驱动曲柄,该驱动曲柄与所述锁轴固接;曲柄锁钩,该曲柄锁钩与所述手柄主体铰接,且能与所述驱动曲柄相合以及相离;离合摇臂,该离合摇臂与所述手柄主体铰接,并经由连杆与所述曲柄锁钩铰接,且被第一弹性构件施加打开方向或关闭方向的载荷而经由连杆使曲柄锁钩与驱动曲柄相合或相离;以及开启盖板,该开启盖板独立于所述离合摇臂地与所述手柄主体铰接,且能通过相对于所述手柄主体转动而在与设置于舱门主体的舱门侧锁钩锁定以限制手柄主体的运动的关闭状态和与所述舱门侧锁钩脱开以允许手柄主体的运动的打开状态之间切换。An outer handle mechanism for an eversion-type emergency hatch according to one aspect of the present invention includes: a handle body, which is hinged to a lock shaft fixed to the hatch body; a drive crank, which is fixed to the lock shaft A crank lock hook, which is hinged with the handle body, and can be engaged with and separated from the drive crank; a clutch rocker arm, which is hinged with the handle body and connected to the handle body via a connecting rod. The crank lock hook is hinged, and a load in the opening direction or the closing direction is applied by the first elastic member to make the crank lock hook engage or separate from the driving crank via a connecting rod; and an opening cover plate is independent of the clutch. The rocker arm is hingedly connected to the handle body, and can be locked with a door-side latch provided on the door body by being rotated relative to the handle body to limit the movement of the handle body in a closed state and with the door The side lock hooks are disengaged to allow movement of the handle body to switch between open states.
根据本发明的一形态的用于外翻式应急舱门的外手柄机构,离合机构与开启盖板机构完全独立,该设计方式简化了外手柄机构,降低了零件的加工难度。According to one aspect of the present invention, the outer handle mechanism for the eversion-type emergency hatch is completely independent of the clutch mechanism and the cover opening mechanism. This design method simplifies the outer handle mechanism and reduces the processing difficulty of the parts.
上述外手柄机构也可以是,所述开启盖板被第二弹性构件施加载荷而始终趋向于限制手柄主体的运动。In the above-mentioned outer handle mechanism, the opening cover plate may always tend to restrict the movement of the handle body by being loaded by the second elastic member.
根据上述结构的外手柄机构,第二弹性构件施加载荷始终使开启盖板趋向于关闭,保证例如无人员操作时盖板始终关闭,手柄始终处于锁定状态,从而防止外手柄因外力干扰而翻转。According to the outer handle mechanism of the above structure, the second elastic member always exerts a load to make the opening cover tend to be closed, ensuring that the cover is always closed and the handle is always in a locked state when there is no human operation, thereby preventing the outer handle from turning over due to external force interference.
上述外手柄机构也可以是,所述手柄主体具有贯通所述手柄主体的第一贯通部,所述开启盖板的至少一部分经由所述第一贯通部向所述手柄主体的外侧露出。In the outer handle mechanism, the handle body may have a first penetration portion penetrating the handle body, and at least a part of the open cover may be exposed to the outside of the handle body via the first penetration portion.
根据上述结构的外手柄机构,例如,操作人员能容易地对抗第二弹性构的施加载荷而使开启盖板成为允许手柄主体的运动的打开状态,例如能容易地从手柄主体的外侧经由第一贯通部对开启盖板向里侧施力。According to the outer handle mechanism of the above structure, for example, the operator can easily oppose the applied load of the second elastic mechanism to bring the opening cover into the open state that allows the movement of the handle body, for example, can easily pass the first handle from the outside of the handle body. The penetration portion urges the opening cover inward.
上述外手柄机构也可以是,所述锁轴的旋转轴线、所述曲柄锁钩的旋转轴线、所述离合摇臂的旋转轴线和所述开启盖板的旋转轴线中,至少所述锁轴的旋转轴线、所述曲柄锁钩的旋转轴线和所述离合摇臂的旋转轴线相互平行。The above-mentioned outer handle mechanism may also be such that among the rotation axis of the lock shaft, the rotation axis of the crank lock hook, the rotation axis of the clutch rocker arm and the rotation axis of the cover opening, at least the rotation axis of the lock shaft is The rotation axis, the rotation axis of the crank lock hook and the rotation axis of the clutch rocker arm are parallel to each other.
上述外手柄机构也可以是,所述手柄主体具有:手柄基部;以及两个支承部,该两个支承部在所述外手柄机构的里侧从所述手柄基部向与所述锁轴的轴向正交的第一方向延伸,并在与所述轴向以及第一方向正交的第二方向扩展,且在所述轴向上隔开间隔相对,所述开启盖板、所述离合摇臂、所述曲柄锁钩和所述锁轴依次沿所述第二方向排列地设置在两个所述支承部之间,且分别与两个所述支承部铰接。In the above-mentioned outer handle mechanism, the handle main body may have: a handle base; and two support parts that extend from the handle base to an axis with the lock shaft on the rear side of the outer handle mechanism. extend in a first orthogonal direction, expand in a second direction orthogonal to the axial direction and the first direction, and are opposite to each other at an interval in the axial direction, the opening cover plate, the clutch rocker The arm, the crank lock hook and the lock shaft are arranged in sequence along the second direction between the two support parts, and are respectively hinged with the two support parts.
上述外手柄机构也可以是,所述手柄主体具有贯通所述手柄主体的第二贯通部,通过所述离合摇臂与所述手柄主体的相对转动,所述离合摇臂的前端部穿过所述第二贯通部向所述手柄主体的外侧突出。The outer handle mechanism may also be such that the handle body has a second penetration portion penetrating the handle body, and the front end portion of the clutch rocker arm passes through the handle body through the relative rotation of the clutch rocker arm and the handle body. The second penetration portion protrudes to the outside of the handle body.
根据上述结构的外手柄机构,例如,操作人员能容易地从手柄主体的外侧经由上述连杆等使曲柄锁钩与驱动曲柄相合或相离,同时能减少外手柄机构整体上在垂直于锁轴的轴向的方向、例如外手柄机构的高度方向上的尺寸,进一步紧凑地构成外手柄机构。According to the outer handle mechanism of the above structure, for example, the operator can easily make the crank lock hook engage or separate from the drive crank via the above-mentioned connecting rod or the like from the outside of the handle main body, and at the same time, it is possible to reduce the overall operation of the outer handle mechanism perpendicular to the lock shaft. The dimension in the axial direction of the outer handle mechanism, for example, the height direction of the outer handle mechanism, makes the outer handle mechanism more compact.
上述外手柄机构也可以是,所述外手柄机构还包括第一调节机构,该第一调节机构能在与开启盖板的旋转轴线垂直的方向上对所述舱门侧锁钩与所述开启盖板锁定时所述开启盖板相对于所述舱门主体的相对位置进行调节,从而实现对所述手柄主体相对于所述舱门主体的相对位置进行调节。The above-mentioned outer handle mechanism may also be that, the outer handle mechanism further includes a first adjustment mechanism, and the first adjustment mechanism can adjust the door side lock hook and the open door in a direction perpendicular to the rotation axis of the opening cover plate. When the cover plate is locked, the relative position of the open cover plate relative to the cabin door body is adjusted, so as to realize the adjustment of the relative position of the handle main body relative to the cabin door main body.
根据上述结构的外手柄机构,开启盖板与舱门侧锁钩配合,可实现外手柄机构的锁定和阶差调节功能。According to the outer handle mechanism of the above structure, the opening cover is matched with the side lock hook of the cabin door, so that the locking and step adjustment functions of the outer handle mechanism can be realized.
上述外手柄机构也可以是,所述第一调节机构包括锁钩法兰和两个第一螺纹构件,所述舱门侧锁钩在前端具有与所述开启盖板进行锁定的第一部分,在基端具有外周面形成有螺纹的圆柱状的第二部分,所述舱门侧锁钩经由所述锁钩法兰固定于所述舱门主体,所述锁钩法兰能滑动地嵌套在所述舱门侧锁钩的第二部分的外周,两个所述第一螺纹构件分别与形成于所述第二部分的外周面的螺纹结合,且从两侧直接或间接地与所述锁钩法兰抵接。The above-mentioned outer handle mechanism may also be that, the first adjustment mechanism includes a lock hook flange and two first threaded members, and the hatch side lock hook has a first part at the front end that is locked with the open cover plate, The base end has a cylindrical second portion whose outer peripheral surface is threaded, and the door-side lock hook is fixed to the door body via the lock hook flange slidably nested in the lock hook flange. On the outer circumference of the second part of the door-side lock hook, the two first threaded members are respectively combined with the threads formed on the outer circumference of the second part, and are directly or indirectly connected to the lock from both sides. Hook flange abuts.
根据上述结构的外手柄机构,开启盖板与舱门侧锁钩配合,能进一步可靠地实现外手柄的锁定和阶差调节功能并抑制零件的加工难度增加。舱门侧锁钩与舱门主体间采用螺纹连接,可通过上述第一螺纹构件等调节舱门侧锁钩与开启盖板锁定时开启盖板相对于舱门主体的相对位置,对手柄阶差进行调节。According to the outer handle mechanism of the above structure, the opening cover is matched with the door side lock hook, the locking and step adjustment functions of the outer handle can be further reliably realized and the increase in the processing difficulty of the parts can be suppressed. The side lock hook of the cabin door and the main body of the cabin door are connected by threaded connection, and the relative position of the open cover plate relative to the main body of the cabin door when the lock hook of the cabin door side and the open cover plate can be adjusted through the above-mentioned first threaded member, etc. Make adjustments.
上述外手柄机构也可以是,在两个所述第一螺纹构件与所述锁钩法兰之间分别夹设有锁钩衬套。In the above-mentioned outer handle mechanism, a lock hook bushing may be sandwiched between the two first threaded members and the lock hook flange, respectively.
上述外手柄机构也可以是,所述手柄主体具有能沿所述锁轴的周向与所述驱动曲柄直接或间接抵接而对所述驱动曲柄进行支承的抵接接受部,所述外手柄机构还包括第二调节机构,该第二调节机构对所述抵接接受部与所述驱动曲柄在抵接时的相对位置进行调节。In the above-mentioned outer handle mechanism, the handle body may have an abutment receiving portion capable of directly or indirectly abutting with the drive crank in the circumferential direction of the lock shaft to support the drive crank, and the outer handle may The mechanism further includes a second adjustment mechanism that adjusts the relative position of the abutment receiving portion and the drive crank when they are in abutment.
根据上述结构的外手柄机构,手柄主体和驱动曲柄抵接时的相对位置可由第二调节机构调节,可方便外手柄机构与锁轴旋转角度关系的调节,降低手柄主体和驱动曲柄的加工难度。According to the outer handle mechanism of the above structure, the relative position of the handle body and the driving crank can be adjusted by the second adjusting mechanism, which can facilitate the adjustment of the rotation angle relationship between the outer handle mechanism and the lock shaft, and reduce the processing difficulty of the handle body and the driving crank.
上述外手柄机构也可以是,所述第二调节机构包括:贯穿所述驱动曲柄的孔部;以及与所述孔部中螺纹结合而能与所述抵接接受部抵接的螺钉。In the above-mentioned outer handle mechanism, the second adjustment mechanism may include: a hole portion penetrating the drive crank; and a screw threadedly coupled with the hole portion and capable of abutting with the abutment receiving portion.
根据上述结构的外手柄机构,可通过上述螺钉和孔部调节手柄主体和驱动曲柄间的间隙,能进一步可靠地方便外手柄与锁轴旋转角度关系的调节并抑制零件的加工难度增加。According to the outer handle mechanism of the above structure, the clearance between the handle main body and the driving crank can be adjusted through the screw and the hole, which can further reliably facilitate the adjustment of the rotational angle relationship between the outer handle and the lock shaft and restrain the increase in machining difficulty of the parts.
本发明的一形态的应急舱门,具有上述任一种外手柄机构。An emergency hatch according to one aspect of the present invention has any one of the above-mentioned outside handle mechanisms.
本发明的一形态的飞行器,具有上述应急舱门。An aircraft according to one aspect of the present invention has the above-mentioned emergency hatch.
发明效果Invention effect
根据本发明的外翻式应急舱门的外手柄机构、应急舱门和飞行器,能够实现舱门的打开和关闭,能够实现内外手柄的离合功能,具有手柄锁定功能,该外手柄机构符合CCAR-25-R4第25.783相关条款要求,例如用于飞机舱门机构设计领域。本发明的外手柄机构的离合机构与开启盖板机构完全独立,该设计方式简化了外手柄机构,降低了零件的加工难度。The outer handle mechanism of the everted emergency cabin door, the emergency cabin door and the aircraft according to the present invention can realize the opening and closing of the cabin door, realize the clutch function of the inner and outer handles, and have the handle locking function, and the outer handle mechanism conforms to the CCAR- 25-R4 Section 25.783, for example, in the field of aircraft door mechanism design. The clutch mechanism of the outer handle mechanism of the present invention is completely independent from the cover opening mechanism, and the design method simplifies the outer handle mechanism and reduces the processing difficulty of the parts.
附图说明Description of drawings
图1a是示意性示出本发明一实施方式的用于外翻式应急舱门的外手柄机构的剖视图,图中外手柄处于打开状态且离合机构处于“离”状态。Fig. 1a is a cross-sectional view schematically showing an outer handle mechanism for an everted emergency hatch according to an embodiment of the present invention, in which the outer handle is in an open state and the clutch mechanism is in a "disengaged" state.
图1b是示意性示出本发明一实施方式的用于外翻式应急舱门的外手柄机构的锁钩结构的剖视图。Fig. 1b is a cross-sectional view schematically showing a lock hook structure of an outer handle mechanism for an everted emergency hatch according to an embodiment of the present invention.
图2是示意性示出本发明一实施方式的用于外翻式应急舱门的外手柄机构的剖视图,图中外手柄处于打开状态且离合机构处于“合”状态。Fig. 2 is a cross-sectional view schematically showing an outer handle mechanism for an everted emergency hatch according to an embodiment of the present invention, in which the outer handle is in an open state and the clutch mechanism is in a "closed" state.
图3是示出本发明一实施方式的用于外翻式应急舱门的外手柄机构的立体图,图中外手柄处于关闭状态且离合机构处于“离”状态。3 is a perspective view showing an outer handle mechanism for an everted emergency hatch according to an embodiment of the present invention, in which the outer handle is in a closed state and the clutch mechanism is in a “disengaged” state.
图4是示出本发明一实施方式的用于外翻式应急舱门的外手柄机构的开启盖板机构的立体图。4 is a perspective view showing a cover opening mechanism of an outer handle mechanism for an eversion-type emergency hatch according to an embodiment of the present invention.
图5a是示出本发明一实施方式的用于外翻式应急舱门的外手柄机构的锁钩结构的立体图。Fig. 5a is a perspective view showing a lock hook structure of an outer handle mechanism for an eversion-type emergency hatch according to an embodiment of the present invention.
图5b是示出本发明一实施方式的用于外翻式应急舱门的外手柄机构的锁钩结构的剖视图。Fig. 5b is a cross-sectional view showing a lock hook structure of an outer handle mechanism for an everted emergency hatch according to an embodiment of the present invention.
图6是示出本发明一实施方式的用于外翻式应急舱门的外手柄机构的离合机构的立体图。6 is a perspective view showing a clutch mechanism of an outer handle mechanism for an eversion-type emergency hatch according to an embodiment of the present invention.
图7是打开装设有本发明一实施方式的用于外翻式应急舱门的外手柄机构的舱门工作流程。FIG. 7 is a working flow of opening a hatch equipped with an outer handle mechanism for an everted emergency hatch according to an embodiment of the present invention.
图8是关闭装设有本发明一实施方式的用于外翻式应急舱门的外手柄机构的舱门关闭流程。FIG. 8 is a process of closing the hatch provided with the outer handle mechanism for the eversion-type emergency hatch according to an embodiment of the present invention.
图9示意性示出一实施方式的沿轴向观察第二衬套在与锁钩脱开后返回锁定状态的情况下的第二衬套与锁钩的位置关系的图。FIG. 9 is a diagram schematically showing the positional relationship between the second bushing and the locking hook when the second bushing returns to the locked state after being disengaged from the locking hook in an axial direction according to an embodiment.
(符号说明)(Symbol Description)
1手柄基部;1 handle base;
1a第一贯通部;1a the first penetration part;
2开启盖板;2 Open the cover;
3第一销轴;3 The first pin;
4扭簧;4 torsion springs;
5第一衬套;5 first bushing;
6第二衬套;6 second bushing;
7第二销轴;7 The second pin;
8锁钩;8 lock hooks;
9锁钩法兰;9 locking hook flange;
10锁钩调节螺母;10 lock hook adjustment nut;
11锁钩衬套,11 shackle bushing,
12曲柄锁钩;12 crank lock hook;
13连杆;13 connecting rods;
14第三销轴;14 The third pin;
15拉簧;15 tension spring;
16第四销轴;16 fourth pin;
17离合摇臂;17 clutch rocker arm;
18驱动曲柄;18 drive crank;
19螺钉;19 screws;
20锁轴20 lock shaft
具体实施方式Detailed ways
下面结合具体实施例和附图对本发明作进一步说明,在以下的描述中阐述了更多的细节以便于充分理解本发明,但是本发明显然能够以多种不同于此描述的其它方式来实施,本领域技术人员可以在不违背本发明内涵的情况下根据实际应用情况作类似推广、演绎,因此不应以此具体实施例的内容限制本发明的保护范围。The present invention will be further described below with reference to specific embodiments and accompanying drawings. More details are set forth in the following description to facilitate a full understanding of the present invention, but it is obvious that the present invention can be implemented in many other ways that are different from those described herein. Those skilled in the art can make similar promotion and deduction according to the actual application situation without violating the connotation of the present invention, so the content of this specific embodiment should not limit the protection scope of the present invention.
以下,如无特殊说明,将锁轴的轴线延伸的方向简称为“轴向”,将绕轴向的周方向简称为“周向”,外手柄机构的“里侧”表示外手柄机构装设于舱门时从外手柄机构朝舱门的方向,外手柄机构的“外侧”表示外手柄机构装设于舱门时从外手柄机构离开舱门的方向。Hereinafter, unless otherwise specified, the direction in which the axis of the lock shaft extends is referred to as "axial direction", and the circumferential direction around the axial direction is referred to as "circumferential direction". The direction from the outer handle mechanism to the cabin door when the cabin door is used, and the "outside" of the outer handle mechanism means the direction from the outer handle mechanism to leave the cabin door when the outer handle mechanism is installed on the cabin door.
实施方式1
图1a是示意性示出本发明实施方式1的用于外翻式应急舱门的外手柄机构(以下,有时简称“外手柄”)100的剖视图,图中外手柄处于打开状态且离合机构C处于“离”状态。图3是示出本发明实施方式的用于外翻式应急舱门的外手柄机构100的立体图,图中外手柄处于关闭状态且离合机构C处于“离”状态。如图1a、3所示,外手柄主要包括手柄主结构A、开启盖板机构B和离合机构C。1a is a cross-sectional view schematically illustrating an outer handle mechanism (hereinafter, sometimes referred to as “outer handle”) 100 for an everted emergency hatch according to
手柄主结构A包括手柄基部1和两个支承部1b。本实施方式中,手柄基部1形成为纵长的大致板状,手柄基部1的长度方向(第二方向)与轴向正交或大致正交。手柄主结构A与固定于舱门主体且用于开启、关闭舱门的锁轴20铰接,锁轴20亦是手柄主结构A的转轴。锁轴20例如通过轴承安装在舱门主体上,能旋转地固定于舱门。即,手柄主结构A与锁轴20能绕锁轴20的轴线相对转动。本实施方式中,手柄主结构A在长度方向一侧与锁轴20铰接。这里,手柄主结构A的“长度方向一侧”表示向锁轴20靠近的方向,手柄主结构A的“长度方向另一侧”表示远离锁轴20的方向。两个支承部1b分别从手柄基部1向外手柄机构100里侧、例如向正交于轴向以及上述长度方向的方向(第一方向)突出地延伸,并彼此相向,在轴向上隔开间隔相对。两个支承部1b例如分别在上述长度方向上扩展。两个支承部1b例如形成为相同结构。两个支承部1b例如分别呈在与轴向正交的方向扩展。手柄基部1和两个支承部1b相当于本发明的“手柄主体”。The handle main structure A includes a
两个支承部1b分别包括多个铰接位,本实施方式中,例如包括与后述曲柄锁钩12铰接的铰接位12.1、与后述离合摇臂17铰接的铰接位17.3及与后述第三销轴14铰接的铰接位(参见图1a和图6)。手柄主结构A的两个支承部1b还包括与后述开启盖板2铰接的铰接位。此外,本实施方式中,手柄主结构A在两个支承部1b上与锁轴20铰接。也就是,手柄主结构A包括与锁轴20铰接的铰接位、与曲柄锁钩12铰接的铰接位、与离合摇臂17铰接的铰接位和与开启盖板2铰接的铰接位。各铰接位在手柄主结构A的长度方向上排列配置。在本实施方式中,以手柄主结构A与开启盖板2铰接的铰接位、手柄主结构A与离合摇臂17铰接的铰接位、手柄主结构A与曲柄锁钩12铰接的铰接位、手柄主结构A与锁轴20铰接的铰接位的顺序在手柄主结构A的长度方向上排列配置。The two supporting
手柄主结构A在两个支承部1b之间还包括从手柄基部1向外手柄机构100里侧突出的抵接接受部1d(参见图2),用于与后述承接部18b相抵接。The handle main structure A further includes an
手柄主结构A还包括第一贯通部1a(参见图2),用于操作后述开启盖板2以将外手柄机构100解锁。第一贯通部1a设置于手柄基部1的长度方向另一侧。本实施方式中,在手柄基部1上,在与后述开启盖板2对应的位置具有第一贯通部,该第一贯穿部在厚度方向上贯通手柄基部1,操作人员能经由第一贯通部对开启盖板2施力。如图3所示,手柄基部1的设置有第一贯通部1a的部分的宽度方向尺寸例如大于手柄基部1的其余部分(例如手柄基部1的比第一贯通部1a靠近长度方向一侧的部分)。The handle main structure A further includes a first through
手柄主结构A还包括第二贯通部1c(参见图2),用于使后述离合摇臂17的一部分穿过。本实施方式中,在手柄基部1上,在与后述离合摇臂17的头部17a(参见图2)对应的位置具有第二贯通部1c,该第二贯通部在厚度方向上贯通手柄基部1。The handle main structure A further includes a second penetration portion 1c (see FIG. 2 ) for passing a part of the
图4是示出本发明实施方式1的用于外翻式应急舱门的外手柄机构100的开启盖板机构B的立体图。开启盖板机构B主要包括开启盖板2、第一销轴3、第一衬套5和第二弹性构件4。第一销轴3固定于开启盖板2。本实施方式中,开启盖板2具有平板状的主体部2a和从主体部2a延伸并彼此相向的两个销轴固定部2b。本实施方式中,两个销轴固定部2b从主体部2a的一侧的面向与主体部2a正交或大致的方向突出地延伸。两个销轴固定部2b例如在所述轴向上隔开间隔相对。但不限于上述结构,销轴固定部2b也可以从主体部2a的一侧的面向与主体部2a交叉的方向突出。两个销轴固定部2b例如形成为相同结构。第一销轴3分别贯穿固定于两个销轴固定部2b。而且,第一销轴3与手柄主结构A的两个支承部1b分别铰接,形成手柄主结构A与开启盖板2铰接的铰接位。本实施方式中,在第一销轴3上的比固定于两个销轴固定部2b的部位靠近轴向两端部处,第一销轴3经由手柄主结构A的两个支承部1b与手柄主结构A铰接。但第一销轴3也可以在比固定于销轴固定部2b的部位远离轴向两端部处与手柄主结构A铰接。FIG. 4 is a perspective view showing a cover opening mechanism B of the
第一衬套5在第一销轴3的径向外侧与第一销轴3间隙配合。在第一衬套5的外侧,设有与第一衬套5配合的第二弹性构件4。第二弹性构件4以始终使开启盖板2趋向于关闭的形式对开启盖板2施加载荷。这里,“使开启盖板2趋向于关闭”的“关闭”是指,开启盖板2返回至能与后述锁钩结构D配合将外手柄锁定(限制手柄主体的运动)的位置。第二弹性构件4例如可以采用拉簧、压簧、扭簧等。本实施方式中,第二弹性构件4例如采用扭簧,在开启盖板2关闭的状态下通过作为第二弹性构件的扭簧4的施力而紧贴或抵接于手柄基部1。并且,例如在开启盖板2没有受到来自外手柄机构外部的施加载荷的情况下(这里,包括未受到后述锁钩结构D的施加载荷的情况),开启盖板2被扭簧4的施加力按压并抵接于手柄基部1。进一步,通过扭簧4的施力,开启盖板2的主体部2a的一部分例如以位于手柄基部1的外表面以内的形式与手柄主结构A的第一贯通部1a嵌合(开启盖板2的主体部2a的厚度与手柄主结构A的手柄基部1的厚度重叠),其他部分抵接于手柄基部1的内表面。该情况下,可以进一步减小外手柄机构100厚度尺寸并对第一贯通部1a进行补强。这里,外表面是指手柄基部1的外侧的面,内表面是指手柄基部1的里侧的面。The
开启盖板机构B还具有第二销轴7和第二衬套6。第二衬套6在第二销轴7的径向外侧与第二销轴7间隙配合。第二销轴7分别贯穿固定于两个销轴固定部2b。本实施方式中,第二销轴7例如固定于销轴固定部2b上的比第一销轴3远离主体部2a的位置。The cover opening mechanism B also has a
外手柄机构100还具有锁钩结构D(图1b),该锁钩结构D能与开启盖板机构B配合将外手柄机构100锁定。锁钩结构D安装于舱门。锁钩结构D包括锁钩8,锁钩8具有锁定部,该锁定部形成为能通过钩挂于开启盖板机构B的第二衬套6而将外手柄锁定的形状(例如参照图1b中的锁钩结构D,虚线表示第二衬套6)。也就是,第二衬套6与锁钩8相配合,可实现外手柄锁定功能。锁钩8相当于本发明的舱门侧锁钩。本实施方式中,随着手柄主体相对于锁轴20转动,第二衬套6与锁钩8例如在垂直于轴向的方向上相对靠近或远离。伴随于此,锁钩8钩挂于第二衬套6或从第二衬套6脱开,由此,将外手柄锁定或解锁。进一步,锁定部以配合第二衬套6的延伸方向的形式沿与轴向交叉的方向(本实施方式中,沿垂直于轴向的方向)凹陷。本实施方式中,锁定部的凹陷部位面向手柄基部1的长度方向一侧。例如在开启盖板2关闭的情况下,从第二衬套6的轴线到锁轴20轴线的距离与从锁定部内部的中心到锁轴20轴线的距离相等。在开启盖板2受到来自外手柄机构外部的朝里侧的施加载荷的情况下(这里,包括受到锁钩结构D的施加载荷的情况),以从第二衬套6的轴线到锁轴20轴线的距离变得小于从锁定部内部的中心到锁轴20轴线的距离的形式运动。The
锁钩8进一步在比锁定部靠前端部处具有凸轮部,用于将第二衬套6引导至锁定部。在本实施方式中,第二衬套6通过沿锁钩8凸轮部的边缘滑动而被引导至锁定部。例如,在欲将外手柄解锁的情况下,按压开启盖板2,与第二弹性构件4的施加力对抗,从而使第二衬套6从锁钩8的锁定部脱开(允许手柄主体的运动)。在欲将外手柄从解锁状态锁定的情况下,开启盖板2自身在作用有第二弹性构件4的施加力的状态下随着手柄主体运动,可以通过凸轮的作用运动,与第二弹性构件4的施加力对抗,使第二衬套6自动进入锁钩8的锁定部(无需另外对开启盖板2施加朝里侧的载荷)。另外,也可以通过朝里侧对开启盖板2施加载荷来使第二衬套6自动进入锁钩8的锁定部。图9示意性示出实施方式1的沿轴向观察第二衬套6在与锁钩8脱开后通过凸轮部的边缘返回锁定状态的情况下的第二衬套6与锁钩8的位置关系的图,虚线示出的圆形C1~C5表示第二衬套6的位置。第二衬套6在与锁钩8脱开后通过凸轮部的边缘返回锁定状态的情况例如包括外手柄关闭过程。如图9所示,从圆形C1到圆形C3的位置变化例如示出在外手柄关闭过程中第二衬套6接触锁钩8后的运动轨迹。接着,从圆形C3到圆形C5的位置变化例如示出外手柄完全关闭后,开启盖板2上无操作人员的施加力等来自外部的施加载荷的情况下,第二衬套6在扭簧4作用下上锁的轨迹。The
本实施方式中,开启盖板2的一部分经由手柄基部1的第一贯通部向外露出。由此,操作人员能容易地从手柄基部1的外侧经由第一贯通部对开启盖板2向里侧施力。即,能通过朝向与第二弹性构件4的施加力对抗的方向施力,使通过锁钩8锁定的第二衬套6解除锁定(脱开),将外手柄机构100解锁。这里,“里侧”对应于手柄基部1的设置有支承部1b的一侧。“外侧”对应于手柄基部1的支承部相反侧。In the present embodiment, a part of the
锁轴20与手柄主结构A铰接。本实施方式中,锁轴20与手柄主结构A铰接于两个支承部1b,锁轴20与支承部1b(手柄主结构A)能绕锁轴20的轴线相对转动。外手柄机构100还包括驱动曲柄18(有时简称“曲柄18”)。驱动曲柄18与锁轴20固连,即驱动曲柄18能与锁轴20一起转动。在锁轴20的与两个支承部1b铰接的铰接处之间的部位,驱动曲柄18外设于锁轴20。驱动曲柄18在外周部在隔着锁轴20的两侧具有被钩挂部18a和承接部18b。被钩挂部18a设置于靠近后述离合机构C的那侧(手柄主结构A长度方向另一侧)。沿轴向观察外手柄机构100时,被钩挂部18a例如从驱动曲柄18的外周部沿朝向外手柄机构100外侧的方向延伸。承接部18b设置于远离后述离合机构C的那侧(手柄主结构A长度方向一侧),且与手柄主结构A的抵接接受部1d能分离地抵接,即,承接部18b能通过例如锁轴20与支承部1b的相对转动抵接于抵接接受部1d以及从抵接接受部1d分离。换言之,抵接接受部1d沿正交于轴向的方向、例如沿锁轴20的周向以能分离的形式进行支承。例如,允许驱动曲柄18相对于手柄主结构A从承接部18b抵接于抵接接受部1d的状态朝向承接部18b从抵接接受部1d离开的方向(图1a中,逆时针)转动。而且,通过承接部18b抵接于抵接接受部1d,能从外手柄机构100的手柄主结构A经由承接部18b对驱动曲柄18施力使其转动。例如,在舱门关闭且外手柄关闭(锁定)时,承接部18b与手柄主结构A抵接;在舱门打开且外手柄关闭(用内手柄开门或者用外手柄开门后离合处于“离”的状态下关闭外手柄)时,承接部18b与手柄主结构A不抵接;在舱门打开且外手柄打开(解锁)时,承接部18b与手柄主结构A抵接。The
图6是示出本发明实施方式1的用于外翻式应急舱门的外手柄机构100的离合机构C的立体图。离合机构C主要包括离合摇臂17、第四销轴16、第一弹性构件15、第三销轴14、连杆13和曲柄锁钩12。离合机构C配置于手柄主结构A的两个支承部1b之间。曲柄锁钩12具有能钩挂或卡合于驱动曲柄18的被钩挂部18a的锁钩部12a,并与手柄主结构A铰接(图6中,铰接位12.1)。本实施方式中,曲柄锁钩12与手柄主结构A的两个支承部1b铰接。并且,曲柄锁钩12在铰接于支承部1b的部位与锁钩部12a之间与连杆13铰接。本实施方式中,在沿轴向观察时,曲柄锁钩12在一端具有锁钩部12a,在另一端通过例如销轴与两个支承部1b铰接,在大致中间部(图6中,铰接位13.1)与连杆13铰接。通过连杆13带动曲柄锁钩12使锁钩部12a钩挂或卡合于被钩挂部18a,或从被钩挂部18a脱开。6 is a perspective view showing the clutch mechanism C of the
连杆13的一端与曲柄锁钩12铰接,另一端与离合摇臂17铰接(图6中,铰接位17.4)。离合摇臂17还与手柄主结构A的两个支承部1b铰接。如此,离合摇臂17可与手柄主结构A相对转动。在沿轴向观察时,离合摇臂17在一端部(本实施方式中,前端部)具有头部17a,并在另一端部(本实施方式中,基端部)铰接于连杆13。并且,离合摇臂17在铰接于连杆13的部位与头部17a之间与手柄主结构A铰接(图6中,铰接位17.3)。本实施方式中,头部17a具有朝向外手柄机构100外侧的平面17.1,平面17.1经由第二贯通部1c朝外手柄机构100外露出。通过离合摇臂17与手柄主结构A的相对转动,离合摇臂17的一部分、例如头部17a能穿过第二贯通部1c朝手柄主结构A外突出。头部17a还具有朝向外手柄机构100里侧的平面17.5。第一弹性构件15通过第四销轴16和第三销轴14分别与离合摇臂17及手柄主结构A的两个支承部1b铰接。如图6所示,离合摇臂17例如具有U字形的主体部。该U字形中的两条臂通过平面17.5连接。并且,离合摇臂17在这两条臂的前端铰接于连杆13,在这两条臂的基端铰接于手柄主结构A。头部17a从该U字形中的底部延伸,在沿轴向观察时,头部17a从该U字形中的底部朝向外手柄机构100外侧弯曲延伸。第一弹性构件15在轴向上位于该U字形的两条臂的里侧,第四销轴16铰接于该U字形中的比铰接位17.3更靠长度方向另一侧处。也就是第四销轴16与离合摇臂17的铰接位17.2比铰接位17.3更靠长度方向另一侧处。在沿轴向观察时,第三销轴14与手柄主结构A的两个支承部1b铰接的铰接位比铰接位17.3更靠外手柄机构100外侧,且在手柄主结构A的长度方向上比铰接位17.3更靠长度方向一侧。One end of the connecting
如此,通过例如对平面17.5、17.1施力,能使曲柄锁钩12与驱动曲柄18的相合或相离。也就是,通过操作离合摇臂17,可使曲柄锁钩12与驱动曲柄18相合或相离(切换曲柄锁钩12与驱动曲柄18的相合或相离状态),从而实现内外手柄的离合控制。第一弹性构件15在曲柄锁钩12与驱动曲柄18相离状态时,其施加载荷使离合摇臂17趋向于关闭,从而使曲柄锁钩12与驱动曲柄18保持相离状态,当曲柄锁钩12与驱动曲柄18处于相合状态时,第一弹性构件15作用载荷使离合摇臂17趋向于打开,从而使曲柄锁钩12与驱动曲柄18保持相合状态。这里,“使离合摇臂趋向于关闭”的“关闭”是指,离合摇臂17返回至曲柄锁钩12与驱动曲柄18保持相离且平面17.1(离合摇臂17)与手柄基部1的外表面能确保机身的气动外形的位置,包括离合摇臂17整体位于手柄基部1的外表面以内,例如平面17.1与手柄基部1(手柄主结构A)外表面齐平。“使离合摇臂趋向于打开”的“打开”是指,离合摇臂17处于曲柄锁钩12与驱动曲柄18保持相合且平面17.1从手柄基部1的第二贯通部1c突出的位置。可根据情况变更第四销轴16、第一弹性构件15、第三销轴14的设置位置等,例如,可根据手柄主结构A或离合摇臂17的不同配置等调整第一弹性构件15与离合摇臂17及手柄主结构A铰接的铰接位。第一弹性构件15例如可以采用压簧、扭簧等。本实施方式中,第一弹性构件15例如采用拉簧,第三销轴14与手柄主结构A铰接,并与作为第一弹性构件的拉簧15连接;第四销轴16与离合摇臂17铰接,并与拉簧15连接。In this way, the
本实施方式中,各销轴设置为轴线与锁轴20的轴向平行。即,锁轴20的旋转轴线、曲柄锁钩12的旋转轴线、离合摇臂17的旋转轴线和开启盖板2的旋转轴线相互平行。但不限于上述结构,至少锁轴20的旋转轴线、曲柄锁钩12的旋转轴线和离合摇臂17的旋转轴线相互平行即可。In this embodiment, each pin shaft is arranged so that the axis is parallel to the axial direction of the
(打开和关闭装设有外手柄机构的舱门的动作)(action of opening and closing a hatch equipped with an outer handle mechanism)
以下,对打开和关闭装设有根据实施方式1的用于外翻式应急舱门的外手柄机构100的舱门的动作进行说明。打开舱门工作流程如图7所示,关闭舱门工作流程如图8所示。Hereinafter, the operation of opening and closing the hatch equipped with the
舱门开启步骤:Steps to open the door:
内手柄开启舱门:内手柄开启舱门时,锁轴20转动(图1a中,锁轴20相对于手柄主结构A朝逆时针方向转动),驱动曲柄18随之转动,此时外手柄离合机构C处于离状态,外手柄静止,外手柄仍保持关闭状态。The inner handle opens the cabin door: when the inner handle opens the cabin door, the
外手柄开启舱门:扭簧4施加载荷始终使开启盖板2趋向于关闭,手指按压开启盖板2,打开开启盖板2,开启盖板2打开后第二衬套6与锁钩8自动脱开,外手柄解锁。拉动外手柄,手柄主结构A转动,手柄主结构A带动驱动曲柄18转动,驱动曲柄18带动锁轴20转动(图1a中,锁轴20相对于手柄主结构A朝逆时针方向转动),舱门随锁轴20转动而解闩解锁,舱门打开。The door is opened by the outer handle: the load of the
舱门关闭步骤:Door closing steps:
外手柄关闭舱门(外手柄被解锁):手指按压离合摇臂17上平面17.5,离合摇臂17转动并通过连杆13带动曲柄锁钩12与驱动曲柄18相合,此时转动手柄主结构A,手柄主结构A带动曲柄锁钩12转动,曲柄锁钩12带动驱动曲柄18转动,驱动曲柄18带动锁轴20转动(图2中,锁轴20相对于手柄主结构A朝顺时针方向转动)。转动手柄主结构A时,第二衬套6在锁钩8上凸轮部作用下,缓慢转动直到与锁钩8上钩槽相合,外手柄上锁,外手柄上锁后离合摇臂17仍从手柄主结构A突出,按压离合摇臂17上突出平面17.1,离合摇臂17转动并带动曲柄锁钩12与驱动曲柄18相离,离合摇臂17进入手柄主结构A中,平面17.1与手柄主结构A齐平,外手柄关闭,舱门关闭。The outer handle closes the door (the outer handle is unlocked): the finger presses the upper plane 17.5 of the
外手柄关闭状态下,开启盖板2通过扭簧4保持在关闭位置,离合摇臂17通过拉簧15保持在关闭位置,从而保证了机身的气动外形。When the outer handle is closed, the
若舱门已由内手柄打开,外手柄处于关闭状态,此时需手指按压开启盖板2,打开开启盖板2,开启盖板2打开后第二衬套6与锁钩8自动脱开,外手柄解锁。拉动外手柄,手柄主结构A转动,外手柄开启,后执行舱门关闭步骤。If the cabin door has been opened by the inner handle and the outer handle is in the closed state, you need to press your finger to open the
根据实施方式1的用于外翻式应急舱门的外手柄机构100,离合机构C与开启盖板机构B完全独立,该设计方式简化了外手柄机构,降低了零件的加工难度。扭簧施加载荷始终使盖板趋向于关闭,保证无人员操作时盖板始终关闭,手柄始终处于锁定状态,从而防止外手柄因外力干扰而翻转。According to the
(实施方式2)(Embodiment 2)
外翻式应急舱门外手柄现有技术包括空客系列、庞巴迪C系列飞机等的外手柄机构难以调节手柄阶差,进一步增加了设计和加工难度。The existing technology of the outer handle of the everted emergency cabin door includes the outer handle mechanism of Airbus series, Bombardier C series aircraft, etc. It is difficult to adjust the handle step difference, which further increases the difficulty of design and processing.
相对于此,本发明实施方式2的外手柄机构进一步具有手柄阶差调节功能,其他结构同实施方式1,因此,对与实施方式1相同的结构标注同一附图标记并省略重复说明。On the other hand, the outer handle mechanism of the second embodiment of the present invention further has a handle step adjustment function, and other structures are the same as those of the first embodiment.
图5a、图5b示出本发明实施方式2的用于外翻式应急舱门的外手柄机构的锁钩结构D的概略结构。锁钩结构D包括锁钩8、锁钩法兰9、两个锁钩调节螺母(第一螺纹构件)10和两个锁钩衬套11。FIGS. 5 a and 5 b show the schematic structure of the lock hook structure D for the outer handle mechanism of the everted emergency hatch according to
锁钩8在前端具有包括锁定部的第一部分,在基端具有圆柱状的第二部分。两个锁钩调节螺母10分别与锁钩8的第二部分的外周面螺纹结合。锁钩法兰9可滑动地嵌套在锁钩8的外周。两个锁钩调节螺母10分别隔着锁钩衬套11邻接设置于锁钩法兰9的两侧。锁钩结构D通过锁钩法兰9固定于舱门主体结构。详细而言,锁钩8的第二部分在外周面具有外螺纹,两个锁钩调节螺母10分别设有在内周面具有内螺纹的两端开口的孔部。锁钩法兰9包括圆柱状的锁钩法兰主体9a。锁钩法兰主体9a的前端设有从外周面朝径向外扩展的固定部9b。例如,固定部9b上设置有孔部,锁钩结构D通过这些孔部被固定于舱门主体。从,锁钩法兰9(锁钩法兰主体9a)的轴向观察时,固定部9b例如呈圆角三角形,但也可以呈其他能固定于舱门主体的形状。也就是,锁钩结构D在固定部9b处装设于舱门主体。通过旋拧两个锁钩调节螺母10中的、与锁钩8的更靠前端处螺纹结合的锁钩调节螺母10,调节锁钩8位置。例如,外手柄关闭状态下的外手柄阶差由锁钩8控制,通过锁钩调节螺母10调节锁钩8位置,可实现对外手柄阶差的控制。锁钩法兰9和两个锁钩调节螺母10分别是构成本发明的第一调节机构的构件。The
根据本的实施方式的用于外翻式应急舱门的外手柄机构,开启盖板机构B中第二衬套6与门体(舱门主体)上锁钩8配合,可实现外手柄的锁定和阶差调节功能,锁钩8通过锁钩法兰9固定于门体结构上,当开启盖板2关闭时,第二衬套6与锁钩8相合,手柄处于锁定状态,当开启盖板打开,第二衬套6和锁钩8相离,外手柄处于解锁状态,此时可通过外手柄开启舱门,锁钩8与门体主结构间采用螺纹连接,可通过锁钩调节螺母10调节锁钩8相对于门体的位置,调节第二衬套6与锁钩8相合时开启盖板2相对于门体的相对位置,从而实现手柄阶差的调节。According to the outer handle mechanism for the everted emergency hatch of the present embodiment, the
(实施方式3)(Embodiment 3)
外翻式应急舱门外手柄现有技术包括空客系列、庞巴迪C系列飞机等的外手柄机构难以调节外手柄与锁轴转动角度关系,进一步增加了设计和加工难度。The existing technology of the outer handle of the everted emergency cabin door includes the outer handle mechanism of Airbus series, Bombardier C series aircraft, etc. It is difficult to adjust the rotation angle relationship between the outer handle and the lock shaft, which further increases the difficulty of design and processing.
相对于此,本发明实施方式3的外手柄机构进一步具有外手柄与锁轴转动角度调节功能,其他结构同实施方式1,因此,对与实施方式1相同的结构标注同一附图标记并省略重复说明。On the other hand, the outer handle mechanism of the third embodiment of the present invention further has the function of adjusting the rotation angle of the outer handle and the lock shaft, and the other structures are the same as those of the first embodiment. Therefore, the same reference numerals are attached to the same structures as those of the first embodiment and the repetition is omitted. illustrate.
本实施方式中,具有包括驱动曲柄18和螺钉19(见图2)的驱动曲柄机构。驱动曲柄18的承接部18b具有两端开口的孔部18b1。也就是,承接部18b具有贯穿承接部18b的孔部18b1。承接部18b的孔部的内周面设有内螺纹。在孔部18b1中螺纹结合有螺钉19。螺钉19设有在外周面具有外螺纹的圆柱状的外螺纹部。螺钉19的一端具有比外螺纹部大径的头部。在螺钉19离合于驱动曲柄18的状态下,驱动曲柄18通过螺钉19的头部与手柄主结构A的抵接接受部1d抵接。也就是,驱动曲柄18通过螺钉19与抵接接受部1d抵接。而且,设有在内周面具有内螺纹且两端开口的孔部的螺母(第二螺纹构件)21与孔部18b1相邻地与螺钉19的外周面螺纹结合。另外,可以在螺母21与孔部18b1之间介设衬套。通过旋拧螺钉19和螺母21,调节螺钉19位置。例如,外手柄开启舱门时,手柄主结构A通过驱动曲柄18带动锁轴20转动,手柄主结构A与驱动曲柄18抵接时的相对位置可通过螺钉19进行调节。孔部18b1和调节螺钉19分别是构成本发明的第二调节机构的构件。In this embodiment, there is a drive crank mechanism including a drive crank 18 and a screw 19 (see FIG. 2 ). The receiving
根据本的实施方式的用于外翻式应急舱门的外手柄机构,驱动曲柄机构包括驱动曲柄18和螺钉19,驱动曲柄18与锁轴20固连,通过外手柄开启舱门时,手柄主结构A转动带动驱动曲柄18转动,锁轴20随之转动。手柄主结构A和驱动曲柄18间的间隙可由螺钉19调节,该螺钉设计可方便外手柄与锁轴旋转角度关系的调节,降低手柄主结构A和驱动曲柄18加工难度。外手柄关闭舱门时,手柄主结构A通过曲柄锁钩带动驱动曲柄转动,锁轴20随之转动。According to the outer handle mechanism for the eversion type emergency hatch according to the present embodiment, the drive crank mechanism includes a drive crank 18 and a
以上对本发明的实施方式进行了说明,但本发明的范围并不受此限定,能在不脱离发明主旨的范围内追加各种改变加以实施。此外,能将所述实施方式及其变形例适当地任意组合。The embodiments of the present invention have been described above, but the scope of the present invention is not limited thereto, and various modifications can be added and implemented without departing from the gist of the invention. In addition, the above-described embodiments and modifications thereof can be appropriately combined arbitrarily.
例如实施方式1~3中,开启盖板2的主体部2a形成为平板状,可以方便操作人员施力。但开启盖板2的主体部不一定为平板状,只要是操作人员能例如经由第一贯通部来推动的结构,就可以是任意形状。离合摇臂17的头部17a的平面17.1、17.5亦是如此。For example, in
本发明例如能用于包括外翻式应急舱门的民用飞机等飞行器。The present invention can be used, for example, for aircrafts such as civil aircraft including an everted emergency hatch.
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| CN114872878B (en) * | 2022-05-18 | 2025-03-07 | 中航沈飞民用飞机有限责任公司 | A civil aircraft cabin door emergency handle locking mechanism |
| CN115465457B (en) * | 2022-10-12 | 2024-09-06 | 中国航空工业集团公司西安飞机设计研究所 | An emergency slide throwing mechanism for an aircraft emergency exit door |
| CN116238681B (en) * | 2023-04-24 | 2025-07-04 | 中国商用飞机有限责任公司 | A hatch door upper locking mechanism device |
| CN116641610A (en) * | 2023-06-19 | 2023-08-25 | 菲舍尔航空部件(镇江)有限公司 | A civil aircraft door interior lock assembly |
| CN117163287B (en) * | 2023-09-07 | 2025-11-18 | 中航沈飞民用飞机有限责任公司 | A water-dropping hatch for firefighting aircraft |
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