CN115419349A - A space two-way pressure-bearing hatch - Google Patents
A space two-way pressure-bearing hatch Download PDFInfo
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- CN115419349A CN115419349A CN202210838631.5A CN202210838631A CN115419349A CN 115419349 A CN115419349 A CN 115419349A CN 202210838631 A CN202210838631 A CN 202210838631A CN 115419349 A CN115419349 A CN 115419349A
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- 238000007789 sealing Methods 0.000 claims abstract description 44
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- E—FIXED CONSTRUCTIONS
- E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
- E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
- E06B3/00—Window sashes, door leaves, or like elements for closing wall or like openings; Layout of fixed or moving closures, e.g. windows in wall or like openings; Features of rigidly-mounted outer frames relating to the mounting of wing frames
- E06B3/32—Arrangements of wings characterised by the manner of movement; Arrangements of movable wings in openings; Features of wings or frames relating solely to the manner of movement of the wing
- E06B3/34—Arrangements of wings characterised by the manner of movement; Arrangements of movable wings in openings; Features of wings or frames relating solely to the manner of movement of the wing with only one kind of movement
- E06B3/36—Arrangements of wings characterised by the manner of movement; Arrangements of movable wings in openings; Features of wings or frames relating solely to the manner of movement of the wing with only one kind of movement with a single vertical axis of rotation at one side of the opening, or swinging through the opening
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
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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
- E05C9/00—Arrangements of simultaneously actuated bolts or other securing devices at well-separated positions on the same wing
- E05C9/06—Arrangements of simultaneously actuated bolts or other securing devices at well-separated positions on the same wing with three or more sliding bars
- E05C9/063—Arrangements of simultaneously actuated bolts or other securing devices at well-separated positions on the same wing with three or more sliding bars extending along three or more sides of the wing or frame
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- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D11/00—Additional features or accessories of hinges
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- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D3/00—Hinges with pins
- E05D3/02—Hinges with pins with one pin
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- E—FIXED CONSTRUCTIONS
- E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
- E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
- E06B7/00—Special arrangements or measures in connection with doors or windows
- E06B7/16—Sealing arrangements on wings or parts co-operating with the wings
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- Mechanical Engineering (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Power-Operated Mechanisms For Wings (AREA)
- Wing Frames And Configurations (AREA)
Abstract
Description
技术领域technical field
本发明涉及一种载人航天器舱门,具体涉及一种空间双向承压舱门,属于载人航天器机构设计技术领域。The invention relates to a cabin door of a manned spacecraft, in particular to a two-way pressure-bearing cabin door in space, and belongs to the technical field of mechanism design of a manned spacecraft.
背景技术Background technique
空间舱门作为载人飞行器的重要组成部分,是实现密封舱密封功能的关键结构,同时也是航天员出入密封舱的通道。载人航天器舱门的研究与设计不仅对航天员的舱内安全保障及太空出舱活动,而且对于载人航天器的交会对接都具有重要意义。As an important part of the manned aircraft, the space hatch is the key structure to realize the sealing function of the airtight cabin, and it is also the passage for astronauts to enter and exit the airtight cabin. The research and design of manned spacecraft hatch is not only of great significance to the safety of astronauts in the cabin and space out activities, but also to the rendezvous and docking of manned spacecraft.
载人飞船在飞行过程中,载荷需要承受极其严峻的工作环境,例如,受到猛烈的冲击与振动。舱门在开启和关闭时,内外的压力差对舱门受力影响很大;另外,由于舱门结构比较重,单纯地手动开启比较困难。钱海鲲等人在2015年03期《上海航天》中发表的《航天器电动手动一体化舱门锁紧机构设计》中提出了一种舱门锁紧执行机构布局方案,其原理是通过驱动中间齿轮带动两个扇形齿轮运动,从而带动连杆滚轮机构实现舱门的锁紧与打开,并实现端面密封,该装置具有结构简单,可靠性高的特征;但同时该特征使得这种装置只能单向承压密封,不具备双向承压密封的能力。During the flight of a manned spacecraft, the load needs to withstand an extremely severe working environment, for example, it is subjected to severe shock and vibration. When the hatch is opened and closed, the pressure difference between the inside and outside has a great influence on the force of the hatch; in addition, due to the relatively heavy structure of the hatch, it is difficult to simply open it manually. Qian Haikun and others proposed a layout scheme of the cabin door locking actuator in the "Design of Spacecraft Electric and Manual Integrated Hatch Door Locking Mechanism" published in "Shanghai Aerospace" in 2015, the principle of which is to drive The intermediate gear drives the two sector gears to move, thereby driving the connecting rod and roller mechanism to lock and open the cabin door and realize the end face sealing. This device has the characteristics of simple structure and high reliability; but at the same time, this feature makes this device only Capable of one-way pressure-bearing sealing, but not capable of bi-directional pressure-bearing sealing.
空间舱门分为两种,第一种为飞行器内部空间与外界环境的接口;第二种为两个相邻舱段之间的接口。目前对空间舱门的结构设计多集中在上述第一种,由于外界环境为真空环境,该种舱门在设计时采用内压密封的方式(即单向承压密封),且只能实现向内的打开;而对于上述第二种,由于相邻两个舱段中任意一个舱段内即可能是真空环境也可能是大气环境,因此上述第一种舱门结构并不适用于作为两个相邻舱段之间的接口。There are two types of space hatches. The first type is the interface between the interior space of the aircraft and the external environment; the second type is the interface between two adjacent cabins. At present, most of the structural design of the space hatch is focused on the first type mentioned above. Since the external environment is a vacuum environment, the internal pressure sealing method (that is, one-way pressure-bearing seal) is adopted in the design of this kind of hatch, and it can only achieve one-way pressure sealing. As for the above second type, since any one of the two adjacent cabin sections may be in a vacuum environment or an atmospheric environment, the above-mentioned first type of cabin door structure is not suitable for use as two Interface between adjacent compartments.
发明内容Contents of the invention
有鉴于此,本发明提供一种空间双向承压舱门,作为载人飞行器相邻两个舱段之间的接口,能够实现双向承压密封,且能够保证在相邻两个舱段内处于各种环境下的开启。In view of this, the present invention provides a space two-way pressure-bearing cabin door, as the interface between two adjacent cabin sections of a manned aircraft, which can realize two-way pressure-bearing sealing, and can ensure that the two-way adjacent cabin sections are in the same position. Enabled under various circumstances.
所述的空间双向承压舱门,包括:设置在舱体上的环形门框结构;The space two-way pressure-bearing cabin door includes: an annular door frame structure arranged on the cabin body;
通过门轴机构铰接在所述门框结构上的门体结构;所述门体结构能够绕门轴机构转动;且所述门体结构的两侧均设置有平衡阀;A door body structure hinged on the door frame structure through a door shaft mechanism; the door body structure can rotate around the door shaft mechanism; and both sides of the door body structure are provided with balance valves;
用于对所述门体结构进行锁紧的传动锁紧机构;所述传动锁紧机构包括:两个以上连杆以及与所述连杆一一对应的滑块;在门体结构的外圆周以及门框结构的内圆周均沿周向均匀间隔分布有与所述滑块一一对应的条形槽;当舱门处于关闭状态时,门体结构上的条形槽和门框结构上的条形槽一一对接形成滑槽;A transmission locking mechanism for locking the door body structure; the transmission locking mechanism includes: more than two connecting rods and sliders corresponding to the connecting rods one by one; on the outer circumference of the door body structure And the inner circumference of the door frame structure is evenly distributed along the circumferential direction with strip grooves corresponding to the sliders one by one; when the hatch is in the closed state, the strip grooves on the door structure and the strip grooves on the door frame structure The grooves are butted together to form a chute;
设置在门体结构中心位置,用于驱动所述传动锁紧机构运动的驱动机构;所述连杆的一端与所述驱动机构铰接,另一端铰接滑块;在所述驱动机构驱动下,所述滑块在滑槽内滑动,实现对所述门体结构的锁紧与解锁;Set at the center of the door body structure, it is used to drive the driving mechanism for the movement of the transmission locking mechanism; one end of the connecting rod is hinged to the driving mechanism, and the other end is hinged to the slider; driven by the driving mechanism, the The slider slides in the chute to realize the locking and unlocking of the door structure;
采用径向密封的方式实现门体结构和门框结构之间密封的密封结构。The radial sealing method is used to realize the sealing structure between the door body structure and the door frame structure.
作为本发明的一种优选方式:所述驱动机构包括:主轴套以及行星齿轮系;As a preferred mode of the present invention: the drive mechanism includes: a main shaft sleeve and a planetary gear train;
所述主轴套安装在门体结构的中心位置,所述主轴套上沿周向均匀间隔分布有与所述连杆一一对应的铰接点,用于所述连杆的铰接;The main shaft sleeve is installed at the center of the door body structure, and the main shaft sleeve is uniformly distributed along the circumferential direction with hinge points corresponding to the connecting rods one by one, which are used for the hinge of the connecting rods;
所述行星轮系包括:主轴以及在围绕主轴呈正三角状态分布的三个行星齿轮;行星轮系和开关转动手柄分别设置在主轴套的端面两侧;所述主轴套朝向行星轮系所在侧沿其轴向延伸有环形内齿;The planetary gear train includes: a main shaft and three planetary gears distributed in an equilateral triangle around the main shaft; the planetary gear train and the switch handle are respectively arranged on both sides of the end face of the main shaft sleeve; the main shaft sleeve faces the side edge where the planetary gear train is located Its axial extension has annular internal teeth;
所述主轴的一端穿过主轴套的中心孔后与开关转动手柄固接,另一端伸出门体结构与舱外操作接口及指针相连;所述主轴中部固接主轴齿轮,三个行星齿轮分别与主轴齿轮啮合;同时三个行星齿轮分别与主轴套上的内齿啮合。One end of the main shaft passes through the central hole of the main shaft sleeve and is fixedly connected to the switch handle, and the other end extends out of the door structure to connect with the operation interface outside the cabin and the pointer; the middle part of the main shaft is fixed to the main shaft gear, and the three planetary gears are respectively connected to The main shaft gear meshes; at the same time, the three planetary gears mesh with the internal teeth on the main shaft sleeve respectively.
作为本发明的一种优选方式:所述门轴机构包括:门轴机构舱门框固件、门轴轴体、拉紧弹簧以及门轴机构舱门固件;As a preferred mode of the present invention: the door shaft mechanism includes: door shaft mechanism cabin door frame hardware, door shaft shaft body, tension spring and door shaft mechanism cabin door hardware;
所述门轴机构舱门框固件固定在所述门框结构上,用于支撑所述门轴轴体;所述门轴机构舱门固件的一端与门体结构固接,另一端套装在门轴轴体上;所述门轴轴体为门体结构相对门框结构打开和关闭的旋转轴;The hatch door frame firmware of the door shaft mechanism is fixed on the door frame structure to support the shaft body of the door shaft; one end of the hatch door firmware of the door shaft mechanism is fixedly connected to the door body structure, and the other end is sleeved on the door shaft on the body; the door shaft shaft body is a rotating shaft for the door body structure to open and close relative to the door frame structure;
所述门轴机构舱门固件通过条形孔套装在门轴轴体上,所述拉紧弹簧的一端套装在门轴轴体上,另一端与门轴机构舱门固件相连;所述拉紧弹簧的伸缩方向与条形孔的长度方向一致,均沿门体结构的轴向。The hatch door firmware of the door shaft mechanism is set on the door shaft shaft body through a strip hole, one end of the tension spring is sleeved on the door shaft body, and the other end is connected with the hatch door firmware of the door shaft mechanism; The expansion and contraction direction of the spring is consistent with the length direction of the strip hole, both along the axial direction of the door body structure.
作为本发明的一种优选方式:所述门框结构上条形槽的端部设置有压紧曲面,所述压紧曲面为所述条形槽沿门框结构的轴向下沉形成的曲面结构;所述滑块端部具有滚轮;关闭所述门体结构时,所述滑块进入位于门框结构上的滑槽内运动至压紧曲线所在位置时,其端部滚轮沿着压紧曲面移动,带动所述门体结构轴向平移。As a preferred mode of the present invention: the end of the bar-shaped groove on the door frame structure is provided with a pressing curved surface, and the pressing curved surface is a curved surface structure formed by sinking the bar-shaped groove along the axial direction of the door frame structure; There are rollers at the end of the slider; when the door structure is closed, the slider enters the chute on the door frame structure and moves to the position of the pressing curve, and the rollers at the end move along the pressing surface, Drive the door body structure to move axially.
作为本发明的一种优选方式:还包括导向机构;用于门体结构闭合时的导向;As a preferred mode of the present invention: it also includes a guiding mechanism; used for guiding when the door structure is closed;
所述导向机构位包括:导向槽和导向辊;所述导向槽固定在所述门框结构上,导向槽的长度与门框结构的轴向平行;所述门体结构外圆周具有导向槽滑动配合的凸起柱体;The guide mechanism position includes: a guide groove and a guide roller; the guide groove is fixed on the door frame structure, and the length of the guide groove is parallel to the axial direction of the door frame structure; the outer circumference of the door body structure has a sliding fit of the guide groove raised cylinder;
所述导向槽具有喇叭状开口,导向槽的外侧具有与该侧面垂直的套筒;所述导向辊位于该套筒内,与该套筒滑动配合;所述导向辊一端端部设置有滑轮,导向槽上与滑轮对应位置设置有开孔;所述导向辊的另一端通过套筒弹簧与套筒的内底面相连;所述弹簧处于自然状态下,所述滑轮凸出于导向槽内底面上的开孔。The guide groove has a trumpet-shaped opening, and the outer side of the guide groove has a sleeve perpendicular to the side; the guide roller is located in the sleeve and slidably fits with the sleeve; one end of the guide roller is provided with a pulley, There is an opening on the guide groove corresponding to the pulley; the other end of the guide roller is connected to the inner bottom surface of the sleeve through the sleeve spring; when the spring is in a natural state, the pulley protrudes from the inner bottom surface of the guide groove opening.
作为本发明的一种优选方式:所述门体结构上固定有舱门锁止阀,所述主轴上设置有与所述舱门锁止阀配合的锁止槽;As a preferred mode of the present invention: a hatch lock valve is fixed on the door body structure, and a lock groove cooperating with the hatch lock valve is arranged on the main shaft;
当所述舱门锁止阀的锁止芯位于所述主轴上的锁止槽内时,能够限制所述主轴转动。When the locking core of the hatch locking valve is located in the locking groove on the main shaft, the rotation of the main shaft can be restricted.
作为本发明的一种优选方式:所述传动锁紧机构处于锁紧状态时,所述连杆与所述门体结构的径向重合,处在连杆转动的死点位置。As a preferred mode of the present invention: when the transmission locking mechanism is in the locked state, the connecting rod coincides with the radial direction of the door body structure, and is at the dead point of the connecting rod rotation.
作为本发明的一种优选方式:所述密封结构为设置在所述门体结构外圆周面上的双层密封圈。As a preferred mode of the present invention: the sealing structure is a double-layer sealing ring arranged on the outer peripheral surface of the door body structure.
作为本发明的一种优选方式:所述传动锁紧机构包括:十二根连杆以及与十二根连杆一一对应的滑块。As a preferred mode of the present invention: the transmission locking mechanism includes: twelve connecting rods and sliders corresponding to the twelve connecting rods one by one.
有益效果:Beneficial effect:
(1)本发明提供的空间舱门采用多组连杆滑块机构并联实现锁紧与径向密封相结合的方式实现了舱门的双向承压密封;使其能够作为载人飞行器相邻两个舱段之间的接口,且相邻两个舱段内处于各种环境下均能够实现舱门的开启。具体的:传动锁紧机构中采用周向均匀分布的连杆滑块能够均匀的将加载力传递到门体周边的压紧点,实现舱门的锁紧,该种结构布局提高了舱门的承压能力。(1) The space hatch provided by the present invention realizes the two-way pressure-bearing sealing of the hatch by adopting multiple groups of connecting rod slider mechanisms connected in parallel to realize locking and radial sealing; The interface between two compartments, and the opening of the hatch can be realized under various environments in two adjacent compartments. Specifically: in the transmission locking mechanism, the connecting rod sliders evenly distributed in the circumferential direction can evenly transmit the loading force to the pressing points around the door body to realize the locking of the hatch. This structural layout improves the safety of the hatch. Pressure endurance.
(2)驱动机构和传动锁紧机构之间通过行星轮系传递动力,驱动机构采用中心加载的方式提供驱动力,并将中心加载的驱动力放大传递给传动锁紧机构,能够达到省力并精准控制行程的效果,使操作者只需较小的力就能够实现舱门精准的开启与锁紧,满足了航天员操作对舱门操作力较小的要求。(2) The power is transmitted between the driving mechanism and the transmission locking mechanism through the planetary gear train. The driving mechanism provides the driving force in the way of central loading, and amplifies the driving force of the central loading and transmits it to the transmission locking mechanism, which can achieve labor saving and precision. The effect of controlling the stroke enables the operator to realize the precise opening and locking of the cabin door with only a small force, which meets the requirements of the astronauts for the operation of the cabin door with a small operating force.
(3)采用浮动式门轴机构,门体结构与门轴轴体之间具有一定的活动间隙,使门体结构相对门轴轴体具有轴向平动的位移量,配合在传动锁紧机构的滑槽内设置的压紧曲线,在确保舱门锁紧的同时,实现对径向密封圈的均匀压紧。(3) The floating door shaft mechanism is adopted, and there is a certain movable gap between the door body structure and the door shaft body, so that the door body structure has an axial translational displacement relative to the door shaft body, and is matched with the transmission locking mechanism The compression curve set in the chute ensures that the hatch is locked and at the same time realizes uniform compression of the radial sealing ring.
(4)通过设置导向机构保证舱门闭合后传动锁紧机构能够精准处于对接位,其能够通过力反馈来判断门体结构是否到达密封位置。(4) By setting the guide mechanism to ensure that the transmission locking mechanism can be accurately in the docking position after the hatch is closed, it can judge whether the door body structure has reached the sealing position through force feedback.
(5)传动锁紧机构锁紧时,连杆与门体结构的径向重合,此时处在连杆转动的死点位置,处在死点位置的连杆可以实现自锁效果。(5) When the transmission locking mechanism is locked, the radial direction of the connecting rod and the door structure coincides, and at this time it is at the dead point of the connecting rod rotation, and the connecting rod at the dead point can realize the self-locking effect.
(6)在门体结构的外侧柱体上设置的双层密封圈,使其在遇到内外压力差时舱门两侧不受影响,可以保证两侧具有一致的良好承压能力。(6) The double-layer sealing ring arranged on the outer cylinder of the door body structure makes the two sides of the hatch door unaffected when encountering the internal and external pressure difference, which can ensure that both sides have consistent good pressure bearing capacity.
(7)本发明采用浮动门轴和导向机构相结合的方式,实现了舱门转动灵活、开关便利以及力反馈的功能,从而满足了舱门的人机工效学要求。采用径向密封、浮动门轴、多点压紧以及门体和门框的匹配设计,能够实现舱门两侧均有一个大气压压差条件下的密封功能。(7) The present invention adopts the combination of the floating door shaft and the guide mechanism to realize the functions of flexible hatch door rotation, convenient opening and closing, and force feedback, thereby meeting the ergonomic requirements of the hatch door. The radial seal, floating door shaft, multi-point pressing and matching design of the door body and door frame can realize the sealing function under the condition of an atmospheric pressure difference on both sides of the hatch.
附图说明Description of drawings
为了更清楚地说明本发明实施例的技术方案,下面将对实施例中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。In order to illustrate the technical solutions of the embodiments of the present invention more clearly, the accompanying drawings used in the embodiments will be briefly introduced below. Obviously, the accompanying drawings in the following description are only some embodiments of the present invention. Those of ordinary skill in the art can also obtain other drawings based on these drawings without any creative effort.
图1为本发明的空间双向承压舱门的正面示意图;Fig. 1 is the front schematic view of the space two-way pressurized hatch of the present invention;
图2为本发明的空间双向承压舱门的背面示意图;Fig. 2 is a schematic diagram of the back side of the space two-way pressure-bearing hatch of the present invention;
图3为本发明中的驱动机构爆炸示意图;Fig. 3 is the exploding schematic diagram of driving mechanism among the present invention;
图4为本发明舱门锁紧与打开状态时的传动原理示意图,其中(a)为锁紧状态,(b)为打开状态;Fig. 4 is a schematic diagram of the transmission principle when the cabin door of the present invention is locked and opened, wherein (a) is the locked state, and (b) is the opened state;
图5为本发明中的传动锁紧机构示意图;Fig. 5 is a schematic diagram of the transmission locking mechanism in the present invention;
图6为本发明中采用的密封圈的径向剖面图;Fig. 6 is the radial sectional view of the sealing ring adopted in the present invention;
图7为本发明中的门轴机构示意图及爆炸图;Fig. 7 is a schematic diagram and an exploded view of the door shaft mechanism in the present invention;
图8为本发明中的导向机构示意图及爆炸图。Fig. 8 is a schematic diagram and an exploded view of the guiding mechanism in the present invention.
其中:1-驱动机构,2-舱内指针,3-门轴机构,4-门体结构,5-舱内平衡阀,6-连杆,7-主轴套,8-导向机构,9-舱内把手,10-传动锁紧机构,11-门框结构,12-开关转动手柄,13-舱外操作接口及指针,14-舱外把手,15-舱外平衡阀,16-双层密封圈,17-主轴,18-舱门锁止阀,19-行星齿轮,20-滑块,21-门轴机构舱门框固件,22-门轴轴体,23-拉紧弹簧,24-门轴机构舱门固件,25-拉紧弹簧固定螺丝,26-导向槽,27-导向滑轮,28-导向辊,29-导向弹簧。Among them: 1-driving mechanism, 2-pointer in the cabin, 3-door shaft mechanism, 4-door body structure, 5-balance valve in the cabin, 6-connecting rod, 7-main shaft sleeve, 8-guiding mechanism, 9-cabin Inner handle, 10-transmission locking mechanism, 11-door frame structure, 12-switch rotation handle, 13-outside operation interface and pointer, 14-outside handle, 15-outside balance valve, 16-double-layer sealing ring, 17-main shaft, 18-door lock valve, 19-planetary gear, 20-slider, 21-door shaft mechanism door frame firmware, 22-door shaft body, 23-tension spring, 24-door shaft mechanism cabin Door hardware, 25-tension spring set screw, 26-guide groove, 27-guide pulley, 28-guide roller, 29-guide spring.
具体实施方式Detailed ways
下面结合附图并举实施例,对本发明进行详细描述。The present invention will be described in detail below with reference to the accompanying drawings and examples.
本实施例所描述的用于解释本发明,但不仅仅限于本发明。为使公众对本发明有更好的了解,下文的描述为一些特定的细节部分。The description in this embodiment is used to explain the present invention, but not only to limit the present invention. To enable the public to have a better understanding of the present invention, the following description includes some specific details.
实施例1:Example 1:
本实施例提供一种作为载人飞行器相邻两个舱段之间的接口的空间双向承压舱门,采用中心加载的多胞连杆滑块实现舱门的旋转开关操作,同时结合径向双层密封圈实现了舱门的双向承压密封。This embodiment provides a space two-way pressurized hatch as an interface between two adjacent compartments of a manned aircraft. A center-loaded multicellular connecting rod slider is used to realize the rotary switch operation of the hatch. The double-layer sealing ring realizes the two-way pressure-bearing sealing of the hatch.
令通过该舱门相连的两个舱段分别为舱段A和舱段B,为描述的方便,令舱门朝向舱段A的一面为舱内侧,朝向舱段B的一面为舱外侧;即本例中的舱外并不是指外界环境。Let the two compartments connected by the hatch door be compartment A and compartment B respectively. For the convenience of description, let the side of the hatch door facing compartment A be the interior of the compartment, and the side facing compartment B be the exterior of the compartment; that is The outside of the cabin in this example does not refer to the external environment.
如图1和图2所示,该空间双向承压舱门整体为圆形结构,包括:驱动机构1、门轴机构3、门体结构4、传动锁紧机构10和门框结构11。As shown in Figures 1 and 2, the two-way pressurized cabin door in this space has a circular structure as a whole, including: a driving mechanism 1, a
用于实现对该舱门进行操作(打开或关闭)的操作元件包括:舱内把手9、开关转动手柄12、舱外操作接口及指针13、舱外把手14。The operating elements for realizing the operation (opening or closing) of the cabin door include: a cabin handle 9 , a switch rotation handle 12 , an outside operation interface and a pointer 13 , and an
门框结构11为设置在载人航天器舱体上的环形框架,作为门体结构4与载人航天器的连接基座;门框结构11上设有与门体结构4相匹配的端框;门体结构4一端通过门轴机构3铰接在门框结构11上,门体结构4可绕门轴机构3转动,并与端框配合实现门体结构4相对门框结构11的打开和关闭;本例中该舱门为侧开方式,由此门体结构4左侧或右侧中间位置通过门轴机构3铰接在门框结构11上。且在舱段A或舱段B内,均能够采用向内或向外打开门体结构4的方式实现舱门的打开,为方便操作,在门体结构4的两端面均设置有把手,分别为舱内把手9和舱外把手14。The door frame structure 11 is an annular frame arranged on the cabin of the manned spacecraft, as the connection base between the
如图3所示,驱动机构1用于驱动传动锁紧机构10;驱动机构1安装在门体结构4一侧端面上,本例中,驱动机构1安装在门体结构4舱内侧的端面上。驱动机构1包括:主轴套7以及行星齿轮系;其中行星轮系包括:主轴17以及在围绕主轴17呈正三角状态分布的三个行星齿轮19;主轴套7安装在门体结构4的中心位置;行星轮系和开关转动手柄12分别设置在主轴套7的端面两侧;主轴套7朝向行星轮系所在侧沿其轴向延伸有环形凸起,环形凸起的内圆周面加工有内齿;主轴17的一端穿过主轴套7的中心孔后固定开关转动手柄12,作为舱内侧驱动机构1的操作端;另一端通过门体结构4的中心孔伸出门体结构4(主轴17穿过门体结构4,由动密封实现密封)与舱外侧的舱外操作接口及指针13相连;主轴17中部固接有主轴齿轮,三个行星齿轮19分别与主轴齿轮啮合;同时三个行星齿轮19分别与主轴套7上的内齿啮合。As shown in Figure 3, the driving mechanism 1 is used to drive the transmission locking mechanism 10; the driving mechanism 1 is installed on the end face of one side of the
由此通过开关转动手柄12转动主轴17时,行星齿轮系能够将开关转动手柄12提供的中心驱动力通过与主轴齿轮啮合的行星齿轮19传递给主轴套7,通过开关转动手柄12的大运动量转化为主轴套7很小的转动;由此驱动机构1通过二级降速驱动力矩控制传动锁紧机构10达到省力并精准控制行程的效果。Thus, when the main shaft 17 is turned by the
此外,为避免扰动导致主轴17的转动,在门体结构4上固定有舱门锁止阀18,主轴17上设置有与舱门锁止阀18配合的锁止槽;当舱门处于关闭且锁紧状态或解锁打开状态时,舱门锁止阀18的锁止芯位于主轴17上的锁止槽内,以限制主轴17转动。In addition, in order to avoid the rotation of the main shaft 17 caused by disturbance, a hatch lock valve 18 is fixed on the
如图4和图5所示,传动锁紧机构10包括:十二根连杆6以及与十二根连杆6一一对应的滑块20;在门体结构4的外圆周以及门框结构11的内圆周均设置有沿圆周均匀间隔分布有十二个条形槽,当舱门处于关闭状态时,门体结构4上的条形槽和门框结构11上的条形槽一一对接形成用于使滑块20滑动的滑槽。十二个滑槽与十二个连杆机构一一对应铰接。主轴套7外圆周沿周向均匀间隔分布有十二个铰接点;十二根连杆6的一端分别与主轴套7上的十二个铰接点铰接,另一端铰接的滑块20分别位于十二个滑槽内,与滑槽滑动配合。门框结构11上每个滑槽内设置有压紧点,用于和滑块20配合,实现门体结构4与门框结构11之间的压紧。As shown in Figures 4 and 5, the transmission locking mechanism 10 includes: twelve connecting rods 6 and
传动锁紧机构10中连杆6的运动通过主轴套7来控制,通过连杆6来带动滑块20进行更加平稳顺畅地运动,进而实现舱门的锁紧和解锁。传动锁紧机构10锁紧时,连杆6与门体结构4的径向重合,如图4中的(a)所示;此时处在连杆转动的死点位置,处在死点位置的连杆可以达到自锁效果。且传动锁紧机构10中采用十二个滑槽能够较好地对滑块20的行动轨迹进行准确限制。The movement of the connecting rod 6 in the transmission locking mechanism 10 is controlled by the main shaft sleeve 7, and the sliding
传动锁紧机构10解锁和锁紧运动过程中的运动量相对于其他传动机构较小,同时将主轴套7置于门体结构4的中心位置,成功地避免了十二根连杆6之间发生运动干涉。且设计时使主轴套7的尺寸与连杆6相配合,通过主轴套7扩大连杆6的连接周长,可以避免连杆6之间发生运动干涉,并且实现滑块20良好的伸缩同步性。The amount of movement during the unlocking and locking movement of the transmission locking mechanism 10 is relatively small compared with other transmission mechanisms, and at the same time, the main shaft sleeve 7 is placed at the center of the
此外,为直观的显示传动锁紧机构10解锁和锁紧状态,在门体结构4舱内侧设置有舱内指针2,通过舱内指针2指示传动锁紧机构10的状态。舱外侧通过舱外操作接口及指针13中的指针指示传动锁紧机构10的状态。In addition, in order to visually display the unlocked and locked state of the transmission locking mechanism 10 , an in-
如图6所示,在门体结构4和门框结构11之间设置有双层密封圈16,用于门体结构4和门框结构11之间的密封。具体的:双层密封圈16位于门体结构4的圆柱结构的外圆周面上,即门体结构4和门框结构11之间采用径向密封的方式,由于密封效果只与双层密封圈16自身的弹性性能有关,故可以实现双向承压能力一致的良好效果。As shown in FIG. 6 , a double-
此外,门体结构4的舱内侧和舱外侧分别设置有舱内平衡阀5与舱外平衡阀15,用于在门体结构4关闭时保持密封,门体结构4开启前形成气流通道以平衡舱门两侧气压,便于舱门开启。In addition, the inside of the
该空间双向承压舱门能够实现舱门解锁打开与关闭锁紧这两个可重复性实现的功能,具体为:The two-way pressurized cabin door of this space can realize the two repeatable functions of unlocking, opening and closing and locking of the cabin door, specifically:
(1)关闭锁紧功能:在舱门打开状态下,若需要关闭舱门,先利用舱内把手9或舱外把手14关闭门体结构4后;操作者旋转开关转动手柄12带动主轴17作旋转运动,将驱动力通过行星齿轮19放大并传递到与主轴套7连接的十二根连杆6上,带动与其相连的滑块20在滑槽内同步向外滑动,使滑块20进入位于门框结构11上的滑槽内,直至滑块20顶端接触到滑槽内的压紧点,即,使得滑块20沿舱门径向运动至锁紧位置,此时传动锁紧机构10处于图4中的(a)所显示的状态。(1) Close the locking function: when the hatch is open, if you need to close the hatch, first use the handle 9 or the
(2)解锁打开功能:在锁紧密封状态下,若需要打开舱门,当舱内外存在较大的压力差时,很难直接将舱门打开,此时首先舱门内的操作者需要手动打开安装在门体结构4上的舱内平衡阀5,以平衡舱门内外两侧的压力。当舱内外压差较小时,无需进行舱门内外两侧压力平衡的操作。然后,操作者反向旋转开关转动手柄12,通过主轴17带动十二根连杆6转动,使十二个滑块20在滑槽内后退,脱离压紧点,直至从门框结构11上的滑槽内退出,缩回至门体结构4上的滑槽内,实现门体结构4的解锁,此时传动锁紧机构10处于图4中的(b)所显示的状态。之后,操作者拉动舱内把手9,使门体结构4绕门轴机构3转动,便可实现舱门的开启。(2) Unlocking and opening function: In the locked and sealed state, if the hatch door needs to be opened, when there is a large pressure difference between the inside and outside of the cabin, it is difficult to open the hatch door directly. Open the cabin balance valve 5 installed on the
该舱门结构合理,解锁打开与关闭锁紧操作简单,而且所需的操作力不大,可靠性高,承压能力强,可以保证在各种环境下开启。同时,由于舱门高刚度锁紧设计结合径向双冗余密封压缩设计,可以双向承压。The cabin door has a reasonable structure, simple operation of unlocking, opening, closing and locking, requires little operating force, high reliability, strong pressure bearing capacity, and can be opened under various environments. At the same time, due to the high-rigidity locking design of the hatch combined with the radial double redundant seal compression design, it can bear pressure in both directions.
实施例2:Example 2:
在上述实施例1的基础上,给出门轴机构3的一种较优实施例。On the basis of the above-mentioned embodiment 1, a preferred embodiment of the
门轴机构3为浮动式门轴机构,用于实现门体结构4与门框结构11之间的连接以及门体结构4相对门框结构11的转动、平动。The
如图7所示,门轴机构3包括:门轴机构舱门框固件21、门轴轴体22、拉紧弹簧23、门轴机构舱门固件24以及拉紧弹簧固定螺丝25。As shown in FIG. 7 , the
门轴机构舱门框固件21固定在门框结构11上,作为门轴机构3的安装座;门轴机构舱门框固件21上设置有用于安装门轴轴体22的支耳;门轴机构舱门固件24的一端与门体结构4固接,另一端套装在门轴轴体22上;门轴轴体22为门体结构4相对门框结构11打开和关闭时的旋转轴,即门轴机构舱门固件24能够绕门轴轴体22的轴线转动。鉴于本例中舱门为侧开方式,门轴轴体22的轴向沿竖直方向。The door shaft mechanism cabin door frame firmware 21 is fixed on the door frame structure 11 as the mounting seat of the
门轴机构舱门固件24通过长方形孔(或腰形孔)套装在门轴轴体22上,拉紧弹簧23的一端套装在门轴轴体22上,另一端通过拉紧弹簧固定螺丝25与门轴机构舱门固件24相连;拉紧弹簧23的伸缩方向与长方形孔的长度方向一致长方形孔的长度方向沿门体结构4的轴向。通过设置长方形孔使门轴机构舱门固件24与门轴轴体22之间具有沿门体结构4轴向的容差,从而使门体结构4与门轴轴体22之间具有一定的活动间隙,使得门体结构4具有轴向浮动(即门体结构4相对门框结构11的平动),保证舱门的顺利开启与关闭;而在门轴轴体22与门轴机构舱门固件24之间设置的拉紧弹簧23,能够在舱门关闭时,拉紧门轴机构舱门固件24,Door shaft mechanism
在门体结构4相对门框结构11平动的基础上,在门框结构11上的条形槽的端部设置压紧曲面,即门框结构11上条形槽的末端为沿门框结构11的轴向下沉的曲面结构,形成压紧曲面,并将该位置作为压紧点,滑块20端部具有滚轮;由此关闭舱门时,滑块20进入位于门框结构11上的滑槽内运动至压紧曲线所在位置后,其端部滚轮沿着压紧曲面移动,带动门体结构4轴向平移,以均匀压缩双层密封圈16,避免密封圈受力不均导致的单侧磨损;由此在滑块20运动的同时,带动门体结构4沿轴向压向门框结构11,使得门体结构4与门框结构11间的双层密封圈16压缩,从而实现舱门的锁紧密封功能。On the basis of the translation of the
此外,还可在门轴轴体22上设置有卷簧,通过调整卷簧的预紧力,实现舱门打开过程中任意位置的停留。In addition, a coil spring can also be provided on the
实施例3:Example 3:
在上述实施例1或实施例2的基础上,进一步的还设置有导向机构8,并给出导向机构8的一种较优实施例。On the basis of the above embodiment 1 or
导向机构8用于门体结构4闭合时的导向;如图8所示,导向机构8位于门框结构11与门体结构4之间,包括:导向槽26和导向辊28;其中导向槽26固定在门框结构11上(且位于门框结构11上门轴机构3的相对侧,即与门轴机构3位于同一径向),导向槽26的开槽方向与门框结构11的轴向平行,且导向槽具有喇叭状开口;门体结构4外圆周具有导向槽26滑动配合的凸起柱体。The guide mechanism 8 is used for guiding when the
导向槽26的外侧(开槽面的相对侧)具有与该侧面垂直的套筒;导向辊28位于该套筒内,与该套筒滑动配合;导向辊28一端端部设置有滑轮27,导向槽26内与滑轮27对应位置设置有开孔;导向辊28的另一端通过导向弹簧29与套筒的内底面相连。导向弹簧29处于自然状态下,滑轮27凸出于导向槽26内底面上的开孔。The outside of guide groove 26 (opposite side of grooved surface) has the sleeve perpendicular to this side;
当舱门关闭时,门体结构4上的凸起柱体先与导向槽26喇叭状开口接触,校正门体结构4位置;继续关闭门体结构4,门体结构4上的凸起柱体在导向槽26内移动至滑轮27所在位置后挤压滑轮27;滑轮27带动导向辊28后移压缩导向弹簧29,直至凸起柱体越过滑轮27,导向弹簧29回弹,此时判断门体结构4已到达密封位置。When the cabin door was closed, the protruding cylinder on the
导向槽26内开有观察孔,能够观察到导向辊28上导向弹簧29的压缩情况,从而判断门体结构4关闭进程;并且导向弹簧29回弹可以给予操作者力反馈,操作者可通过力反馈与导向辊28的位置变化判断门体结构4的关闭进程。There is an observation hole in the
在具有导向机构8后,关闭舱门时,利用舱内把手9或舱外把手14关闭门体结构4,直至门体结构4顺利导入导向机构8的导向槽26,从导向槽26开孔处观察导向弹簧29的压缩情况,当导向弹簧29发生一次压缩回弹过程后,即判断门体结构4已到达密封位置。After having the guide mechanism 8, when closing the cabin door, utilize the handle 9 or the
且由于导向机构8与浮动式门轴机构3的约束,门体结构4只会发生轴向浮动,不会影响到位于舱门侧面的双层密封圈16的密封效果。Moreover, due to the constraints of the guide mechanism 8 and the floating
综上,以上仅为本发明的较佳实施例而已,并非用于限定本发明的保护范围。凡在本发明的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。To sum up, the above are only preferred embodiments of the present invention, and are not intended to limit the protection scope of the present invention. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present invention shall be included within the protection scope of the present invention.
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