CN103604597A - Cabin door mounting system - Google Patents
Cabin door mounting system Download PDFInfo
- Publication number
- CN103604597A CN103604597A CN201310651548.8A CN201310651548A CN103604597A CN 103604597 A CN103604597 A CN 103604597A CN 201310651548 A CN201310651548 A CN 201310651548A CN 103604597 A CN103604597 A CN 103604597A
- Authority
- CN
- China
- Prior art keywords
- connecting rod
- hatch door
- cabin door
- position joint
- joint
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Images
Landscapes
- Hinges (AREA)
- Support Devices For Sliding Doors (AREA)
Abstract
The invention belongs to the cabin door mounting technology, and specifically relates to a cabin door mounting system. The cabin door mounting system comprises a cabin door, a retractable connecting rod, a base, a sidewall, a brace, an open position connector, a closed position connector, a middle position connector and a hinge connector, wherein one end of the cabin door is connected with the sidewall through a hinge connecting point, while the other end of the cabin door is fixed on the open position connector ( the closed position connector or the middle position connector) according to mounting position requirements through the retractable connecting rod; one end of the retractable connecting rod is articulated to the middle part of the inner wall of the cabin door; the other end of the retractable connecting rod is articulated with the closed position connector located on the base, or the open position connector or the middle position connector located on the brace. The cabin door mounting system provided by the invention is characterized in that the direction of the retractable connecting rod is adjusted and the connection position of the retractable connecting rod is changed to complete the switching of the test gestures of the cabin door, and the gesture of the main body of the cabin door is stable; therefore, the cabin door mounting system is quick in test reloading and convenient to use; consequently, the labor intensity of mounting is alleviated.
Description
Technical field
The invention belongs to hatch door field engineering, be specifically related to a kind of installation system of hatch door.
Background technology
The hatch door of the means of transport such as aircraft or automobile, boats and ships has unique mounting structure.During actual test, need special testing equipment to install.
The support of existing undercarriage hatch door testpieces is to support and two kinds of modes of design specialized supporting structure in airframe real structure.By the real jack of aircraft or design, produce and a plurality ofly to there is the support that can meet specific inclination angle and realize the test needs of hatch door in different folding situations.
The test method of supporting with fuselage real structure, installs due to the real jack of needs device or otherwise designed analogue means, and test unit is more complicated, reference field disunity when test is installed, and installation accuracy requires to be difficult for guaranteeing.
As adopted, keep the supportive device of the specific mounted angle of hatch door to test, need design to produce the multiple test gripping clamping apparatus of hatch door in different folding situations, versatility is not strong, increased production cost, and during due to test, testpieces installment state changes greatly, corresponding test unit all needs to adjust thereupon, and test implementation amount is larger.
Summary of the invention
The object of the invention: provide a kind of and can realize the hatch door installation system that hatch door multi-pose is supported and adjusted.
Technical scheme of the present invention: a kind of hatch door installation system, it comprises hatch door 7, folding and unfolding connecting rod 6, base 1, sidewall 9, pillar 2, open position joint 5, off-position joint 4, centre position joint 3, articulated joint 8.Wherein, undercarriage door 7 one end are connected with sidewall 9 by articulated joint 8, the other end requires to be fixed on open position joint 5(off-position joint 4 or centre position joint 3 by folding and unfolding connecting rod 6 according to installation site) on, described folding and unfolding connecting rod 6 one end are hinged on the middle part of hatch door 7 inwalls, the other end of folding and unfolding connecting rod 6 be positioned at the off-position joint on base 1 or be articulated and connected with the open position joint or the centre position joint 3 that are positioned on column.
On pillar 2, be provided with the centre position joint 3 that can be hinged with folding and unfolding connecting rod 6.
When off-position joint 4 is positioned at sidewall 9 outside, on sidewall 9, offer the gap of passing through for folding and unfolding connecting rod 6.
Described pillar 2 is detachable stacked structure.
Technique effect of the present invention: hatch door installation system of the present invention is by adjusting folding and unfolding connecting rod 6 directions, change jointing position and complete the conversion that hatch door is tested attitude, hatch door 7 subjective postures are motionless, thereby test changes the outfit quick, easy to usely, alleviated the labour intensity of installing; And two kinds of trystates need only a set of gripping clamping apparatus, there is larger versatility.
Accompanying drawing explanation
Fig. 1 is hatch door installation system structural representation of the present invention;
Schematic diagram during Fig. 2 hatch door installation system closure state;
Schematic diagram during Fig. 3 hatch door installation system open mode,
Wherein, 1-base, 2-pillar, 3-centre position joint, 4-off-position joint, 5-open position joint, 6-folding and unfolding connecting rod, 7-hatch door, 8-articulated joint, 9-sidewall.
Embodiment
Below in conjunction with embodiment and accompanying drawing, the present invention is described further:
Hatch door installation system of the present invention comprises hatch door 7, folding and unfolding connecting rod 6, base 1, sidewall 9, pillar 2, open position joint 5, off-position joint 4, centre position joint 3, articulated joint 8.Wherein, hatch door 7 one end are connected with sidewall 9 by articulated joint 8, the other end is fixing by folding and unfolding connecting rod 6, hatch door folding and unfolding connecting rod 6 one end are hinged on the middle part of undercarriage door inwall, the other end of hatch door folding and unfolding connecting rod 6 be positioned at the off-position joint 4 on base or be articulated and connected with the open position joint 5 being positioned on pillar 2.
On pillar 2, be provided with the centre position joint 3 that can be hinged with hatch door folding and unfolding connecting rod 6, for realizing the support of centre position attitude.
When off-position joint 4 is positioned at sidewall 9 outside, on sidewall 9, offers the gap of passing through for hatch door folding and unfolding connecting rod 6, thereby can avoid the interference of sidewall 9 and hatch door folding and unfolding connecting rod 6.
Described pillar 2 is detachable stacked structure, thereby facilitates height control, is applicable to different hatch door structures, improves versatility.
In actual use, base 1 is fixed on to ground, hatch door 7 one end are installed on to articulated joint 8, hatch door folding and unfolding connecting rod 6 is fixed on off-position joint 4 and completes the installation of hatch door system closure state.When needs carry out hatch door system opening installation state, only hatch door folding and unfolding connecting rod 6 need be untied from off-position joint 4, be connected in open position joint 5.Equally, when needs carry out the middle installment state of hatch door system, only hatch door folding and unfolding connecting rod 6 need be untied from off-position joint 4, be connected in centre position joint 3.
When conversion Installation posture, only need be connected with correspondence position joint and can complete closing, opening and centre position Installation posture of hatch door by change folding and unfolding connecting rod angle.Its advantage is: only need a covering device can complete the installation of multiple hatch door attitude; Only by folding and unfolding connecting rod position, change the state of realization and change, in application, reduce the work that changes the outfit; Hatch door profile attitude is constant, can make hatch door in constant position, improve the comparability of test result.
Claims (5)
1. a hatch door installation system, it is characterized in that, comprise hatch door (7), folding and unfolding connecting rod (6), base (1), sidewall (9), pillar (2), open position joint (5), centre position joint (3), off-position joint (4), articulated joint (8), hatch door (7) one end is connected with sidewall (9) by hinged contact (8), the other end requires to be fixed on open position joint (5) or off-position joint (4) or centre position joint (3) according to installation site by folding and unfolding connecting rod (6), described folding and unfolding connecting rod (6) one end is hinged on the middle part of hatch door (7) inwall, the other end of folding and unfolding connecting rod (6) be positioned at the off-position joint on base (1) or be articulated and connected with the open position joint or the centre position joint (3) that are positioned on column.
2. hatch door installation system according to claim 1, is characterized in that, is provided with the centre position joint (3) that can be hinged with folding and unfolding connecting rod (6) on pillar (2).
3. hatch door installation system according to claim 1, is characterized in that, open position joint (5), off-position joint (4) and centre position joint (3) are open type auricle joint.
4. hatch door installation system according to claim 1, is characterized in that, when off-position joint (4) is positioned at sidewall (9) outside, offers the gap of passing through for hatch door folding and unfolding connecting rod (6) on sidewall (9).
5. hatch door installation system according to claim 1, is characterized in that, described pillar (2) is detachable stacked structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310651548.8A CN103604597B (en) | 2013-12-04 | 2013-12-04 | A kind of hatch door installation system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310651548.8A CN103604597B (en) | 2013-12-04 | 2013-12-04 | A kind of hatch door installation system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103604597A true CN103604597A (en) | 2014-02-26 |
| CN103604597B CN103604597B (en) | 2016-04-20 |
Family
ID=50122842
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310651548.8A Active CN103604597B (en) | 2013-12-04 | 2013-12-04 | A kind of hatch door installation system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103604597B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112455647A (en) * | 2020-11-13 | 2021-03-09 | 中国航空工业集团公司沈阳飞机设计研究所 | Aircraft landing gear cabin door suspension structure |
| CN113607559A (en) * | 2021-07-14 | 2021-11-05 | 武汉航达航空科技发展有限公司 | Static test platform for cockpit door |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060202087A1 (en) * | 2005-03-11 | 2006-09-14 | Mortland Michael T | Aircraft door hinge assembly |
| CN201633919U (en) * | 2010-01-07 | 2010-11-17 | 哈尔滨飞机工业集团有限责任公司 | Cabin door stay bar for airplane |
| CN202305227U (en) * | 2011-10-06 | 2012-07-04 | 郑州宇通客车股份有限公司 | Carriage hand-operated upturning luggage compartment door endurance testing stand |
| US20120305336A1 (en) * | 2011-05-31 | 2012-12-06 | Willy Walker | Variable door coupling |
| CN202686545U (en) * | 2012-08-02 | 2013-01-23 | 宁波吉江汽车制造有限责任公司 | Side cabin door of passenger car |
| CN203050315U (en) * | 2012-12-18 | 2013-07-10 | 北汽福田汽车股份有限公司 | Cabin door installation structure and passenger vehicles |
| CN203129788U (en) * | 2012-12-21 | 2013-08-14 | 中航通飞研究院有限公司 | Supporting mechanism for opening state of airplane cabin door |
-
2013
- 2013-12-04 CN CN201310651548.8A patent/CN103604597B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060202087A1 (en) * | 2005-03-11 | 2006-09-14 | Mortland Michael T | Aircraft door hinge assembly |
| CN201633919U (en) * | 2010-01-07 | 2010-11-17 | 哈尔滨飞机工业集团有限责任公司 | Cabin door stay bar for airplane |
| US20120305336A1 (en) * | 2011-05-31 | 2012-12-06 | Willy Walker | Variable door coupling |
| CN202305227U (en) * | 2011-10-06 | 2012-07-04 | 郑州宇通客车股份有限公司 | Carriage hand-operated upturning luggage compartment door endurance testing stand |
| CN202686545U (en) * | 2012-08-02 | 2013-01-23 | 宁波吉江汽车制造有限责任公司 | Side cabin door of passenger car |
| CN203050315U (en) * | 2012-12-18 | 2013-07-10 | 北汽福田汽车股份有限公司 | Cabin door installation structure and passenger vehicles |
| CN203129788U (en) * | 2012-12-21 | 2013-08-14 | 中航通飞研究院有限公司 | Supporting mechanism for opening state of airplane cabin door |
Non-Patent Citations (1)
| Title |
|---|
| 邵骞: "简支条件大跨度高梁试验技术研究与应用", 《工程与试验》, vol. 50, no. 2, 31 May 2010 (2010-05-31) * |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112455647A (en) * | 2020-11-13 | 2021-03-09 | 中国航空工业集团公司沈阳飞机设计研究所 | Aircraft landing gear cabin door suspension structure |
| CN112455647B (en) * | 2020-11-13 | 2023-08-22 | 中国航空工业集团公司沈阳飞机设计研究所 | Aircraft landing gear cabin door hanging structure |
| CN113607559A (en) * | 2021-07-14 | 2021-11-05 | 武汉航达航空科技发展有限公司 | Static test platform for cockpit door |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103604597B (en) | 2016-04-20 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106596029A (en) | Wing pneumatic load follow-up loading device | |
| WO2013107123A1 (en) | Mechanical arm control system, method and engineering machinery | |
| CN103604597A (en) | Cabin door mounting system | |
| CN203259333U (en) | Durable testing apparatus for luggage case cover of automobile | |
| CN105258912B (en) | A kind of low-speed wind tunnel model test support meanss based on internal balance | |
| CN105382843A (en) | Coordination control method for mechanical arm and operation platform in final stage of grabbing | |
| CN206634197U (en) | A kind of aircraft wing equipment hanger | |
| CN104091475A (en) | Mobile multifunctional classroom | |
| CN205209730U (en) | Wind -tunnel bearing structure | |
| CN105021414A (en) | Movable wing surface servo loading device | |
| CN102909152A (en) | Foldable telescopic spray bar frame | |
| CN104159813A (en) | Mounting frame for a vehicle door | |
| CN202893587U (en) | Foldable and telescopic spray lance frame | |
| CN206382143U (en) | A kind of transmission line of electricity paint finishing based on unmanned plane | |
| CN205228763U (en) | Low speed wind tunnel model test strutting arrangement based on internal balance | |
| CN205052029U (en) | Regulator cubicle gate -type connector mounting panel | |
| CN107063707B (en) | Air power steering tubing string regulating mechanism fatigue test board | |
| CN104060855B (en) | A kind of glass sunlight house | |
| CN206470526U (en) | A kind of computer teaching curtain device | |
| CN203996550U (en) | A kind of electric cabinet controller Telescopic installing support | |
| CN205134658U (en) | Hyperboloid fossil fragments connecting device | |
| CN104150408B (en) | Work high above the ground work platform erection mechanism | |
| CN103253377B (en) | Method for curved docking with airplanes | |
| CN108489702B (en) | Double-channel aerodynamic loading test device of double-pendulum thrust vectoring nozzle | |
| CN110295917A (en) | Drill jumbo span device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |