CN102914322B - Cabin door sensor mounting seat - Google Patents

Cabin door sensor mounting seat Download PDF

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Publication number
CN102914322B
CN102914322B CN201210454929.2A CN201210454929A CN102914322B CN 102914322 B CN102914322 B CN 102914322B CN 201210454929 A CN201210454929 A CN 201210454929A CN 102914322 B CN102914322 B CN 102914322B
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China
Prior art keywords
sliding sleeve
target
seat
target seat
sleeve
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CN201210454929.2A
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Chinese (zh)
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CN102914322A (en
Inventor
何明松
李芳�
付友波
路航
田世雄
宋艳龙
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Xian Aircraft Industry Group Co Ltd
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Xian Aircraft Industry Group Co Ltd
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Priority to CN201210454929.2A priority Critical patent/CN102914322B/en
Publication of CN102914322A publication Critical patent/CN102914322A/en
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Publication of CN102914322B publication Critical patent/CN102914322B/en
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Abstract

The invention discloses a cabin door mounting seat. According to the cabin door sensor mounting seat, one end of a sliding sleeve provided with a sliding surface is positioned in a supporting sleeve; one end of a target seat provided with a sliding surface is arranged in the sliding sleeve and is in sliding fit with the inner surface of the sliding sleeve; an inner spring is arranged in an inner hole of the sliding sleeve and is matched with an end face of the sliding surface end of the target seat; a fine adjustment bolt is arranged at the other end of the inner hole of the sliding sleeve; an outer spring is sleeved on the outer surface of one end of the sliding sleeve; and an induction surface of the target seat is positioned at one end of the target seat and is matched with the end face of the target seat. During use, a sensor is arranged on a mounting box, and the requirement of the effective working distance of the sensor is met through the fine adjustment bolt; when a cabin door handle is rotated anticlockwise, a rocker is driven to rotate to a horizontal position, a door fork presses down a tongue piece, and the distance between the induction surface of the sensor and the target is always in an inductive range under the action of the inner spring; and when the cabin door handle is rotated clockwise, the target is separated from a working area under the action of the outer spring, and the sensor warns opening of the cabin door. According to the tests, when the cabin door is opened and closed every 100 times averagely, the error indication phenomenon time of a warning lamp is zero.

Description

A kind of hatch door sensor installation seat
Technical field
The present invention relates to aeroplane structure design field, specifically a kind of hatch door sensor installation seat.
Background technology
The afterbody hatch door of certain type machine is the entrance door of fuselage deck store, and its Main Function is that the maintenance for deck store structure and control system provides passage.Aircraft is in flight course, and this door and other hatch door common guarantee fuselage interior are airtight, on its frame door, are provided with door lock and alarm switch, and when hatch door is during in correct off-position, alarm switch extinguishes the stand by lamp of driving cabin; When hatch door is in an open position, alarm switch makes stand by lamp bright aobvious, and whole process realizes by the mechanical motion between door lock and alarm switch.
Original structure is that door fork directly contacts with alarm switch.Owing to manufacturing assembly precision, the reason such as in flight course the working range of the distortion of housing construction under inside and outside differential pressure effect and switch itself is less, if adopt original structure may occur the phenomenon that stand by lamp mistake is indicated.
Summary of the invention
For overcoming the deficiency that there will be the indication of stand by lamp mistake existing in prior art, the present invention proposes a kind of hatch door sensor installation seat.
The present invention includes target, spring, trimming bolt, target seat and sliding sleeve, outer spring, inner spring and stop sleeve.Wherein:
The present invention includes target, spring, trimming bolt, target seat and sliding sleeve, outer spring, stop sleeve; Wherein: sliding sleeve has slipping plane one end to be arranged in stop sleeve, and the inside surface that is positioned at this sliding sleeve slipping plane end and stop sleeve be slidably matched.Target seat has slipping plane one end to be arranged in sliding sleeve, and the slipping plane of this target seat and the inside surface of sliding sleeve are slidably matched.Inner spring is arranged in sliding sleeve endoporus, and coordinates with the end face of target seat slipping plane end; Trimming bolt is arranged on the other end of sliding sleeve endoporus.Outer spring is sleeved on the outer round surface of sliding sleeve one end.The sensitive surface of described target seat is positioned at target seat one end, and the sensitive surface of this target seat coordinates with the end face of target seat.
The internal diameter of described sliding sleeve is identical with the external diameter of end plate that forms slipping plane on target seat.There is end plate sliding sleeve one end, and the external diameter of this end plate is greater than the external diameter of sliding sleeve, and identical with the internal diameter of stop sleeve.The slipping plane that the circumferential surface of described sliding sleeve one end end plate is sliding sleeve.There is the mounting hole of target seat at the center of described sliding sleeve one end end plate, and the aperture of this mounting hole is identical with the external diameter of target seat, after target seat is arranged on the end plate of sliding sleeve, between described sliding sleeve and described target seat for being slidably matched.
The circumferential surface of described target seat one end has the boss radially protruding, and the circumferential surface of this boss has formed the slipping plane of target seat.The inside surface of the described target seat other end has the internal thread being connected with target.The internal diameter of described target seat is identical with the external diameter of target.
There is end plate described stop sleeve one end, and there is the mounting hole of sliding sleeve at the center of this end plate.The aperture of described sliding sleeve mounting hole is identical with the external diameter of sliding sleeve, and the aperture of described stop sleeve is identical with the external diameter of sliding sleeve end plate, makes to be slidably matched between described sliding sleeve and stop sleeve.
Described inner spring is arranged in sliding sleeve, and coordinates with the end face of target seat.Outer spring is sleeved on the circular surfaces of sliding sleeve, and coordinates with the outside surface of stop sleeve end plate.
The object of the present invention is to provide a kind of can coordination with airframe, and the housing construction of the installation of sensors use of providing convenience, control better stand by lamp and show hatch door On/Off.
During use, sensor level is arranged on mounting box, by trimming bolt, regulates size, to meet the effective working distance of sensor.When being rotated counterclockwise hatch door handle, drive rocking arm to rotate to horizontal level, the lower spatula of door fork, can guarantee that under the effect of inner spring the sensitive surface of sensor and the distance of target are in induction range all the time.Even if externally vibration and structure, compared with in the situation of small deformation, still can be guaranteed the normal work of sensor, realize closing of sensor warning hatch door; The hatch door handle that turns clockwise, target departs from workspace under the effect of outer spring, realizes the unlatching of sensor warning hatch door.
For verifying effect of the present invention, the present invention to be tested on certain type machine, result is as follows:
Adopt prior art, average every 100 hatch door open and close there will be 2 stand by lamps to indicate phenomenon by mistake.
Adopt the present invention, it is zero that average every 100 hatch door open and close stand by lamps are indicated phenomenon by mistake.
Below in conjunction with implementing illustration, this application is described in further detail.
Accompanying drawing explanation
Fig. 1 is the structural representation of hatch door sensor installation seat;
Fig. 2 is the structural representation of target seat;
Fig. 3 is the structural representation of sliding sleeve;
Fig. 4 is the structural representation of stop sleeve;
Fig. 5 is hatch door sensor installation seat and the schematic diagram that coordinates of hatch door sensor;
Fig. 6 is the schematic diagram that hatch door sensor caution structure is used state.In figure:
1. inductor 2. inductor nut 3. inductor bearing 4. lining 5. tongue piece bearings
6. web member 7. target 8. target seat 9. inner spring 10. trimming bolts
11. 12. of tongue pieces fork, 13. outer spring 14. sliding sleeve 15. stop sleevees
Hatch door inductor caution structure of the present invention is comprised of spring, lining, target seat, sliding sleeve, adjusting bolt, bearing and tongue piece.Sensor level is arranged on mounting box, by trimming bolt, regulates size, to meet the effective working distance of sensor.
Embodiment
The present embodiment is a kind of hatch door sensor installation seat, comprises target 7, spring 9, trimming bolt 10, target seat 8 and sliding sleeve 14, outer spring 13, stop sleeve 15.Wherein, sliding sleeve 14 has slipping plane one end to be arranged in stop sleeve 15, and the inside surface that is positioned at these sliding sleeve 14 slipping plane ends and stop sleeve 15 is slidably matched.
Target seat 8 has slipping plane one end to be arranged in sliding sleeve 14, and the inside surface of the slipping plane of this target seat 8 and sliding sleeve 14 is slidably matched.Inner spring 9 is arranged in sliding sleeve 14 endoporus, and coordinates with the end face of target seat 8 slipping plane ends; Trimming bolt 10 is arranged on the other end of sliding sleeve 14 endoporus.
Outer spring 13 is sleeved on the outer round surface of sliding sleeve 14 1 ends.
Target 7 use can allow the metal of inductor work make, and in the present embodiment, target 7 is made of a steel.The sensitive surface of described target seat 7 is positioned at target seat 8 one end, and the sensitive surface of this target seat 7 coordinates with the end face of target seat 8; The straight-bar of described target seat 7 minor diameters is fixed in target seat 8.
Trimming bolt 10 is arranged on sliding sleeve 14 one end.
Described sliding sleeve 14 is circular shell.The internal diameter of sliding sleeve 14 is identical with the external diameter of end plate that forms slipping plane on target seat 8.There is end plate sliding sleeve 14 one end, and the external diameter of this end plate is greater than the external diameter of sliding sleeve 14, and identical with the internal diameter of stop sleeve 15, and the outer round surface that makes sliding sleeve 14 is stepped.The circumferential surface of described sliding sleeve 14 one end end plates is the slipping plane of sliding sleeve 14.There is the mounting hole of target seat 8 at the center of described sliding sleeve 14 one end end plates, and the aperture of this mounting hole is identical with the external diameter of target seat 8, after target seat 8 is arranged on the end plate of sliding sleeve 14, between described sliding sleeve 14 and described target seat 8 for being slidably matched.The bore area of sliding sleeve 14 other end terminations has screw thread.
Target seat 8 is circular shell.The circumferential surface of target seat 8 one end has the boss radially protruding, and the circumferential surface of this boss has formed the slipping plane of target seat 8.The inside surface of described target seat 8 other ends has the internal thread being connected with target 7.The internal diameter of described target seat 8 is identical with the external diameter of target 7.
Stop sleeve 15 is circular shell.There is end plate one end of stop sleeve 15, and there is the mounting hole of sliding sleeve 14 at the center of this end plate.The aperture of described sliding sleeve mounting hole is identical with the external diameter of sliding sleeve 14, and the aperture of described stop sleeve 15 is identical with the external diameter of sliding sleeve 14 end plates, makes to be slidably matched between described sliding sleeve 14 and stop sleeve 15.
Inner spring 9 is arranged in sliding sleeve 14, and coordinates with the end face of target seat 8.Outer spring 13 is sleeved on the circular surfaces of sliding sleeve 14, and coordinates with the outside surface of stop sleeve 15 end plates.
Described trimming bolt is sleeve-shaped.There is end plate one end at trimming bolt, and the external diameter of this end plate is greater than the external diameter of described sliding sleeve 14.External peripheral surface at described trimming bolt has the external thread coordinating with sliding sleeve 14.
Inductor bearing 3 is connected with housing construction by bolt.
The present embodiment, when work, links together the external peripheral surface of stop sleeve 15 and inductor bearing 3 by gluing.Inductor 1 is fixing with inductor bearing 3 by inductor nut 2, is then connected with web member 6; Tongue piece bearing 5 is connected with body; Tongue piece 11 can rotate by an axle on tongue piece bearing 5; Target 7 is connected with flexible target seat 8; Target seat 8 can be in the interior slip of sliding sleeve 14; Sliding sleeve 14 is in the interior slip of stop sleeve 15.When hatch door is closed, shift fork 12 is rotated counterclockwise to horizontal level, promote tongue piece 11 rotations, tongue piece 11 drives target seats 8 to move until target 7 enters induction zone and make inner spring 9 shrink certain distances, so just can guarantee the distortion that target and inductor can not produce because of aircraft in flight course and departs from workspace.When hatch door is opened, when shift fork 12 turns clockwise, mechanism restores under the effect of outer spring 13.Trimming bolt 10 is for regulating the stroke of target seat 8.
As shown in Figure 3, when 40 frame doors are closed, shift fork 12 is rotated counterclockwise to level, compression target seat, and when target 7 enters workspace, if continue to be moved to the left, target seat 8 shrinks to the right.

Claims (4)

1. a hatch door sensor installation seat, is characterized in that, comprises target, inner spring, trimming bolt, target seat and sliding sleeve, outer spring, stop sleeve; Wherein: sliding sleeve has slipping plane one end to be arranged in stop sleeve, and the slipping plane of this sliding sleeve and the inside surface of stop sleeve be slidably matched; Target seat has slipping plane one end to be arranged in sliding sleeve, and the slipping plane of this target seat and the inside surface of sliding sleeve are slidably matched; Inner spring is arranged in sliding sleeve endoporus, and coordinates with the end face of target seat slipping plane end; Trimming bolt is arranged on the other end of sliding sleeve endoporus; Outer spring is sleeved on the outer round surface of sliding sleeve one end; Target is with allowing the metal of inductor work make, and the sensitive surface of described target is positioned at target seat one end, and the sensitive surface of this target coordinates with the end face of target seat; The straight-bar of described target minor diameter is fixed in target seat.
2. a kind of hatch door sensor installation seat as claimed in claim 1, is characterized in that, the internal diameter of sliding sleeve is identical with the external diameter of end plate that forms slipping plane on target seat; There is end plate sliding sleeve one end, and the external diameter of this end plate is greater than the external diameter of sliding sleeve, and identical with the internal diameter of stop sleeve; The slipping plane that the circumferential surface of described sliding sleeve one end end plate is sliding sleeve; There is the mounting hole of target seat at the center of described sliding sleeve one end end plate, and the aperture of this mounting hole is identical with the external diameter of target seat, after target seat is arranged on the end plate of sliding sleeve, between described sliding sleeve and described target seat for being slidably matched.
3. a kind of hatch door sensor installation seat as claimed in claim 1, is characterized in that, the circumferential surface of target seat one end has the boss radially protruding, and the circumferential surface of this boss has formed the slipping plane of target seat; The inside surface of the described target seat other end has the internal thread being connected with target; The internal diameter of described target seat is identical with the external diameter of target.
4. a kind of hatch door sensor installation seat as claimed in claim 2, is characterized in that, there is end plate stop sleeve one end, and there is the mounting hole of sliding sleeve at the center of this end plate; The aperture of described sliding sleeve mounting hole is identical with the external diameter of sliding sleeve, and the aperture of described stop sleeve is identical with the external diameter of sliding sleeve end plate, makes to be slidably matched between described sliding sleeve and stop sleeve.
CN201210454929.2A 2012-11-13 2012-11-13 Cabin door sensor mounting seat Active CN102914322B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210454929.2A CN102914322B (en) 2012-11-13 2012-11-13 Cabin door sensor mounting seat

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210454929.2A CN102914322B (en) 2012-11-13 2012-11-13 Cabin door sensor mounting seat

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CN102914322A CN102914322A (en) 2013-02-06
CN102914322B true CN102914322B (en) 2014-12-10

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Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109733626B (en) * 2018-11-12 2023-06-30 中航通飞华南飞机工业有限公司 Amphibious aircraft cabin door alarm and indication system
CN114536293B (en) * 2020-11-24 2023-06-30 云南电网有限责任公司昆明供电局 Automatic target positioning robot for measuring parallelism

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4552326A (en) * 1983-07-08 1985-11-12 Societe Nationale Industrielle Et Aerospatiale Safety device for opening an outwardly opening aircraft door in the event of excess pressure inside this aircraft and door equipped therewith
CN2233364Y (en) * 1994-12-22 1996-08-21 朱进先 Magnetic-control switch for hatch of warship
CN1975083A (en) * 2005-11-28 2007-06-06 皮尔茨公司 Safety switch of a movable security door
CN201951214U (en) * 2010-06-09 2011-08-31 力帆实业(集团)股份有限公司 Vehicle door stop device
CN102227536A (en) * 2008-12-10 2011-10-26 迪尔航空航天有限公司 Electromechanical blocking device, particularly for door of airplane

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4552326A (en) * 1983-07-08 1985-11-12 Societe Nationale Industrielle Et Aerospatiale Safety device for opening an outwardly opening aircraft door in the event of excess pressure inside this aircraft and door equipped therewith
CN2233364Y (en) * 1994-12-22 1996-08-21 朱进先 Magnetic-control switch for hatch of warship
CN1975083A (en) * 2005-11-28 2007-06-06 皮尔茨公司 Safety switch of a movable security door
CN102227536A (en) * 2008-12-10 2011-10-26 迪尔航空航天有限公司 Electromechanical blocking device, particularly for door of airplane
CN201951214U (en) * 2010-06-09 2011-08-31 力帆实业(集团)股份有限公司 Vehicle door stop device

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