CN106697310A - Quick-disassembly structure for aviation displayer - Google Patents
Quick-disassembly structure for aviation displayer Download PDFInfo
- Publication number
- CN106697310A CN106697310A CN201611140634.2A CN201611140634A CN106697310A CN 106697310 A CN106697310 A CN 106697310A CN 201611140634 A CN201611140634 A CN 201611140634A CN 106697310 A CN106697310 A CN 106697310A
- Authority
- CN
- China
- Prior art keywords
- aviation
- bracket
- locking arm
- aviation displays
- quick
- 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.)
- Pending
Links
- 229910000831 Steel Inorganic materials 0.000 claims description 7
- 239000010959 steel Substances 0.000 claims description 7
- 230000006835 compression Effects 0.000 claims description 6
- 238000007906 compression Methods 0.000 claims description 6
- 238000003754 machining Methods 0.000 abstract 1
- 238000010586 diagram Methods 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000002596 correlated effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/04—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mutual Connection Of Rods And Tubes (AREA)
Abstract
The invention belongs to the field of aviation airborne equipment and particularly relates to a quick-disassembly structure for an aviation displayer. The quick-disassembly structure comprises a bracket body and a bracket locking plate, wherein the bracket locking plate is installed on the bracket body. A lower portion positioning pin is arranged in the middle of the bracket locking plate, and locking arms are symmetrically arranged on the two sides of the bracket locking plate. According to the quick-disassembly structure for the aviation displayer, the structure is skillful, an existing aviation displayer do not need to be subjected to any machining; by using an existing positioning hole of the aviation displayer and relying on the bracket locking plate and the locking arms, quick assembly and disassembly over the aviation displayer are achieved; and the finite space of an aircraft instrument panel is sufficiently utilized, the space of a cockpit is not occupied, and flying comfort and manipulation convenience of a pilot are improved.
Description
Technical field
The invention belongs to aviation airborne equipment field, and in particular to a kind of aviation displays quick-release structure.
Background technology
The display of Novel helicopter is required to realize fast assembling-disassembling function.Though also there is quick-release on conventional display product
Structure, but structure it is complex, it is necessary to process over the display it is various complexity boss wedge structures, while requiring quick-release structure
Correlated parts there is precision higher, quick-release construction profile size is also relatively large, takes larger driving cabin space, aircraft
Instrument panel space utilization rate is relatively low, influences the comfortableness of pilot driver.
The content of the invention
Goal of the invention：There is provided it is a kind of can be applied to small space use when conveniently aviation displays unload the goods from the airplane soon
Structure.
Technical scheme：A kind of aviation displays quick-release structure, including bracket body 1 and on bracket body 1
Bracket latch 2, the middle setting of bracket latch 2 has bottom alignment pin 6, and both sides are symmetrically arranged with locking arm 4, and locking arm 4 can
3 rotate around the shaft, aviation displays locating piece is matched for clamping tightly with bracket latch 2 when tightening, the inner side of locking arm 4 is provided with spiral shell
Compression spring 12 is provided with line sleeve 10, screw shell 10, compression spring 12 applies elastic force to steel ball 11, and the one end of shift fork 5 leads to
Rivet 7 is crossed on the bracket body 1, the other end stretches out the preformed hole of locking arm 4, extension spring 8 by two shift forks 5 in left and right to
Centre tenses and clasps locking arm 4 by the pin 13 of locking arm 4.
When aviation displays are installed, the pusher of location hole aligned with lower alignment pin 6 below aviation displays is entered into bracket sheet
Body 1, aviation displays locating piece is blocked by bracket latch 2, and two locking arms 4 are turned to the inside, and steel ball 11 is by display
Locating piece is compressed, and two shift forks 5 block the pin 13 on locking arm 4 in the presence of extension spring 8, and realization shows to aviation
Device is locked.
Two shift forks 5 are allocated to both sides respectively, locking arm 4 is released, realize the dismounting to aviation displays.
Beneficial effect：Clever structure of the present invention, does any processing, using aviation displays without to existing aviation displays
Existing location hole, tightens plate and locking arm is realized being rapidly assembled and disassembled aviation displays, fully profit by bracket
With the confined space of aircraft instrument panel, driving cabin space is not take up, flight comfortableness and the manipulation that improve pilot are convenient
Property.
Brief description of the drawings
Fig. 1 is schematic structural view of the invention.
Fig. 2 is upward view of the present invention.
Fig. 3 is aviation displays schematic diagram.
Fig. 4 is the assembling schematic diagram of locking arm.
Fig. 5 assembly relation schematic diagrames
Fig. 6 assembly relation upward views
Fig. 7 removing relation schematic diagrames.
Specific embodiment
The present invention is described in further detail below in conjunction with the accompanying drawings, refers to Fig. 1 to Fig. 7.
A kind of aviation displays quick-release structure, including bracket body 1 and the locking of the bracket on bracket body 1
Plate 2, the middle setting of bracket latch 2 has bottom alignment pin 6, and both sides are symmetrically arranged with locking arm 4, and locking arm 4 can around the shaft 3 turns
It is dynamic, aviation displays locating piece is matched for clamping tightly with bracket latch 2 when tightening, the inner side of locking arm 4 is provided with screw shell 10,
Compression spring 12 is provided with screw shell 10, compression spring 12 applies elastic force by elastic force to steel ball 11, and the one end of shift fork 5 passes through
Rivet 7 is arranged on bracket body 1, and the other end stretches out the preformed hole of locking arm 4, and extension spring 8 is by two shift forks 5 in left and right in
Between tense locking arm 4 clasped by the pin 13 of locking arm 4.
When aviation displays are installed, the pusher of location hole aligned with lower alignment pin 6 below aviation displays is entered into bracket sheet
Body 1, aviation displays locating piece is blocked by bracket latch 2, and two locking arms 4 are turned to the inside, and steel ball 11 is by display
Locating piece is compressed, and two shift forks 5 block the pin 13 on locking arm 4 in the presence of extension spring 8, and realization shows to aviation
Device is locked.
Two shift forks 5 are allocated to both sides respectively, locking arm 4 is released, realize the dismounting to aviation displays.
Screw thread between locking arm 4 and bracket body 1 by rotating shaft 3 is attached.It is embodied in the middle of middle rotating shaft 3 one
Section boss can be provided with certain altitude so that leave portion gap between locking arm 4 and bracket body 1, facilitate locking arm 4 certainly
By rotating, also allow in the future repairing locking arm 4.
When needing for aviation displays to load onto bracket, only need to be by the location hole aligning bracket body 1 below display
Then aviation displays are pushed bracket body 1, when the locating piece of aviation displays bottom is locked by bracket by bottom alignment pin 6
Plate 2 is blocked, and after aviation displays cannot continue to move ahead, now two locking arms 4 is turned to the inside, and the steel ball 11 on the inside of it will
Display locating piece is compressed, and the pin 13 on locking arm 4 is also blocked, now locked by two shift forks 5 in the presence of extension spring 8
Tight arm 4 fixed and cannot be rotated, it is achieved thereby that aviation displays are locked.
When needing to unload aviation displays from bracket body 1, only two shift forks 5 need to be respectively allocated to two with hand
Side, now locking arm 4 be released, aviation displays can be extracted out from bracket body 1.
Clever structure of the present invention, any processing is done without to existing aviation displays, existing fixed using aviation displays
Position hole, tightens plate and locking arm is realized being rapidly assembled and disassembled aviation displays by bracket, takes full advantage of aircraft
The confined space of instrument board, is not take up driving cabin space, improves the flight comfortableness and manipulation convenience of pilot.
Claims (3)
1. a kind of aviation displays quick-release structure, it is characterised in that including bracket body [1] and installed in bracket body [1]
On bracket latch [2], bracket latch [2] middle setting has bottom alignment pin [6], and both sides are symmetrically arranged with locking arm
[4], locking arm [4] [3] can be rotated around the shaft, and aviation displays locating piece is matched for clamping tightly with bracket latch [2] when tightening, and be locked
It is provided with screw shell [10], screw shell [10] on the inside of tight arm [4] and is provided with compression spring [12], compression spring [12]
Apply elastic force to steel ball [11], by rivet [7] on bracket body [1], the other end stretches out locking arm for shift fork [5] one end
[4] preformed hole, extension spring [8] tenses two shift forks [5] in left and right to centre, the pin that shift fork [5] passes through locking arm [4]
[13] locking arm [4] is clasped.
2. a kind of aviation displays quick-release structure according to claim 1, it is characterised in that when installing aviation displays,
Location hole aligned with lower alignment pin [6] pusher below aviation displays is entered into bracket body [1], aviation displays locating piece quilt
Bracket latch [2] is blocked, and two locking arms [4] are turned to the inside, and steel ball [11] compresses display locating piece, and two are dialled
Fork [5] blocks the pin [13] on locking arm [4] in the presence of extension spring [8], realizes the locking to aviation displays
It is fixed.
3. a kind of aviation displays quick-release structure according to claim 1, it is characterised in that by two shift forks [5] respectively
Both sides are allocated to, locking arm [4] is released, realize the dismounting to aviation displays.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611140634.2A CN106697310A (en) | 2016-12-12 | 2016-12-12 | Quick-disassembly structure for aviation displayer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611140634.2A CN106697310A (en) | 2016-12-12 | 2016-12-12 | Quick-disassembly structure for aviation displayer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106697310A true CN106697310A (en) | 2017-05-24 |
Family
ID=58937096
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611140634.2A Pending CN106697310A (en) | 2016-12-12 | 2016-12-12 | Quick-disassembly structure for aviation displayer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106697310A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109488866A (en) * | 2018-12-05 | 2019-03-19 | 太原航空仪表有限公司 | A kind of bracket for fast assembling-disassembling airborne indicator |
| CN112610832A (en) * | 2020-12-31 | 2021-04-06 | 滨州学院 | Aviation display quick-release structure |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1160499A1 (en) * | 2000-05-22 | 2001-12-05 | Frank Lemieux | Camera-to-tripod quick-release mounting |
| CN101495707A (en) * | 2005-06-07 | 2009-07-29 | Csav股份有限公司 | Self-balancing adjustable mounting system with friction adjustment |
| CN201621435U (en) * | 2010-01-27 | 2010-11-03 | 中航工业雷达与电子设备研究院 | Support capable of tool-free and fast dismounting of display |
| US20130214105A1 (en) * | 2012-02-21 | 2013-08-22 | L-3 Communication Avionics Systems, Inc. | Retention mechanism and method for removeably supporting a portable flight controller |
| CN204178298U (en) * | 2014-06-30 | 2015-02-25 | 中国航空无线电电子研究所 | A kind of Novel chassis bracket latch mechanism |
| CN204785351U (en) * | 2015-06-27 | 2015-11-18 | 泰州市创新电子有限公司 | Quick detach installation constructs for display |
| CN105173099A (en) * | 2015-09-15 | 2015-12-23 | 航宇救生装备有限公司 | Quick disassembly and assembly mechanism of airborne equipment |
-
2016
- 2016-12-12 CN CN201611140634.2A patent/CN106697310A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1160499A1 (en) * | 2000-05-22 | 2001-12-05 | Frank Lemieux | Camera-to-tripod quick-release mounting |
| CN101495707A (en) * | 2005-06-07 | 2009-07-29 | Csav股份有限公司 | Self-balancing adjustable mounting system with friction adjustment |
| CN201621435U (en) * | 2010-01-27 | 2010-11-03 | 中航工业雷达与电子设备研究院 | Support capable of tool-free and fast dismounting of display |
| US20130214105A1 (en) * | 2012-02-21 | 2013-08-22 | L-3 Communication Avionics Systems, Inc. | Retention mechanism and method for removeably supporting a portable flight controller |
| CN204178298U (en) * | 2014-06-30 | 2015-02-25 | 中国航空无线电电子研究所 | A kind of Novel chassis bracket latch mechanism |
| CN204785351U (en) * | 2015-06-27 | 2015-11-18 | 泰州市创新电子有限公司 | Quick detach installation constructs for display |
| CN105173099A (en) * | 2015-09-15 | 2015-12-23 | 航宇救生装备有限公司 | Quick disassembly and assembly mechanism of airborne equipment |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109488866A (en) * | 2018-12-05 | 2019-03-19 | 太原航空仪表有限公司 | A kind of bracket for fast assembling-disassembling airborne indicator |
| CN112610832A (en) * | 2020-12-31 | 2021-04-06 | 滨州学院 | Aviation display quick-release structure |
| WO2022142768A1 (en) * | 2020-12-31 | 2022-07-07 | 滨州学院 | Quick disassembly structure for aviation display |
| GB2610310A (en) * | 2020-12-31 | 2023-03-01 | Univ Binzhou | Quick disassembly structure for aviation display |
| GB2610310B (en) * | 2020-12-31 | 2024-04-10 | Univ Binzhou | Quick disassembly structure for aviation display |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170524 |
|
| RJ01 | Rejection of invention patent application after publication |