CN207045762U - A kind of aircraft engine nacelle fire perceiving device erecting device - Google Patents
A kind of aircraft engine nacelle fire perceiving device erecting device Download PDFInfo
- Publication number
- CN207045762U CN207045762U CN201720326314.XU CN201720326314U CN207045762U CN 207045762 U CN207045762 U CN 207045762U CN 201720326314 U CN201720326314 U CN 201720326314U CN 207045762 U CN207045762 U CN 207045762U
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- fire perceiving
- installing plate
- aircraft engine
- engine nacelle
- fire
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Abstract
Aircraft engine nacelle structure-design technique is the utility model is related to, more particularly to a kind of aircraft engine nacelle fire perceiving device erecting device.Fire perceiving device erecting device is used for the motor mounts that fire perceiving device is arranged on to tubulose, specifically includes：Installing plate；First clip, for lock ring fire perceiving device, and it is removably secured and is arranged on the installing plate one side；Second clip, for motor mounts described in lock ring, and it is removably secured and is arranged on described installing plate one end end face.Aircraft engine nacelle fire perceiving device erecting device of the present utility model, fire perceiving device and installing plate are fixed by the first clip, the installing plate with fire perceiving device is lifted on the motor mounts being fixed in enging cabin by the second clip again so that dismounting is more convenient.
Description
Technical field
Aircraft engine nacelle structure-design technique is the utility model is related to, more particularly to a kind of aircraft engine nacelle fire alarm passes
Sensor erecting device.
Background technology
Fire perceiving device is usually provided with aircraft engine nacelle, is overheated for detecting in enging cabin and is caught fire and send
Alarm signal, the generation for preventing fire from expanding, improve security.Fire perceiving device mainly be arranged on engine nacelle flame range it
It is interior, still, the nacelle flame range narrow space, and internal each system attachment is more, is not easy to dismount using traditional erecting device
And safeguard.
The content of the invention
The purpose of this utility model there is provided a kind of aircraft engine nacelle fire perceiving device erecting device, existing to solve
At least one problem existing for fire perceiving device erecting device.
The technical solution of the utility model is：
A kind of aircraft engine nacelle fire perceiving device erecting device, for fire perceiving device to be arranged on to the engine of tubulose
On mounting bracket, the aircraft engine nacelle fire perceiving device erecting device includes：
Installing plate；
First clip, match with the outer contour shape of the fire perceiving device, for fire perceiving device described in lock ring, and
It is removably secured and is arranged on the installing plate one side；
Second clip, match with the outer contour shape of the motor mounts, installed for engine described in lock ring
Frame, and be removably secured and be arranged on described installing plate one end end face.
Preferably, each fire perceiving device carries out lock ring, and two described first by two first clips
Axis direction of the clip along the fire perceiving device is set up in parallel.
Preferably, the openend of first clip is bolted on the installing plate one side.
Preferably, the fire perceiving device is two, is disposed in parallel in the installing plate one side；
The opening for adjacent two first clip being separately positioned on the fire perceiving device is relative, and by same
One is bolted to the installing plate one side.
Preferably, the motor mounts are consolidated by two second clips and described installing plate one end end face
It is fixed.
The utility model has the advantage of：
Aircraft engine nacelle fire perceiving device erecting device of the present utility model, by the first clip by fire perceiving device with
Installing plate is fixed, then the installing plate with fire perceiving device is lifted into the hair being fixed in enging cabin by the second clip
On motivation mounting bracket so that dismounting is more convenient.
Brief description of the drawings
Fig. 1 is the structural representation of the utility model aircraft engine nacelle fire perceiving device erecting device；
Fig. 2 is the side view of the utility model aircraft engine nacelle fire perceiving device erecting device.
Embodiment
To make the purpose, technical scheme and advantage that the utility model is implemented clearer, below in conjunction with the utility model
Accompanying drawing in embodiment, the technical scheme in the embodiment of the utility model is further described in more detail.In the accompanying drawings, from beginning
Same or similar element is represented to same or similar label eventually or there is the element of same or like function.Described reality
It is the utility model part of the embodiment to apply example, rather than whole embodiments.Below with reference to the embodiment of accompanying drawing description
It is exemplary, it is intended to for explaining the utility model, and it is not intended that to limitation of the present utility model.It is new based on this practicality
Embodiment in type, the every other implementation that those of ordinary skill in the art are obtained under the premise of creative work is not made
Example, belong to the scope of the utility model protection.Embodiment of the present utility model is described in detail below in conjunction with the accompanying drawings.
In description of the present utility model, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", "front", "rear",
The orientation or position relationship of the instruction such as "left", "right", " vertical ", " level ", " top ", " bottom ", " interior ", " outer " is based on accompanying drawing institutes
The orientation or position relationship shown, it is for only for ease of description the utility model and simplifies description, rather than indicates or imply and be signified
Device or element must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that to this practicality
The limitation of novel protected scope.
1 and Fig. 2 is done further to the utility model aircraft engine nacelle fire perceiving device erecting device below in conjunction with the accompanying drawings
Describe in detail.
The utility model provides a kind of aircraft engine nacelle fire perceiving device erecting device, for by fire perceiving device 1
On the motor mounts 2 of tubulose.Specifically, aircraft engine nacelle fire perceiving device erecting device can include installation
Plate 3 and yoke configurations.
Installing plate 3 can be arranged as required to be in a variety of suitable platy structures, to facilitate installation clip.
Clip can use a variety of suitable yoke configurations being currently known, typically with an openend, by opening
Locking device (such as bolts and nuts form) at mouth end wants locking hoop；In the present embodiment, clip includes the He of the first clip 4
Second clip 5.
The size and the outer contour shape of fire perceiving device 1 of first clip 4 match, for lock ring (in the locked condition)
Fire perceiving device 1, and be removably secured and be arranged on the one side of installing plate 3.
The size and the outer contour shape of motor mounts 2 of second clip 5 match, for lock ring (in locking state
Under) motor mounts 2, and be removably secured and be arranged on one end end face of installing plate 3.In the present embodiment, the side of being detachably fixed
Formula is preferably by the way of bolt 6 and nut coordinate, also, preferably the first clip 4 and the second clip 5 are in openend opening position
The one side of installing plate 3 is fixed on by bolt 6, meanwhile, the fixing bolt 6 also serves as the locking device of clip in itself.
Aircraft engine nacelle fire perceiving device erecting device of the present utility model, by the first clip 4 by fire perceiving device 1
It is fixed with installing plate 3, then is hung the installing plate 3 (overall structure of formation) with fire perceiving device 1 by the second clip 5
Dress is fixed on the motor mounts 2 in enging cabin so that dismounting is more convenient.
In aircraft engine nacelle fire perceiving device erecting device of the present utility model, each fire perceiving device 1 can pass through
At least one first clip 4 carries out lock ring；In the present embodiment, in order that obtaining, stability is stronger, and preferably each fire perceiving device 1 is logical
Cross two the first clips 4 and carry out lock ring, and axis direction of two the first clips 4 along fire perceiving device 1 is set up in parallel.
Further, in the present embodiment, preferably fire perceiving device 1 is two；Two fire perceiving devices 1 are disposed in parallel in installation
The one side of plate 3.Also, the opening for the first clip of adjacent two 4 being separately positioned on fire perceiving device 1 is relative, and passes through
Same bolt 6 is fixed on the one side of installing plate 3, so that more compact structure and stability is stronger.
Equally, motor mounts 2 can be fixed by least one second clip 5 and one end end face of installing plate 3；
In the present embodiment, preferably each fire perceiving device 1 is fixed by two the second clips 5 and one end end face of installing plate 3, two
Second clip 5 is set up in parallel in the axis direction of motor mounts 2.
It is described above, only specific embodiment of the present utility model, but the scope of protection of the utility model is not limited to
In this, any one skilled in the art is in the technical scope that the utility model discloses, the change that can readily occur in
Change or replace, should all cover within the scope of protection of the utility model.Therefore, the scope of protection of the utility model should be with described
Scope of the claims is defined.
Claims (5)
- A kind of 1. aircraft engine nacelle fire perceiving device erecting device, for fire perceiving device (1) to be arranged on into starting for tubulose On machine mounting bracket (2), it is characterised in that the aircraft engine nacelle fire perceiving device erecting device includes：Installing plate (3)；First clip (4), for fire perceiving device described in lock ring (1), and it is removably secured and is arranged on the installing plate (3) one Side；Second clip (5), for motor mounts described in lock ring (2), and it is removably secured and is arranged on the installing plate (3) One end end face.
- 2. aircraft engine nacelle fire perceiving device erecting device according to claim 1, it is characterised in that each fire Alert sensor (1) carries out lock ring by two first clips (4), and two first clips (4) pass along the fire alarm The axis direction of sensor (1) is set up in parallel.
- 3. aircraft engine nacelle fire perceiving device erecting device according to claim 2, it is characterised in that first card The openend of hoop (4) is fixed on the installing plate (3) one side by bolt (6).
- 4. aircraft engine nacelle fire perceiving device erecting device according to claim 3, it is characterised in that the fire alarm passes Sensor (1) is two, is disposed in parallel in the installing plate (3) one side；The opening for adjacent two first clip (4) being separately positioned on the fire perceiving device (1) is relative, and passes through Same bolt (6) is fixed on the installing plate (3) one side.
- 5. the aircraft engine nacelle fire perceiving device erecting device according to claim any one of 1-4, it is characterised in that institute Motor mounts (2) are stated to be fixed with the installing plate (3) one end end face by two second clips (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720326314.XU CN207045762U (en) | 2017-03-30 | 2017-03-30 | A kind of aircraft engine nacelle fire perceiving device erecting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720326314.XU CN207045762U (en) | 2017-03-30 | 2017-03-30 | A kind of aircraft engine nacelle fire perceiving device erecting device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207045762U true CN207045762U (en) | 2018-02-27 |
Family
ID=61489514
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720326314.XU Active CN207045762U (en) | 2017-03-30 | 2017-03-30 | A kind of aircraft engine nacelle fire perceiving device erecting device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207045762U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109360463A (en) * | 2018-12-07 | 2019-02-19 | 北京维盛网域科技有限公司 | A kind of fixed structure, sensor and simulation system |
-
2017
- 2017-03-30 CN CN201720326314.XU patent/CN207045762U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109360463A (en) * | 2018-12-07 | 2019-02-19 | 北京维盛网域科技有限公司 | A kind of fixed structure, sensor and simulation system |
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