CN206939107U - Starting device for aircraft - Google Patents
Starting device for aircraft Download PDFInfo
- Publication number
- CN206939107U CN206939107U CN201720477985.6U CN201720477985U CN206939107U CN 206939107 U CN206939107 U CN 206939107U CN 201720477985 U CN201720477985 U CN 201720477985U CN 206939107 U CN206939107 U CN 206939107U
- Authority
- CN
- China
- Prior art keywords
- aircraft
- support
- guide rail
- starting device
- footstock
- 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.)
- Expired - Fee Related
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Abstract
The utility model provides a kind of starting device for aircraft, and it includes：Stand (4), there is the first side and the second side；Thermomechanical components are started, are arranged at the first side, starting thermomechanical components includes first support (3) and the starter (1) being fixed in first support (3)；And connection component, it is arranged at the second side, connection component includes second support (8) and the guideway being arranged in second support (8), wherein, guideway includes the first guide rail (7) being fixed in second support (8) and the second guide rail (6) that can be slidably connected or separate with the first guide rail (7), the second guide rail (6) are connected to aircraft.The purpose of this utility model is to provide a kind of starting device for aircraft, and the starting device can separate starter from aircraft, so as to mitigate the overall weight of aircraft, reduces the consumption of airborne power supply, improves endurance.
Description
Technical field
Aircraft field is the utility model is related to, in particular it relates to the starting device for aircraft.
Background technology
General aircraft starter is respectively mounted on board the aircraft, and no longer needs starter to continue work after engine start
Make, in-flight empty gain in weight；Installation then needs to use airborne power supply as annex on board the aircraft, influences endurance.
Utility model content
For problem present in correlation technique, the purpose of this utility model is to provide a kind of starting for aircraft
Device, the starting device can separate starter from aircraft, so as to mitigate the overall weight of aircraft, reduce machine
The consumption of power supply is carried, improves endurance.
To achieve the above object, on the one hand the utility model provides a kind of starting device for aircraft, and this is used to fly
The starting device of row device includes：Stand, there is the first side and the second side；Thermomechanical components are started, are arranged at the first side, start thermomechanical components
Including first support and the starter being fixed in first support；And connection component, the second side is arranged at, connection component includes
The guideway of second support and setting on the secondary support bracket, wherein, guideway includes fixed the first guide rail on the secondary support bracket
And the second guide rail that can be slidably connected or separate with the first guide rail, the second guide rail are connected to aircraft.
According to one embodiment of the present utility model, the first guide rail includes footstock, base and between footstock and base
Intermediate rib, base is connected in second support；Second guide rail includes bending frame, and bending frame is set on footstock and can be with
Footstock is slidably connected or separated.
According to one embodiment of the present utility model, the second guide rail includes footstock, base and between footstock and base
Intermediate rib, base is connected in aircraft；First guide rail includes bending frame, and bending frame is set on footstock and can be with top
Seat is slidably connected or separated.
According to one embodiment of the present utility model, mounting seat is provided with first support, starter passes through mounting seat
It is fixed in first support.
According to one embodiment of the present utility model, the quantity that mounting seat is set is two, and two mounting seats are set respectively
In the opposite sides of first support, and two mounting seats emit the installing space of the top surface formation starter for first support.
According to one embodiment of the present utility model, mounting seat is bolted in first support, and starter
It is installed to by bolt in mounting seat.
According to one embodiment of the present utility model, stand is rectangular frame, and the first side and the second side are rectangular frame
Adjacent both sides or relative both sides.
According to one embodiment of the present utility model, the bottom of stand is provided with road wheel.
According to one embodiment of the present utility model, first support, second support can be bolted, be welded and fixed
It is integrally formed to stand, or with stand.
According to one embodiment of the present utility model, it is provided with gear on starter, gear can start with aircraft
Startup gear ring engagement on machine is connected to start aircraft.
Advantageous effects of the present utility model are：
Starting device of the present utility model for aircraft can separate starter from aircraft, so as to subtract
The overall weight of Airplane Lighter Than Air, the consumption of airborne power supply is reduced, improve endurance；In addition, of the present utility model be used to fly
The starting device of device realizes the quick connection of starting device and aircraft with tearing open by using the guideway slidably separated
Unload.
Brief description of the drawings
, below will be to embodiment in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art
In the required accompanying drawing used be briefly described, it should be apparent that, drawings in the following description are only of the present utility model
Some embodiments, for those of ordinary skill in the art, on the premise of not paying creative work, can also be according to this
A little accompanying drawings obtain other accompanying drawings.
Fig. 1 is the structural representation according to the starting device for aircraft of an exemplary embodiment of the present utility model
Figure；
Fig. 2 in detail exemplified with the starting device for aircraft shown in Fig. 1 stand concrete structure；
Fig. 3 in detail exemplified with the starting device for aircraft shown in Fig. 1 first support concrete structure；
Fig. 4 in detail exemplified with the starting device for aircraft shown in Fig. 1 second support concrete structure；
Fig. 5 in detail exemplified with the starting device for aircraft shown in Fig. 1 starter concrete structure；
Fig. 6 in detail exemplified with the starting device for aircraft shown in Fig. 1 mounting seat concrete structure；
Fig. 7 in detail exemplified with the starting device for aircraft shown in Fig. 1 the first guide rail concrete structure；
Fig. 8 in detail exemplified with the starting device for aircraft shown in Fig. 1 the second guide rail concrete structure；And
Fig. 9 in detail exemplified with the starting device for aircraft shown in Fig. 1 road wheel concrete structure.
Embodiment
Below with reference to accompanying drawing, embodiment of the present utility model is described in detail.It should be appreciated that referring to the drawings
The description carried out to the utility model is only illustrative, and nonrestrictive.Phase can be carried out between each different embodiments
Mutually combination, to form the other embodiment not shown in the following description.In addition, the various directional terminologies used in following description
Equally it is only illustrative, and any restrictions is not formed to the utility model.
As shown in Figures 1 to 9, the embodiment of the utility model one side provides a kind of starting for aircraft and filled
Put.The starting device includes stand 4, starts thermomechanical components and connection component.Wherein, stand 4 has the first side and the second side, and
And the first side that thermomechanical components are arranged on stand 4 is started, connection component is arranged on the second side of stand 4.Specifically, thermomechanical components are started
Including first support 3 and the starter 1 being fixed in first support 3.Connection component includes second support 8 and is arranged on second
Guideway on frame 8, wherein, guideway further comprises the first guide rail 7 and the second guide rail 6, and the first guide rail 7 is fixed on second
On frame 8, the second guide rail 6 is connected and can be slidably connected or separate with the first guide rail 7 with aircraft.
Further, in the above-described embodiments, first support 3, second support 8 can by the machanical fasteners such as bolt,
Welding, bonding etc. are fixed to stand 4, or can be integrally formed with stand 4.
In addition, in the above-described embodiments, may be provided with gear on starter 1, gear can with the engine of aircraft
Startup gear ring engagement, to start aircraft.
When using starting device of the present utility model for aircraft, the second guide rail 6 is fixed on first winged
On row device, and the first guide rail 7 and the second guide rail 6 is set to be slidably connected so that aircraft is fixed on stand 4, then by starter
1 gear engages connection with the startup gear ring on aircraft engine, to realize the start-up operation of aircraft engine；Flying
After the engine start of device, itself and starter 1 are disconnected, the first guide rail 7 is slided with the second guide rail 6 and separates, so as to
Aircraft is separated with starting device, alleviate the overall weight of aircraft, thus reduce the consumption of airborne power supply, improve continuation of the journey
Ability；In addition, the starting device of the present utility model for aircraft is by using the guideway slidably separated, i.e. first
The guide rail 6 of guide rail 7 and second, realize the quick connection and dismounting of starting device and aircraft.
Next, describe with reference to the accompanying drawings according to the specific of the guideway of the starting device of the present utility model for aircraft
Construction.With reference first to Fig. 7, the concrete structure of the first guide rail 7 is shown, the first guide rail 7 is vertical with substantially i shaped cross section
Long guideway, it includes footstock, base and the intermediate rib between footstock and base, wherein, base is used to be connected to second
Frame 8.Referring next to Fig. 8, the concrete structure of the second guide rail 6 is shown, the second guide rail 6 is that the lengthwise with approximate c-shaped cross section is led
Rail, it includes bending frame, wherein, bending frame can be set on the footstock of the first guide rail 7 and can be slidably connected or divide with footstock
From to realize being slidably connected or separating for the first guide rail 7 and the second guide rail 6.
In another possible embodiment of the present utility model, the construction of the first guide rail 7 and the second guide rail 6 can also be mutual
Change, the second guide rail 6 can include footstock, base and the intermediate rib between footstock and base, base and be connected in flight
Device；First guide rail 7 includes bending frame, and bending frame is set on footstock and can be slidably connected or separate with footstock.I.e. second leads
Rail 6 is configured with the longitudinal rail of substantially i shaped cross section, and the first guide rail 7 is configured with the lengthwise of approximate c-shaped cross section
Guide rail, such two kinds of interchangeable guide rail forms are simple in construction, easily fabricated.First guide rail 7, the second guide rail 6 need to be resisted
Mill processing, to extend its service life.
It should be noted that in above-mentioned each embodiment, the first guide rail 7 and the second guide rail 6 can also be configured to reality
The other any form of cooperation guideways for being now slidably connected or separating, this can be depending on practical application, and the utility model is not
It is confined to this.
According to one embodiment of the present utility model, reference picture 1 and Fig. 6, mounting seat 2 is provided with first support 3, risen
Motivation 1 is fixed in first support 3 by mounting seat 2.In a possible embodiment of the present utility model, in first support
Two mounting seats 2 are provided with 3, and the two mounting seats 2 are oppositely arranged and emit the top surface for first support 3, with two
Installing space is formed between individual mounting seat 2, starter 1 is mountable in the installing space.
In one embodiment of the present utility model, such as best exemplified in Fig. 1 and Fig. 6, it is distributed with each mounting seat 2
8 screwed holes, and the corresponding position on starter 1 and first support 3 is provided with corresponding screwed hole, mounting seat 2
It is bolted in first support 3, and similarly, starter 1 is installed in mounting seat 2 by bolt, so as to realize
Starter 1 is stably mounted to first support 3, ensures not loosen when starting aircraft.Starter 1 can be different disposing way
Installed in first support 3, such as in a manner of the central axis of the gear ring of starter 1 is horizontally oriented or belongs to vertical direction
Put, be applicable to different types of aircraft engine, add the scope of application of starting device.
Certainly, mounting seat 2 can be also fixed in first support 3 by other suitable fastening means (for example, welding), and
And starter 1 can be also installed in mounting seat 2 by other suitable modes, this can be depending on practical application, and this practicality is new
Type does not limit to and this.
As shown in Fig. 2 according to one embodiment of the present utility model, stand 4 is configured to rectangular frame, and the first side and
Adjacent both sides or relative both sides of second side for rectangular frame.In addition, in one embodiment of the present utility model, in stand 4
The also settable road wheel 5 in bottom, to facilitate the movement of stand 4.
In the above-described embodiments, although showing that stand 4 is rectangular frame, in other possible embodiments, stand 4
Can also have other suitable constructions, for example, triangular framing, polygonal frame etc., this can be depending on practical application, this reality
This is not limited to new.
It is further noted that the starter in each embodiment described above is not limited to aircraft engine
Starter；In addition, the starting device of the present utility model for aircraft can be used as the frock that starter is temporarily deposited.
Preferred embodiment of the present utility model is the foregoing is only, is not limited to the utility model, for this
For the technical staff in field, the utility model can have various modifications and variations.It is all in the spirit and principles of the utility model
Within, any modification, equivalent substitution and improvements made etc., it should be included within the scope of protection of the utility model.
Claims (10)
- A kind of 1. starting device for aircraft, it is characterised in that including：Stand (4), there is the first side and the second side；Thermomechanical components are started, are arranged at first side, the starting thermomechanical components include first support (3) and are fixed on described first Starter (1) on support (3)；AndConnection component, is arranged at second side, and the connection component includes second support (8) and is arranged on the second support (8) guideway on, wherein, the guideway includes being fixed on the first guide rail (7) in the second support (8) and can be with The second guide rail (6) that first guide rail (7) is slidably connected or separated, second guide rail (6) are connected to the aircraft.
- 2. the starting device according to claim 1 for aircraft, it is characterised in that first guide rail (7) includes Footstock, base and the intermediate rib between the footstock and the base, the base are connected in the second support (8)；Second guide rail (6) includes bending frame, and the bending frame is set on the footstock and can slided with the footstock Connection or separation.
- 3. the starting device according to claim 2 for aircraft, it is characterised in that second guide rail (6) includes Footstock, base and the intermediate rib between the footstock and the base, the base are connected in the aircraft；Institute State the first guide rail (7) include bending frame, it is described bending frame be set on the footstock and can be slidably connected with the footstock or Separation.
- 4. the starting device according to claim 1 for aircraft, it is characterised in that in the first support (3) Mounting seat (2) is provided with, the starter (1) is fixed in the first support (3) by the mounting seat (2).
- 5. the starting device according to claim 4 for aircraft, it is characterised in that what the mounting seat (2) was set Quantity is two, and two mounting seats (2) are separately positioned on the opposite sides of the first support (3), and described in two The top surface that mounting seat (2) is emitted for the first support (3) forms the installing space of the starter (1).
- 6. the starting device according to claim 5 for aircraft, it is characterised in that the mounting seat (2) passes through spiral shell Bolt is fixed in the first support (3), and the starter (1) is installed in the mounting seat (2) by bolt.
- 7. the starting device according to claim 1 for aircraft, it is characterised in that the stand (4) is rectangle frame The adjacent both sides or relative both sides of frame, first side and second side for the rectangular frame.
- 8. the starting device according to claim 1 for aircraft, it is characterised in that in the bottom of the stand (4) It is provided with road wheel (5).
- 9. the starting device according to claim 1 for aircraft, it is characterised in that the first support (3), described Second support (8) can be bolted, be welded and fixed to the stand (4), or is integrally formed with the stand (4).
- 10. the starting device according to claim 1 for aircraft, it is characterised in that set on the starter (1) Gear is equipped with, the gear can engage connection to start the aircraft with the startup gear ring on the engine of the aircraft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720477985.6U CN206939107U (en) | 2017-05-03 | 2017-05-03 | Starting device for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720477985.6U CN206939107U (en) | 2017-05-03 | 2017-05-03 | Starting device for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206939107U true CN206939107U (en) | 2018-01-30 |
Family
ID=61359979
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720477985.6U Expired - Fee Related CN206939107U (en) | 2017-05-03 | 2017-05-03 | Starting device for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206939107U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108791945A (en) * | 2017-05-03 | 2018-11-13 | 深圳光启合众科技有限公司 | Starting device for aircraft |
-
2017
- 2017-05-03 CN CN201720477985.6U patent/CN206939107U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108791945A (en) * | 2017-05-03 | 2018-11-13 | 深圳光启合众科技有限公司 | Starting device for aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180130 Termination date: 20210503 |