CN107290602A - A kind of vacant lot state simulation exerciser - Google Patents
A kind of vacant lot state simulation exerciser Download PDFInfo
- Publication number
- CN107290602A CN107290602A CN201610224002.8A CN201610224002A CN107290602A CN 107290602 A CN107290602 A CN 107290602A CN 201610224002 A CN201610224002 A CN 201610224002A CN 107290602 A CN107290602 A CN 107290602A
- Authority
- CN
- China
- Prior art keywords
- vacant lot
- signal
- single knife
- exerciser
- helicopter
- 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
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Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Traffic Control Systems (AREA)
Abstract
The invention belongs to Airplane detection field, it is related to a kind of vacant lot state simulation exerciser, sky/earth signal is provided to go straight up to electrical-mechanical system by vacant lot state simulation exerciser, to go straight up to the pattern that electrical-mechanical system experiment provides sky/ground State Transferring.
Description
Technical field
The invention belongs to Airplane detection field, it is related to a kind of vacant lot state simulation exerciser.
Background technology
Helicopter vacant lot state, be mainly used in judging helicopter in the air or ground state, be to go straight up to electrical-mechanical
The important state of system.It is frequently necessary to carry out the simulation switching of vacant lot state in process of the test, tooling device is more
And disunity, it is unfavorable for operating and safeguards.
The content of the invention
The technical problem to be solved in the present invention：
Sky/earth signal is provided to go straight up to electrical-mechanical system by vacant lot state simulation exerciser, to go straight up to electrical-mechanical
System test provides the pattern of sky/ground State Transferring.
Technical scheme：
A kind of vacant lot state simulation exerciser, including control circuit 1 and matching cable 2, the control circuit 1
By socket J1 A, B, C, D, E end, single knife switch K1, K2, K3, K3, K5, indicator lamp
L1, L2, L3, L4, L5 are composed in parallel, and single knife switch K1, K2, K3, K3, K5 one end are common
Ground connection, the other end connects indicator lamp L1, L2, L3, L4, L5 respectively, and socket J1 is by matching cable 2
It is connected with Helicopter System, during any single knife switch closure, circuit vacant lot signal simulator is provided where it
Signal to helicopter is the state of ground, when any single knife switch disconnects, circuit vacant lot signal mode where it
Intending device is supplied to the signal of helicopter to be airborne status, and described five hilted broadswords of K1, K2, K3, K3, K5 are opened
Air-ground analog signal can be provided for five different systems respectively by closing.
Beneficial effects of the present invention：
The present invention can helicopter simulating vacant lot state, the versatility of exerciser can be realized.
Brief description of the drawings
Fig. 1 is that exerciser controls circuit theory diagrams；
Fig. 2 is matching cable connection；
Fig. 3 is exerciser theory diagram.
Embodiment
This exerciser can control the State Transferring of vacant lot signal by switching, and pass through the light on and off of status indicator lamp
The display of vacant lot state is realized, is controlled while multiple signals can have been realized, when certain road signal is in the state of ground
When, indicator lamp is lighted.Simultaneously by matching the connection of cable, the versatility of exerciser is realized.
7.1 embodiment
This exerciser by：Control circuit 1；Match the two parts of cable 2 composition.Schematic diagram institute as shown in Figure 1, Figure 2
Show, theory diagram is shown in Fig. 3
The control circuit of exerciser by socket J1 A, B, C, D, E end, single knife switch K1, K2,
K3, K3, K5, indicator lamp L1, L2, L3, L4, L5 connection composition.
Cable J2 and J1 is matched to mating connection, J3 is connected with undercarriage electric control system on helicopter.Matching
J3 can do adaptability change with the demand of different model aircraft and versatility can be achieved in cable.
One end common ground of 5 single knife switches, the other end connect respectively 5 indicator lamps be connected, indicator lamp with
Terminal in socket J1 is connected by wire.By taking the loop that K1, L1 and J1 socket A ends are constituted as an example,
When socket J1 is connected by matching cable with undercarriage electric control system on helicopter.K1,L1,J1,J2,J3
When constituting a bulk loop with system on machine, when switch K1 is in open-circuit condition, status indicator lamp L1 is not
Bright, vacant lot signal simulator is supplied to the signal of J3 1 end points to be airborne status.Closed when switch K1 is in
Conjunction state, status indicator lamp L1 brightens, and vacant lot signal simulator is supplied to J3 1 end points to be the state of ground.
The signal principle on remaining 4 tunnel is ibid.
Claims (1)
1. a kind of vacant lot state simulation exerciser, including control circuit (1) and matching cable (2),
Characterized in that, the control circuit (1) is by socket J1 A, B, C, D, E end,
Single knife switch K1, K2, K3, K3, K5, indicator lamp L1, L2, L3, L4, L5 are simultaneously
Joint group is into single knife switch K1, K2, K3, K3, K5 one end common ground, the other end
Indicator lamp L1, L2, L3, L4, L5 are connected respectively, and socket J1 is by matching cable (2)
It is connected with Helicopter System, during any single knife switch closure, circuit vacant lot signal where it
Simulator is supplied to the signal of helicopter to be the state of ground, when any single knife switch disconnects,
Circuit vacant lot signal simulator is supplied to the signal of helicopter to be airborne status where it, described
Five single knife switches of K1, K2, K3, K3, K5 can be provided for five different systems respectively
Air-ground analog signal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610224002.8A CN107290602A (en) | 2016-04-12 | 2016-04-12 | A kind of vacant lot state simulation exerciser |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610224002.8A CN107290602A (en) | 2016-04-12 | 2016-04-12 | A kind of vacant lot state simulation exerciser |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107290602A true CN107290602A (en) | 2017-10-24 |
Family
ID=60095631
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610224002.8A Pending CN107290602A (en) | 2016-04-12 | 2016-04-12 | A kind of vacant lot state simulation exerciser |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107290602A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111332477A (en) * | 2020-02-21 | 2020-06-26 | 中国电子科技集团公司第二十九研究所 | Reverse boosting turbine bypass control device and method |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2676257Y (en) * | 2004-01-09 | 2005-02-02 | 朱路 | Multiway control device for power supply |
| CN200959183Y (en) * | 2006-03-30 | 2007-10-10 | 中国人民解放军66440部队 | Testing and exercising analog system for ground missile priming system |
| US20110050244A1 (en) * | 2007-11-29 | 2011-03-03 | Airbus Operations Gmbh | Method and apparatus for testing aircraft electrical systems |
| CN202711061U (en) * | 2012-08-03 | 2013-01-30 | 中铁八局集团电务工程有限公司 | Simulation rail control test apparatus |
| CN103823459A (en) * | 2012-11-16 | 2014-05-28 | 哈尔滨飞机工业集团有限责任公司 | Engine control box tester |
| CN104345228A (en) * | 2013-08-05 | 2015-02-11 | 哈尔滨飞机工业集团有限责任公司 | Distribution box tester |
| CN105091673A (en) * | 2014-05-07 | 2015-11-25 | 哈尔滨飞机工业集团有限责任公司 | Flutter flight test small rocket switch control plate |
-
2016
- 2016-04-12 CN CN201610224002.8A patent/CN107290602A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2676257Y (en) * | 2004-01-09 | 2005-02-02 | 朱路 | Multiway control device for power supply |
| CN200959183Y (en) * | 2006-03-30 | 2007-10-10 | 中国人民解放军66440部队 | Testing and exercising analog system for ground missile priming system |
| US20110050244A1 (en) * | 2007-11-29 | 2011-03-03 | Airbus Operations Gmbh | Method and apparatus for testing aircraft electrical systems |
| CN202711061U (en) * | 2012-08-03 | 2013-01-30 | 中铁八局集团电务工程有限公司 | Simulation rail control test apparatus |
| CN103823459A (en) * | 2012-11-16 | 2014-05-28 | 哈尔滨飞机工业集团有限责任公司 | Engine control box tester |
| CN104345228A (en) * | 2013-08-05 | 2015-02-11 | 哈尔滨飞机工业集团有限责任公司 | Distribution box tester |
| CN105091673A (en) * | 2014-05-07 | 2015-11-25 | 哈尔滨飞机工业集团有限责任公司 | Flutter flight test small rocket switch control plate |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111332477A (en) * | 2020-02-21 | 2020-06-26 | 中国电子科技集团公司第二十九研究所 | Reverse boosting turbine bypass control device and method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20171024 |