CN207300277U - A kind of static pressure of observable connection reliability/total head one air speed pipe clamp - Google Patents

A kind of static pressure of observable connection reliability/total head one air speed pipe clamp Download PDF

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Publication number
CN207300277U
CN207300277U CN201721164088.6U CN201721164088U CN207300277U CN 207300277 U CN207300277 U CN 207300277U CN 201721164088 U CN201721164088 U CN 201721164088U CN 207300277 U CN207300277 U CN 207300277U
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China
Prior art keywords
static pressure
pressure hole
total head
air speed
pipe clamp
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Application number
CN201721164088.6U
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Chinese (zh)
Inventor
李永强
鞠新星
朱倩倩
童琴
周恩华
刘毅
徐志龙
刘永安
张成标
喻芳
袁欢欢
罗海鹰
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Jiangxi Hongdu Aviation Industry Group Co Ltd
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Jiangxi Hongdu Aviation Industry Group Co Ltd
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Priority to CN201721164088.6U priority Critical patent/CN207300277U/en
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Abstract

A kind of design of air speed pipe clamp is the utility model is related to, discloses a kind of static pressure of observable connection reliability/total head one air speed pipe clamp, which is effectively integrated by static pressure/total head air speed pipe clamp, and ensure that static pressure and the isolation test of total head;Whether in place using the bucket wall of glass steel material, fixture installation can be directly observed when mounted.

Description

A kind of static pressure of observable connection reliability/total head one air speed pipe clamp
Technical field
The present invention relates to a kind of design of air speed pipe clamp, more particularly to a kind of static pressure of observable connection reliability/complete The integral air speed pipe clamp of pressure.
Background technology
Atmosphere data acquisition device of the pitot as machine/missile-borne air data system, is widely used in various aviations and flies On row device.The static pressure that aircraft is measured according to pitot can calculate the flying height of aircraft itself, and be surveyed according to pitot The total head obtained can calculate the flying speed of aircraft.Before ground test is carried out to air data system, by pressure altitude mould Intend the static pressure hole of device and full pressure hole is respectively connected to the static pressure hole and full pressure hole of air speed pipe clamp by gas circuit pipe, then by pitot Fixture is reliably connected to pitot.During test, pressure altitude simulator simulating atmospheric environment exports corresponding static pressure and complete Pressure value, is conducted to pitot by gas circuit pipe and air speed pipe clamp, forms the excitation to air data system, to realize to big The performance verification of gas data system.
Existing air speed pipe clamp generally uses two sections of metal material fixtures, wherein one section is used for the test to static pressure, it is another Section is used for the test to total head.Not only quality is heavy for such a fixture, it is cumbersome to connect, but also easily occurs sealing ring in connection procedure and block up The firmly situation of pitot static pressure hole, causes the test crash of manual operation reason.
The content of the invention
The object of the invention:According to the pitot features of shape of certain model, a kind of the quiet of observable connection reliability has been invented Pressure/total head one air speed pipe clamp.
Technical solution of the present invention:A kind of static pressure of observable connection reliability/total head one air speed pipe clamp, its feature exist In main body respectively has a pressure hole into tubbiness, front end and side, and wherein side pressure hole is static pressure hole 2, and front end pressure hole is complete Hole 1 is pressed, isolation elastic tape 3 is installed between static pressure hole 2 and full pressure hole 1, and closing rubber ring 4 is installed in body rear port Side, dead ring 5 are installed on the outside of body rear port.
The jig main body uses glass steel material.
The isolation elastic tape 3, closing rubber ring 4 are close to the outer wall of tested pitot 6, form total head room 9 and quiet 10 two independent confined spaces of pressure chamber.
Tested pitot full pressure hole 7 and tested pitot static pressure hole 8 on the tested pitot 6 is only positioned at two respectively Vertical is closed interior.
The side pressure hole is static pressure hole 2, front end pressure hole for full pressure hole 1 respectively with the pressure altitude in test equipment The static pressure output of simulator is connected with total head efferent duct.
Advantageous effect of the invention
Static pressure/total head air speed pipe clamp is effectively integrated by the invention, and ensure that the isolation of static pressure and total head is surveyed Examination;Whether in place using the bucket wall of glass steel material, fixture installation can be directly observed when mounted.
Brief description of the drawings
Fig. 1 schematic structural views of the invention
Wherein:1- full pressure holes, 2- static pressure holes, 3- isolation elastic tape, 4- closings elastic tape, 5- dead rings
Fig. 2 measured piece mounted configuration schematic diagrames
Wherein:6- is tested pitot, 7- is tested pitot full pressure hole, 8- is tested pitot static pressure hole, 9- total heads room, 10- Plenum chamber
Embodiment
The present invention will be further described below in conjunction with the accompanying drawings:
As shown in Figure 1, this fixture, main body respectively has a pressure hole into tubbiness, front end and side, and wherein side pressure hole is Static pressure hole, top pressure hole are full pressure hole, are respectively used to static pressure output and the total head efferent duct of connection pressure altitude simulator.Every It is installed on from elastic tape 3 between static pressure delivery outlet and total head delivery outlet, closes rubber ring 4 and be installed on the inside of body rear port, For the aeroseal with air speed tube wall.Dead ring 5 is installed on the outside of body rear port, for by air speed pipe clamp and air speed Pipe is reliably connected.
As shown in Fig. 2, after air speed pipe clamp is installed to tested pitot, its structure is as shown in Figure 2.Rolling clamp is tight Gu clamp can be installed on tested pitot by ring 5, isolation elastic tape 3, closing rubber ring 4 are close to tested pitot 6 Outer wall on, form total head room 9 and 10 two independent confined spaces of plenum chamber, and the tested pitot on tested pitot 6 Full pressure hole 7 and tested pitot static pressure hole 8 respectively positioned at two it is independent it is closed in, therefore can accomplish not do mutually between the two Disturb.
Whether in place in addition, this fixture uses the bucket wall of glass steel material, fixture installation can be directly observed when mounted, no As for the situation for elastic tape occur and blocking tested pitot static pressure hole.
According to tested pitot features of shape, position and the size of rational fixture length and two elastic tapes are calculated, It can make to form two independent confined spaces between pitot and fixture after installation, to realize air speed pipe clamp static pressure/total head Integrated design.

Claims (5)

1. a kind of static pressure of observable connection reliability/total head one air speed pipe clamp, it is characterised in that main body is preceding into tubbiness Respectively there are a pressure hole in end and side, and wherein side pressure hole is static pressure hole (2), and front end pressure hole is full pressure hole (1), isolate rubber Apron (3) is installed between static pressure hole (2) and full pressure hole (1), and closing rubber ring (4) is installed on the inside of body rear port, tightly Gu ring (5) is installed on the outside of body rear port.
2. the static pressure of observable connection reliability as claimed in claim 1/total head one air speed pipe clamp, it is characterised in that The jig main body uses glass steel material.
3. the static pressure of observable connection reliability as claimed in claim 1 or 2/total head one air speed pipe clamp, its feature exist In, it is described isolation elastic tape (3), closing rubber ring (4) be close to the outer wall of tested pitot (6), formed total head room (9) and (10) two independent confined spaces of plenum chamber.
4. the static pressure of observable connection reliability as claimed in claim 3/total head one air speed pipe clamp, it is characterised in that Tested pitot full pressure hole (7) and tested pitot static pressure hole (8) on the tested pitot (6) are located at two independences respectively It is closed in.
5. the static pressure of observable connection reliability as claimed in claim 4/total head one air speed pipe clamp, it is characterised in that The side pressure hole is static pressure hole (2), and front end pressure hole is simulated with the pressure altitude in test equipment respectively for full pressure hole (1) The static pressure output of device is connected with total head efferent duct.
CN201721164088.6U 2017-09-12 2017-09-12 A kind of static pressure of observable connection reliability/total head one air speed pipe clamp Active CN207300277U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721164088.6U CN207300277U (en) 2017-09-12 2017-09-12 A kind of static pressure of observable connection reliability/total head one air speed pipe clamp

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721164088.6U CN207300277U (en) 2017-09-12 2017-09-12 A kind of static pressure of observable connection reliability/total head one air speed pipe clamp

Publications (1)

Publication Number Publication Date
CN207300277U true CN207300277U (en) 2018-05-01

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721164088.6U Active CN207300277U (en) 2017-09-12 2017-09-12 A kind of static pressure of observable connection reliability/total head one air speed pipe clamp

Country Status (1)

Country Link
CN (1) CN207300277U (en)

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