A aviation & planes forum. AviationBanter

If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below.

Go Back   Home » AviationBanter forum » rec.aviation newsgroups » Instrument Flight Rules
Site Map Home Register Authors List Search Today's Posts Mark Forums Read Web Partners

Fine example of Tarver Engineering release for service



 
 
Thread Tools Display Modes
  #1  
Old February 27th 04, 03:25 AM
Tarver Engineering
external usenet poster
 
Posts: n/a
Default


"Phil Miller" wrote in message
...

Robert is being rediculess to claim that a pitot tube produces some total
pressure and then the static port pressure is subtracted twice to make IAS.
The whole point of using a static port is to be able to take the guts out of
a pitot tube and produce only pitot pressure, thus increasing the
reliability of the system.

Perhaps this will help:

"Tarver Engineering" wrote:


"Gord Beaman" wrote in message
.. .
"Jim Knoyle" wrote:


Hang on here a second now Jim, you still need two samples. As Dan
says you need 'static pressure' to read the altitude from and you
need 'pitot pressure' (ram air pressure) as well as the static
pressure to derive the airspeed reading from. Sounds like you're
saying that you can read 'both' from just the 'ram air pressure'
alone. Or did I misunderstand you?


Jim has finally figued out what a pitot tube is, but somehow he still wants
to be correct in his archive troll. It is a great paradox.


I know...ain't life a bitch John

--

-Gord.


  #2  
Old February 27th 04, 03:33 AM
Phil Miller
external usenet poster
 
Posts: n/a
Default

On Thu, 26 Feb 2004 19:25:26 -0800, "Tarver Engineering"
wrote:


"Phil Miller" wrote in message
.. .

Robert is being rediculess to claim that a pitot tube produces some total
pressure and then the static port pressure is subtracted twice to make IAS.
The whole point of using a static port is to be able to take the guts out of
a pitot tube and produce only pitot pressure, thus increasing the
reliability of the system.

Perhaps this will help:


Yes that does help, because what Robert said and what Gord said are
practically identical.

"Gord Beaman" wrote in message
. ..
Hang on here a second now Jim, you still need two samples. As Dan
says you need 'static pressure' to read the altitude from and you
need 'pitot pressure' (ram air pressure) as well as the static
pressure to derive the airspeed reading from.


On Thu, 26 Feb 2004 21:06:41 GMT, Robert Moore
wrote:

The Pitot Pressure from the Pitot Tube is a combination of Static
and RAM pressure. The bellows inside the airspeed indicator
uses the ambient static pressure from the static port to cancel
out the static component from the Pitot Tube leaving only the RAM
component to move the airspeed needle.



Phil
--
Great Tarverisms #2

What is the best selling beer in Oz?

Budweiser.

Another illusion shattered.

John

alt.disasters.aviation
18 August 2002
  #3  
Old February 27th 04, 03:39 AM
Phil Miller
external usenet poster
 
Posts: n/a
Default

On Fri, 27 Feb 2004 14:33:43 +1100, Phil Miller
wrote:

On Thu, 26 Feb 2004 19:25:26 -0800, "Tarver Engineering"
wrote:


"Phil Miller" wrote in message
. ..

Robert is being rediculess to claim that a pitot tube produces some total
pressure and then the static port pressure is subtracted twice to make IAS.
The whole point of using a static port is to be able to take the guts out of
a pitot tube and produce only pitot pressure, thus increasing the
reliability of the system.

Perhaps this will help:


Yes that does help, because what Robert said and what Gord said are
practically identical.


Oh! And you didn't enlighten me about the Bombardier GBX?


Phil
--
Great Tarverisms #1

The Air Speed Indicator (ASI) shows


You made that up, didn't you?

The IAS indicator says IAS, not ASI.

Why do you come here pretending to know something
when you don't even know the words?

John
 




Thread Tools
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump


All times are GMT +1. The time now is 05:44 AM.


Powered by vBulletin® Version 3.6.4
Copyright ©2000 - 2025, Jelsoft Enterprises Ltd.
Copyright ©2004-2025 AviationBanter.
The comments are property of their posters.