banner
banner

27 Nov 2025, 17:00 [ UTC - 5; DST ]


Garmin International (Banner)



Reply to topic  [ 676 posts ]  Go to page Previous  1 ... 27, 28, 29, 30, 31, 32, 33 ... 46  Next
Username Protected Message
 Post subject: Re: Single engine pressurized above FL 250
PostPosted: 22 Jan 2016, 00:28 
Offline


 Profile




Joined: 09/21/13
Posts: 33
Post Likes: +8
Aircraft: Barron 55
Username Protected wrote:
I suspect you have made some unrealistic assumptions about cabin leak rates to arrive at your conclusion.

I used 0.55 lbs of air per minute per person as specified in Part 23.831. This actually only applies to flight above FL410, but figure its a reasonable criteria regardless.

If you know of any published leak rates for aircraft, I would love to see it. I've searched and haven't seen any data on that. However my guess is leakage rates are below ventilation requirements and thus doesn't set the pressurization flows.


Top

 Post subject: Re: Single engine pressurized above FL 250
PostPosted: 22 Jan 2016, 01:12 
Offline



User avatar
 Profile




Joined: 12/10/07
Posts: 8227
Post Likes: +7958
Location: New York, NY
Aircraft: Debonair C33A
Username Protected wrote:
Because above 250, the partial pressure of 100% oxygen is insufficient, and also the risk of decompression sickness goes way up.


Why do they bother putting those masks on airliners then?


Top

 Post subject: Re: Single engine pressurized above FL 250
PostPosted: 22 Jan 2016, 01:15 
Offline



User avatar
 Profile




Joined: 12/10/07
Posts: 8227
Post Likes: +7958
Location: New York, NY
Aircraft: Debonair C33A
Username Protected wrote:
FAA Part 23 Regulations.

§ 23.841 Pressurized cabins.
(a) If certification for operation above 25,000 feet is requested, the airplane must be able to maintain a cabin pressure altitude of not more than 15,000 feet, in the event of any probable failure condition in the pressurization system. During decompression, the cabin altitude may not exceed 15,000 feet for more than 10 seconds and 25,000 feet for any duration.

The FAA has said they consider engine failures as a "probable failure", so that presents a challenge to a single engine airplane.


Right, but those can be waived via "equivalent level of safety" procedure. That's how Cirrus got around spin certification for SR series, for example.


Top

 Post subject: Re: Single engine pressurized above FL 250
PostPosted: 22 Jan 2016, 01:27 
Offline


 WWW  Profile




Joined: 12/03/14
Posts: 20781
Post Likes: +26295
Company: Ciholas, Inc
Location: KEHR
Aircraft: C560V
Username Protected wrote:
I used 0.55 lbs of air per minute per person as specified in Part 23.831.

To put that number in context, the FJ33 is rated to extract 50 lbs/min of bleed air.

That's 13 times the flow you used (3.85 lbs/min).

In many twins (mine included), cabin pressure can't quite be maintained on one engine. My engines are rated for 46 lbs/min each, so my leak rates are above what one of my engines put out.

On a "well sealed" cabin, I would expect leak rates around 15 lbs/min are the best that can be achieved. There are just so many little places where leaks can develop such as around control cables and electrical connectors.

As the airplane ages, this will climb without any indication the leak rate has gone up until it hits the limit of what the engine can put out. Then the owner will search for and repair leaks until it again makes full diff, but it may be close to 100% of the air flow is out leaks and not the outflow valve.

Quote:
However my guess is leakage rates are below ventilation requirements

I believe the tightest cabins are many times the minimum. For certain, the engine bleed air systems put out MANY times the minimum during normal operation. Since that hurts engine performance, one expects they wouldn't do that unless they needed to.

Mike C.

_________________
Email mikec (at) ciholas.com


Top

 Post subject: Re: Single engine pressurized above FL 250
PostPosted: 22 Jan 2016, 01:31 
Online


User avatar
 Profile




Joined: 11/08/12
Posts: 7717
Post Likes: +5103
Location: Live in San Carlos, CA - based Hayward, CA KHWD
Aircraft: Piaggio Avanti
Username Protected wrote:
Why do they bother putting those masks on airliners then?

That's why they have second source of pressurization requirements, to keep from exposing those pax to the full altitude of complete decompression. Pilot masks have to be pressure masks, etc. Having hypoxic or sick passengers is preferrable to having a hypoxic or sick pilot.

_________________
-Jon C.


Top

 Post subject: Re: Single engine pressurized above FL 250
PostPosted: 22 Jan 2016, 01:40 
Offline



User avatar
 Profile




Joined: 12/10/07
Posts: 8227
Post Likes: +7958
Location: New York, NY
Aircraft: Debonair C33A
Username Protected wrote:
That's why they have second source of pressurization requirements, to keep from exposing those pax to the full altitude of complete decompression. Pilot masks have to be pressure masks, etc. Having hypoxic or sick passengers is preferrable to having a hypoxic or sick pilot.


I don't think second source of pressurization will help in explosive decompression scenario.


Top

 Post subject: Re: Single engine pressurized above FL 250
PostPosted: 22 Jan 2016, 01:42 
Offline


 WWW  Profile




Joined: 12/03/14
Posts: 20781
Post Likes: +26295
Company: Ciholas, Inc
Location: KEHR
Aircraft: C560V
Username Protected wrote:
Right, but those can be waived via "equivalent level of safety" procedure. That's how Cirrus got around spin certification for SR series, for example.

You have to show "equivalent" safety.

How do you do something that is equivalent to a second engine pressure source?

Whatever that is represents weight and complexity that would have been better as a second engine. Now you get propulsion redundancy as well.

Mike C.

_________________
Email mikec (at) ciholas.com


Top

 Post subject: Re: Single engine pressurized above FL 250
PostPosted: 22 Jan 2016, 01:44 
Offline


 WWW  Profile




Joined: 12/03/14
Posts: 20781
Post Likes: +26295
Company: Ciholas, Inc
Location: KEHR
Aircraft: C560V
Username Protected wrote:
I don't think second source of pressurization will help in explosive decompression scenario.

That is not classified as a "probable" failure thus no redundancy is required to deal with this scenario.

Mike C.

_________________
Email mikec (at) ciholas.com


Top

 Post subject: Re: Single engine pressurized above FL 250
PostPosted: 22 Jan 2016, 03:06 
Offline


 Profile




Joined: 03/09/13
Posts: 929
Post Likes: +472
Location: Byron Bay,NSW Australia
Aircraft: C525,C25A,C25C,CL604
Username Protected wrote:
Jason, short answer to your question is that a prop is much more efficient at converting power from a jet engine at the altitudes and speeds we are talking about. A turboprop is the ultimate high bypass ratio jet engine.


With these new jet engines with bypass ratios up to 14:1 and things like variable pitch fan blades if these guys keep going these manufacturers will invent the propeller....

https://www.asme.org/engineering-topics ... ng-a-pitch

Andrew


Top

 Post subject: Re: Single engine pressurized above FL 250
PostPosted: 22 Jan 2016, 09:40 
Offline


User avatar
 Profile




Joined: 01/31/10
Posts: 13631
Post Likes: +7766
Company: 320 Fam
Aircraft: 58TC
Username Protected wrote:
Your arguments apply to the majority of airplanes...especially those that compete in the market with the SF50.

Every other jet, since none of them are singles, lands at an airport following engine failure.

Mike C.


I said "market". Your arguments revolve around "jet" not "new plane for $2MM". Buyers have budgets. The SF50 is not designed to compete with existing jet designs.
_________________
Views are my own and don’t represent employers or clients
My 58TC https://tinyurl.com/mry9f8f6


Top

 Post subject: Re: Single engine pressurized above FL 250
PostPosted: 22 Jan 2016, 10:37 
Offline


 WWW  Profile




Joined: 12/03/14
Posts: 20781
Post Likes: +26295
Company: Ciholas, Inc
Location: KEHR
Aircraft: C560V
Username Protected wrote:
The SF50 is not designed to compete with existing jet designs.

They have accomplished that goal.

The question is if there is truly a real SEJ market at all once the euphoria of the concept meets reality.

Mike C.

_________________
Email mikec (at) ciholas.com


Top

 Post subject: Re: Single engine pressurized above FL 250
PostPosted: 22 Jan 2016, 13:01 
Offline


User avatar
 Profile




Joined: 01/29/08
Posts: 26338
Post Likes: +13085
Location: Walterboro, SC. KRBW
Aircraft: PC12NG
Username Protected wrote:
The question is if there is truly a real SEJ market at all once the euphoria of the concept meets reality.

Mike C.

You still don't know what reality is for the SF50. None of us do.

I still say...... Cirrus has a lot of smart people working for them. The things you say won't work about the SF50 are the most basic concepts of designing an airplane. Why would they have come this far if things as basic as what you're pointing out were truly realities of SE Jet design? If what you say is true this thing would have never made it through the first meeting on the concept. So how did it get this far?


Top

 Post subject: Re: Single engine pressurized above FL 250
PostPosted: 22 Jan 2016, 13:08 
Offline


 Profile




Joined: 11/09/13
Posts: 1910
Post Likes: +927
Location: KCMA
Aircraft: Aero Commander 980
Do you believe every new product that hits the market is guaranteed success?


Top

 Post subject: Re: Single engine pressurized above FL 250
PostPosted: 22 Jan 2016, 13:11 
Offline


User avatar
 Profile




Joined: 01/29/08
Posts: 26338
Post Likes: +13085
Location: Walterboro, SC. KRBW
Aircraft: PC12NG
Username Protected wrote:
Do you believe every new product that hits the market is guaranteed success?

That's besides the point and not applicable to this situation.

Everything you guys poo poo the SF50 over is widely known knowledge. It's not some secret. It's extremely basic stuff.


Top

 Post subject: Re: Single engine pressurized above FL 250
PostPosted: 22 Jan 2016, 13:15 
Offline


 Profile




Joined: 11/03/08
Posts: 16918
Post Likes: +28739
Location: Peachtree City GA / Stoke-On-Trent UK
Aircraft: A33
Let's get away from engineering and look at the big picture. Cirrus created the market for plastic parachute-equipped planes from thin air just like apple created the market for ipods. There was no need for those products until they were introduced, but once available they became ubiquitous.

Is there a market for a SE jet that sits in a currently unserved niche? Who knows, why don't we wait and see. The track record of the people making it is pretty good when it comes to creating new market segments.


Top

Display posts from previous:  Sort by  
Reply to topic  [ 676 posts ]  Go to page Previous  1 ... 27, 28, 29, 30, 31, 32, 33 ... 46  Next



Postflight (Bottom Banner)

You cannot post new topics in this forum
You cannot reply to topics in this forum
You cannot edit your posts in this forum
You cannot delete your posts in this forum
You cannot post attachments in this forum

Jump to:  

Terms of Service | Forum FAQ | Contact Us

BeechTalk, LLC is the quintessential Beechcraft Owners & Pilots Group providing a forum for the discussion of technical, practical, and entertaining issues relating to all Beech aircraft. These include the Bonanza (both V-tail and straight-tail models), Baron, Debonair, Duke, Twin Bonanza, King Air, Sierra, Skipper, Sport, Sundowner, Musketeer, Travel Air, Starship, Queen Air, BeechJet, and Premier lines of airplanes, turboprops, and turbojets.

BeechTalk, LLC is not affiliated or endorsed by the Beechcraft Corporation, its subsidiaries, or affiliates. Beechcraft™, King Air™, and Travel Air™ are the registered trademarks of the Beechcraft Corporation.

Copyright© BeechTalk, LLC 2007-2025

.aerox_85x100.png.
.Wentworth_85x100.JPG.
.KalAir_Black.jpg.
.AAI.jpg.
.traceaviation-85x150.png.
.blackhawk-85x100-2019-09-25.jpg.
.performanceaero-85x50.jpg.
.aviationdesigndouble.jpg.
.concorde.jpg.
.Elite-85x50.png.
.ssv-85x50-2023-12-17.jpg.
.dbm.jpg.
.8flight logo.jpeg.
.Latitude.jpg.
.jetacq-85x50.jpg.
.Plane AC Tile.png.
.v2x.85x100.png.
.shortnnumbers-85x100.png.
.midwest2.jpg.
.pdi-85x50.jpg.
.boomerang-85x50-2023-12-17.png.
.daytona.jpg.
.kingairnation-85x50.png.
.camguard.jpg.
.ABS-85x100.jpg.
.planelogix-85x100-2015-04-15.jpg.
.wat-85x50.jpg.
.rnp.85x50.png.
.sierratrax-85x50.png.
.SCA.jpg.
.mcfarlane-85x50.png.
.avnav.jpg.
.AeroMach85x100.png.
.stanmusikame-85x50.jpg.
.LogAirLower85x50.png.
.jandsaviation-85x50.jpg.
.CiESVer2.jpg.
.holymicro-85x50.jpg.
.ocraviation-85x50.png.
.tat-85x100.png.
.geebee-85x50.jpg.
.blackwell-85x50.png.
.bullardaviation-85x50-2.jpg.
.KingAirMaint85_50.png.
.BT Ad.png.
.saint-85x50.jpg.
.bpt-85x50-2019-07-27.jpg.
.gallagher_85x50.jpg.
.Wingman 85x50.png.
.tempest.jpg.
.suttoncreativ85x50.jpg.
.Aircraft Associates.85x50.png.
.puremedical-85x200.jpg.
.headsetsetc_Small_85x50.jpg.
.temple-85x100-2015-02-23.jpg.
.sarasota.png.
.garmin-85x200-2021-11-22.jpg.
.MountainAirframe.jpg.
.airmart-85x150.png.
.b-kool-85x50.png.
.kadex-85x50.jpg.