Alphafloor From Chile, joined Jun 2004, 1277 posts, RR: 35 Posted (11 years 9 months 3 weeks 10 hours ago) and read 7149 times:
I have a some questions regarding the pressure of the tires of a plane and gear bays. When the tires of a 737 retracts the gears bay do not close, the tires are still visible when they are retracted after take-off as seen below.
I wonder in which proportions these tires increases volume at cruising altitude due to the lower pressure of the environment. I assume the pressure of the tires also increases when climbing and the tires are strong enough to deal with this increase of pressure. I also wanted to know if the gear bays of the 777, 747, MD-11, a320 are pressurized or not ? Why the 737 don't have a closed gears bay ? Isn’it more reliable to have closed gears bay ?
Greasespot From Canada, joined Apr 2004, 3104 posts, RR: 19
Reply 1, posted (11 years 9 months 3 weeks 10 hours ago) and read 7090 times:
As far as I know no wheel wells are pressurized. I guess Boeing did not used enclosed bays because there is a lot less monkey motion required for gear up. IE: no doors to open or close. Therefore there is no doors to rig or actuators to change. So no doors is in a sense more reliable than having doors.
I do not understand what you mean by which proportions. The tires do not have any chambers so they increase and decrease equally.
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EMBQA From United States of America, joined Oct 2003, 9453 posts, RR: 10
Reply 2, posted (11 years 9 months 3 weeks 10 hours ago) and read 7079 times:
I'm sure with the drop in atmospheric pressure as the aircraft climbs in altitude the tire pressure will go up slightly....but your talking ever so slight. The tire pressure will change more when they heat up after landing.
And No....No wheel wells that I can think of are pressurized.
"It's not the size of the dog in the fight, but the size of the fight in the dog"
Klaus From Germany, joined Jul 2001, 21652 posts, RR: 53
Reply 3, posted (11 years 9 months 3 weeks 10 hours ago) and read 7069 times:
Landing gear bays are generally unpressurized.
The tire pressure is so high anyway that the additional difference between sea level and cruise altitude doesn´t make a big difference. They´d probably survive a total vacuum just as well. On touchdown and taxi they´ll have to deal with much worse.
And the standard answer regarding the 737: The rationale given was that the development cost, the added weight and complexity of full doors (and a "deeper" wheel well) would not have been justified by the relatively small reduction in drag.
HAWK21M From India, joined Jan 2001, 31875 posts, RR: 54
Reply 4, posted (11 years 9 months 3 weeks 8 hours ago) and read 7044 times:
B737s do have LG Doors in fact three on each gear called the Inner,Mid & outer.But these are fixed & rotate with the gear & yes the Outbd side of the Outbd wheel is exposed.Why add to the weight.
320tech From Turks and Caicos Islands, joined May 2004, 491 posts, RR: 5
Reply 5, posted (11 years 9 months 3 weeks 8 hours ago) and read 7034 times:
Think of it this way - tire pressure is around 200 psi. Sea level pressure is about 15 psi. Pressure at 35,000 feet is, well, I dunno, and I just got off midnight shift, so I'm not looking it up - but suppose it's 5 psi. Total relative increase - 10 psi. Big deal.
The primary function of the design engineer is to make things difficult for the manufacturer and impossible for the AME.
Prebennorholm From Denmark, joined Mar 2000, 7142 posts, RR: 53
Reply 8, posted (11 years 9 months 3 weeks ago) and read 6933 times:
The eventually slightly increased tire pressure at altitude is peanuts compared to the pressure increase when the bird is slammed down on the runway on one wheel only in crosswind.
The relative pressure increase is much higher on a car tire when crossing a high mountain pass. A car with a nominal tire pressure of 30 PSI may experience 34 PSI on a high mountain pass - well over 10% increase. Still we don't even notice that. A 737 with 200 PSI will never experience more than a 5% increase at altitude.
I would guess that the heat from the brakes - transferred to the wheels - after a landing produces a much higher pressure increase than any altitude the 737 can reach. But that's guesswork, I don't know.
Always keep your number of landings equal to your number of take-offs
Avioniker From United States of America, joined Dec 2001, 1109 posts, RR: 10
Reply 9, posted (11 years 9 months 2 weeks 6 days 23 hours ago) and read 6907 times:
Just to throw something into the mix;
If the area of a tire expands due to a decrease in external pressure then the internal volume would also increase therefore the internal pressure will decrease (psi, remember?). Pressure (psi) is measured as a representative value of the force exerted on a square inch of internal surface area.
Aircraft tires are designed to resist that sort of expansion but I just thought I'd throw that in.
For you trivia buffs, the standard for aircraft sidewall flex on landing is 35%. An automobile tire is designed to regularly flex 80 to 90%.
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One may educate the ignorance from the unknowing but stupid is forever. Boswell; ca: 1533
MaerskMech From Denmark, joined Oct 2004, 16 posts, RR: 0
Reply 10, posted (11 years 7 months 2 weeks 8 hours ago) and read 6685 times:
10-15 minutes after landing the pressure is between 240 and 260 psi. thats the figures I have measured myself. If the pilot made a high speed landing the pressure might be even higher.
the normal pressure in our company is 210 psi. (737-700).
Goldenshield From United States of America, joined Jan 2001, 6170 posts, RR: 13
Reply 11, posted (11 years 7 months 2 weeks 2 hours ago) and read 6580 times:
Also, the tempurature plays a lot into it as well. As the the air gets colder, the pressure decreases, and as it gets warmer, it increases.
There is also the gas law, or P/DT = R, or Pressure divided by density times tempurature equals a relative constant. So by using this, you can reduce pressure by decreasing the tempurature, by reducing mass, and by increasing the volume. Since a tire is an enclosed object, we cannot reduce the mass, so tempurature and volume play a part here; therefore, as the aircraft rises, the volume in the tire may increase due in part to the nature of rubber, but it is offset by the cooling of the air outside the tire, and over time, inside as well. On landing, the heat created by friction would be enough to raise the pressure inside the tire, while the volume would still remain the same, or maybe a percent or two different due to the rubber heating.
This would explain the tire pressures that Maersk has noted here.
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MaerskMech From Denmark, joined Oct 2004, 16 posts, RR: 0
Reply 12, posted (11 years 7 months 2 weeks 1 hour ago) and read 6550 times:
It's the brakes that heat up the tire. Don't think that the aircraft rise. cause you really can't see any difference if there are 145 psi or 240 psi. If the tire rises it is millimeters we are talking about. The tires are very rigid.
Stealthpilot From India, joined May 2004, 510 posts, RR: 0
Reply 14, posted (11 years 7 months 1 week 6 days 20 hours ago) and read 6430 times:
The topic of pressure was well covered so i wont get into it
The question about why there are no bay doors, well simply because they dont need to be there. There is a negligable difference in drag with LG doors so it's the same thing aerodynamicaly to not have them. saves wieght, moving parts, space, complexity, money..... lots to think of.
StudentFlyer From Australia, joined Sep 2004, 688 posts, RR: 3
Reply 15, posted (11 years 7 months 1 week 3 days 19 hours ago) and read 6127 times:
In relation to aircraft tyres, is it true that instead of using regular air, they use nitrogen? If so, what advantages does nitrogen content in a tyre have compared with normal air? I have heard that this is the technology used these days, so I'm wondering if it's true or not.
LeanOfPeak From United States of America, joined Oct 2004, 509 posts, RR: 1
Reply 16, posted (11 years 7 months 1 week 3 days 16 hours ago) and read 6103 times:
Just to go into nauseating detail...
Conceptual design of a new aircraft is basically a series of trade studies. You start with a payload, a range, a cruise speed, and a required runway performance, etc. That eventually gives you, based largely on historical trends, such things as weights, fuel requirements, wing areas, etc.
Once you have an estimated empty weight for the aircraft and some modicum of aerodynamic data for the various proposed configurations, you can start to trade off.
Gear doors add weight. If you just take off, fly around the pattern, and land again, it costs you more fuel to haul that weight around than the fuel it saves aerodynamically. At some set distance you can assume for the length of a typical trip for the proposed aircraft, the (small) aerodynamic cleanup of the doors will save more fuel than it costs to haul the weight of the doors.
Beyond that trip length, eventually you might save enough fuel (Assuming a given fuel price) to overcome not just the weight of the inner gear doors, but also the up-front purchase-price difference of developing and building the doors, as well as the extra maintenance costs they incur. If the aircraft is planned to fly farther than that distance more often than not, you put on gear doors. If not, you don't.
That same type of trade is applied to most design decisions on the aircraft, sometimes returning to decisions you've already made to see if a design change impacts the trade study for another design decision.
This is the reason you see winglet retrofits on 737's. With an increase in fuel cost, aerodynamic cleanup becomes proportionally less expensive. Eventually, the aerodynamic cleanup (Particularly on longer trips) pays for itself and turns a profit. At the fuel prices expected when the aircraft was designed, it wasn't thought it would pay off, but it will now.
Of course, sometimes a very small performance or cost penalty will be accepted for marketing reasons (OEM winglets sometimes being one of these cases). However, if you told the board of a major airline that they should buy your airplane because it has inner main gear doors, you'd probably be laughed out of the office, so they tend to succumb to the black-and-white, rational trade-study analysis more often than not.
Finally, if you can't justify the time and expense of a trade study or if a good estimate of weight or aerodynamics can not be made, the decision might be made based on what the engineers like, what management likes, what looks like it might work best, or what's easiest to do.
As for the Nitrogen-filled tires, I understand some of the reason to be that Nitrogen is not flammable.