PDA

View Full Version : P51 gear doors


V1650
25th Jan 2014, 13:41
Can anybody shed some light on the purpose of the polished inner section of the P51 main gear clam shell doors.

barit1
25th Jan 2014, 17:35
V1650:

inner section: I presume you mean the inner skin panel, with spanwise "corrugations". This is a stiffener inner skin, riveted to the smooth outer skin, which maintains the shape of the door against air loads. Not unlike corrugated cardboard; It's typical of lightweight stiffening techniques used in aircraft structures.

polished: Restorers like to display pride in their handiwork.

V1650
26th Jan 2014, 15:51
That's the section I'm talking about. I thought it may have also been used to snub the mains on retraction.

clunckdriver
26th Jan 2014, 17:19
No "snubing" should be required, the pilot is suposed to brake the wheels before retraction, its all to do with gyroscopic forces and not getting a nasty smell should the tires {tyres?} indeed "snub" somthing in the gear well. Anyone who forgets to do this on one of the aircraft I fly is rewarded with a fairly load screeching noise, not audible to the pilot but all the folks on the ground hear it.

Old Photo.Fanatic
26th Jan 2014, 20:40
In anticipation that these photographs illustrate the door panel in question.

Taken at Duxford Legends in 2010.

http://i611.photobucket.com/albums/tt200/phredd10/Miscellanious/DSC_0092copy_zpsa3125c16.jpg



Taken at Oshkosh in 2011.

http://i611.photobucket.com/albums/tt200/phredd10/Miscellanious/DSC_1536_01copy_zps91c52f69.jpg


Taken at Duxford Legends 2010.
http://i611.photobucket.com/albums/tt200/phredd10/Miscellanious/DSC_0083_filtered_zps0688b4c2.jpg



Close up from Pic. 3
Good view of the construction of this door panel. (Painted)

http://i611.photobucket.com/albums/tt200/phredd10/Miscellanious/DSC_0083_filteredcopy_zpscc14587f.jpg







OPF

barit1
27th Jan 2014, 20:00
Great shots!

Also readily seen on parked aircraft after the hydraulic system has bled down.

mightyauster
28th Jan 2014, 12:36
The purpose of the polished stainless steel section on the inner surface of the wheel doors is for the tyres to slide on during emergency extension of the undercarriage. For an emergency extension, a "T" handle is pulled on the lower sub panel below the instrument panel which releases the hydraulic system pressure and, IIRC, also releases the wheel door latches. The gear lever is then selected "down", releasing the uplocks and both the mains and tailwheel extend under gravity, hence the tyres sliding on the wheel doors, pushing them out of the way. It is ops normal, after engine shut down on the ground, to pull the "T" handle to to relieve the hydraulic system pressure and consequently the reason why you will normally see a P-51 with the wheel doors open when parked.

Vzlet
29th Jan 2014, 11:54
To hopefully add to the interesting pieces of information already in this thread, here is a retraction shot with unbraked wheels (http://www.airliners.net/photo/North-American-P-51D/1278699/L/), and a video of the gear doors closing (http://www.flickr.com/photos/vzlet/10212877184/in/set-72157636435213654) immediately upon engine start.

clunckdriver
29th Jan 2014, 12:49
When I went through training on various North American products, if the "Eagle Eyed "duty pilot in the shack half way down the runway saw your wheels still rotating at high RPM on retraction it would cost one a contribution to the "Rumble Fund" on return from the flight, for a second incident one would be sent out to the duty pilot shack for a few days to be the "spotter" for gear-up approaches and unbraked retractions along with other student foul ups, both far more effective than a "bolicking" from some senior officer I found! {dont ask how I know}

Vzlet
29th Jan 2014, 13:30
Googling turned up a P-51 (D & K models) flight manual (http://books.google.com/books?id=SfwqCTY9I6MC&pg=PA18&lpg=PA18&dq=p-51+braking+during+gear+retraction&source=bl&ots=hONCTsVTE-&sig=4oRGCZiZ5_JQzoaC4HB_8mrS8fU&hl=en&sa=X&ei=MgzpUrKuKJOosAT1yYHABQ&ved=0CCMQ6AEwADgK#v=onepage&q=p-51%20braking%20during%20gear%20retraction&f=false)that states "After takeoff, never brake the wheels to stop them from turning. If the brakes are hot from excessive ground use, they are likely to freeze."

clunckdriver
29th Jan 2014, 16:01
Well, only about 150 hours on type, but have never been told or read that, I do remember however that when picking up T6s South of the border the Americans were suprised we used the brakes after T/O, they didnt, however now they are all owned by very rich guys , let them worry about it.

barit1
29th Jan 2014, 22:16
After takeoff, never brake the wheels to stop them from turning. If the brakes are hot from excessive ground use, they are likely to freeze.

Rather an overblown academic point of view; possible, not so likely. It would take a lot of aggressive taxiing to get brakes that hot, and the kinetic energy in the wheels after takeoff is quite low compared to braking during landing.

:confused:

Vzlet
30th Jan 2014, 00:42
I don't mean to come across as defending the "don't brake" method (especially as I have "about 150 hours on type" less than clunkdriver!), but it's interesting that there are two such diametrically opposed views. Could the pilot's manual be based on the assumption of much heavier operating weights than is typical today?

mightyauster
30th Jan 2014, 09:45
Part of the retraction test on the P-51 is to ensure there is a minimum clearance of 1/2" between the tyre and any components and/or structure in the wheel well to allow for tyre "growth" due to a spinning wheel. :)