I think of "zoom reserve" as that airspeed above stall speed that could potentially be "converted" into altitude.
A "quick zoom" (rapid deceleration resulting from increasing the angle of attack by pulling on the stick or yoke) initially results in a rapid increase in lift (which translates into altitude). But it also comes at the expense of an equally rapid deceleration in airspeed (law of conservation of energy). It's not sustainable long term, obviously, because eventually airspeed would decrease below stall speed and the airplane would again begin to descend – rather rapidly.
A "slow zoom" is very useful if/when the engine fails, because you can trade off airspeed to "maintain altitude" for at least a little while. That allows you time to re-pitch for best glide speed, select a landing area, run through the emergency procedure, and perhaps even make a "Mayday" call on the radio...
We also take advantage of that "zoom reserve" on every landing, as we flare the plane to convert airspeed into additional lift to slow the rate of descent and cushion the landing. Done to perfection, our trade-off results in touchdown at minimal vertical descent rate just as the wing stalls – those seldom-experienced (at least by me) "chirp-chirp" landings... (And, as Contact often reminds us, that touchdown speed can be well below the published stall speed, due to "ground effect.")
If/when we manage to initiate a stall (or when "stall becomes imminent" per current FAA training directives), we are taught to do the opposite of a "zoom climb" to correct for the stall: we convert altitude back into airspeed by lowering the nose, re-establishing the wing's normal lift profile, and resuming normal flight...
As an Army helicopter instructor pilot, I used to tell our pilots that we were basically "energy managers" when piloting helicopters. Helicopter flight is all about managing lift, drag, gravity, airspeed, and torque – balancing all those using both hands and both feet on the controls. And it is largely a mental exercise which had to learned well enough to only occupy 10-15% of their brain power, so they could use the remaining 85-90% to handle their "real job," which was the combat mission assigned to them. Managing the helicopter's energy had to become a "background" task that didn't disrupt everything else... That was what separated Army Aviators from the "pilots" in civilian life.
But back on the topic of converting airspeed to altitude, or vice-versa: I used to explain autorotation technique (how a helicopter lands following an engine failure) as being the process of preserving as much of the energy the helicopter had acquired before the engine quit, for as long as possible until the helicopter was ready to land. After all, it is impossible to "add" any more energy to the system once the engine quits. (Once again, that pesky "law of conservation of energy" rears its head...)
But because high G-forces are what get people killed in "crash landings" we needed to burn off as much of that remaining energy as we safely could in the process of the helicopter arriving at the landing site and touching down safely. The odds of surviving a moderately slow landing with moderately slow vertical velocity are excellent, because of the low velocities involved. The G-forces would be much higher if you landed at closer to cruise speed, even if your vertical velocity was at zero (like crashing a car into a tree at 60 mph). The G-forces would also be much higher if you landed with zero airspeed, but with a very high descent rate (like jumping off a 3-story building).
Done absolutely perfectly, the landing after an autorotative descent would occur at zero forward airspeed and zero vertical rate of descent. In the "real world," that scenario rarely works out so perfectly. But every Army pilot with whom I ever flew (once they became familiar with the OH-58A) could consistently land at or below a brisk walking speed, with no more "vertical impact" than you would experience in stepping off a low stool. I always found it interesting how almost every pilot was smoother landing from an autorotation (even a "surprise" hovering autorotation) than they were able to land from a normal hover... It was just uncanny!
So, "airspeed into altitude" or "altitude into airspeed" are just different ways of expressing the law of conservation of energy. You can use one to buy the other, or vice-versa. It also helps explain why attitude controls airspeed, but attitude affects both airspeed and altitude... But that's a discussion for another day...