Open main menu
Home
Random
Recent changes
Special pages
Community portal
Preferences
About Wikipedia
Disclaimers
Incubator escapee wiki
Search
User menu
Talk
Dark mode
Contributions
Create account
Log in
Editing
Pulsejet
(section)
Warning:
You are not logged in. Your IP address will be publicly visible if you make any edits. If you
log in
or
create an account
, your edits will be attributed to your username, along with other benefits.
Anti-spam check. Do
not
fill this in!
{{Short description|Engine where combustion is pulsed instead of continuous}} {{Use dmy dates|date=February 2020}} [[file:Pulse Jet Engine.PNG|thumb|300px|Diagram of a valved pulsejet. 1 - Air enters through valve and is mixed with fuel. 2 - The mixture is ignited, expands, closes the valve and exits through the tailpipe, creating thrust.3 - Low pressure in the engine opens the valve and draws in air.]] {{Seriesbox aircraft propulsion}} A '''pulsejet engine''' (or '''pulse jet''') is a type of [[jet engine]] in which combustion occurs in [[Pulse (physics)|pulse]]s. A pulsejet engine can be made with few<ref>{{cite web |url=http://gofurther.utsi.edu/Projects/PulseDE.htm |title=Pulse Detonation Engine |publisher=Gofurther.utsi.edu |access-date=3 March 2014 |archive-url=https://web.archive.org/web/20140904022120/http://gofurther.utsi.edu/Projects/PulseDE.htm |archive-date=4 September 2014 |url-status=dead }}</ref> or no [[moving parts]],<ref>{{cite web|url=https://news.google.com/patents/about?id=vOZsAAAAEBAJ |access-date=23 February 2016 |title=Google News }}{{dead link|date=June 2024|bot=medic}}{{cbignore|bot=medic}}</ref><ref>{{cite web|url=https://patents.google.com/patent/US6216446 |title=Patent US6216446 β Valveless pulse-jet engine with forward facing intake duct β Google Patents |access-date=3 March 2014}}</ref><ref>{{cite web |url=http://www.home.no/andreas.sunnhordvik/English/mechanical/valveless_e.htm |title=Valveless Pulsjet |publisher=Home.no |access-date=3 March 2014 |archive-date=6 September 2013 |archive-url=https://web.archive.org/web/20130906211013/http://www.home.no/andreas.sunnhordvik/English/mechanical/valveless_e.htm |url-status=dead }}</ref> and is capable of running statically (that is, it does not need to have air forced into its inlet, typically by forward motion). The best known example is the [[Argus As 014|Argus As 109-014]] used to propel [[Nazi Germany]]'s [[V-1 flying bomb]]. Pulsejet engines are a lightweight form of jet propulsion, but usually have a poor [[compression ratio]], and hence give a low [[specific impulse]]. The two main types of pulsejet engines use resonant combustion and harness the combustion products to form a pulsating exhaust jet that intermittently produces thrust. The traditional valved pulsejet has one-way valves through which incoming air passes.<ref>{{cite web | url=https://patents.google.com/patent/US2942412A/en | title=Pulse detonation jet propulsion }}</ref> When the fuel mix is ignited, the valves close, which means that the heated gases can only leave through the engine's tailpipe, thus creating forward thrust. The second type is the valveless pulsejet.<ref>{{cite journal|last=Geng|first=T.|author2=Schoen, M. A. | author3 = Kuznetsov, A. V. |author4= Roberts, W. L. |title=Combined Numerical and Experimental Investigation of a 15-cm Valveless Pulsejet|journal=Flow, Turbulence and Combustion | year = 2007 | volume = 78 | issue = 1 | pages=17β33|doi=10.1007/s10494-006-9032-8|bibcode=2007FTC....78...17G |s2cid=122906134}}</ref> The technical terms for this engine are acoustic-type pulsejet, or aerodynamically valved pulsejet. One notable line of research includes the [[pulse detonation engine]], which involves repeated detonations in the engine, and which can potentially give high compression and reasonably good efficiency.
Edit summary
(Briefly describe your changes)
By publishing changes, you agree to the
Terms of Use
, and you irrevocably agree to release your contribution under the
CC BY-SA 4.0 License
and the
GFDL
. You agree that a hyperlink or URL is sufficient attribution under the Creative Commons license.
Cancel
Editing help
(opens in new window)